МОДУЛЬ ДЛЯ ВОЗДУШНОГО СУДНА И СПОСОБ ЕГО ФОРМИРОВАНИЯ

Изобретение относится к области авиастроения, в частности к модулю для воздушного судна и способу его формирования. Модуль содержит рамный компонент (2) и функциональный элемент (4). Боковой участок предназначен для крепления функционального элемента (4) и имеет конфигурацию, соответствующую конфигурации фюзеляжа (6) или элемента (5) пола воздушного судна. При этом рамный компонент выполнен таким образом, что охватывает центр тяжести функционального элемента и приспособлен для крепления к элементу (5) пола воздушного судна в первом местоположении (7) и для крепления к элементу крепления к конструкции фюзеляжа (6) воздушного судна во втором местоположении (7′). Функциональный элемент (4) может представлять собой элементы (14) сиденья, магазины (11) хранения вещей, информационные табло, кухни, туалеты, пассажирские сервисные блоки, лампы, воздушные кондиционеры, громкоговорители, телевизоры, компьютеры и кислородные маски. Также на воздушном судне может использоваться система из множества ...

КРЕПЕЖНОЕ УСТРОЙСТВО

Изобретение относится к области самолетостроения. Устройство (1) для свободного от колебаний закрепления встраиваемых стеновых или половых элементов (3) на несущей конструкции (4) содержит крепежный элемент (5), выполненный на одном конце (6) для фиксации на несущей конструкции (4), а на противоположном конце (7) - для размещения встраиваемых элементов (2). Противоположный конец (7) крепежного элемента (5) установлен с возможностью перемещения в соединяемой с размещаемыми встраиваемыми элементами (2) распорной втулке (21) и выполнен для фиксации на них. Демпфирующий элемент (8) расположен между несущей конструкцией (4) и встраиваемыми элементами (2). Распорная втулка (21) имеет сечение в виде удлиненного отверстия, а конец (6) крепежного элемента (5) образован ножкой (6′) или с возможностью соединения с ножкой (6′), которая выполнена для установки с возможностью перемещения в расположенном на несущей конструкции (4) шинном профиле (14). Изобретение направлено на развязывание от колебаний ...

СЕГМЕНТ САЛОНА И СОДЕРЖАЩЕЕ ЕГО ТРАНСПОРТНОЕ СРЕДСТВО

Изобретение относится к авиации и касается создания сегмента салона для транспортного средства, в частности для воздушного судна. Сегмент салона содержит две или больше площадей паркования, расположенных рядом друг с другом, отделенных друг от друга промежуточной стенкой и предназначенных для установки служебных тележек. Сегмент салона также содержит кресло обслуживающего транспортное средство лица, которое на одной стороне закрепляется на промежуточной стенке с возможностью поворота на оси. Причем кресло обслуживающего лица выполнено с возможностью поворота в положение использования и скрытое положение, расположенные друг от друга под углом 90° или более относительно оси поворота кресла. Достигается улучшенное использование имеющегося пространства для установки оборудования в салоне. 3 н. и 12 з.п. ф-лы, 11 ил.

СБОРНАЯ КОНСТРУКЦИЯ ДЛЯ КРЕПЛЕНИЯ КОМПОНЕНТОВ ОБОРУДОВАНИЯ ВНУТРИ ФЮЗЕЛЯЖА САМОЛЕТА

Изобретение относится к области авиации и касается конструкций крепления компонентов внутреннего оборудования в пассажирском салоне самолета. Сборная конструкция для крепления компонентов оборудования внутри фюзеляжа самолета содержит средства крепления, выполненные на фюзеляже, элементы подвески, неподвижно соединенные с указанными средствами крепления, и проходящую в продольном направлении фюзеляжа системную опору, соединенную с элементами подвески. Элементы подвески включают в себя первый элемент подвески и второй элемент подвески. Причем каждый из первых элементов подвески жестко соединен с системной опорой, а каждый из вторых элементов подвески образует с системной опорой скользящее соединение так, что системная опора имеет возможность скольжения относительно этих вторых элементов подвески вдоль продольной оси фюзеляжа самолета. Достигается значительное снижение передаваемых от системных опор нагрузок на шпангоуты в продольном направлении, компенсация погрешностей при изготовлении, ...

КОМПОНОВКА ВЕРХНЕЙ ЧАСТИ КАБИНЫ ЛЕТАТЕЛЬНОГО АППАРАТА

... 1. Кабина (4) летательного аппарата, предназначенного для пассажирских перевозок, содержащая главную конструкцию (18), соответствующую конструкции летательного аппарата и охватывающую кабину (4); палубу (20), образующую плоскую поверхность, на которой закреплены кресла (12, 42); проход (32), расположенный в кабине (4) в продольном направлении и приподнятый по отношению к палубе (20); и спальные места (14), обслуживаемые с упомянутого прохода (32) и расположенные над креслами (12, 42) палубы (20), отличающаяся тем, что спальные места (14), обслуживаемые с приподнятого прохода (32), расположены поперечно по отношению к проходу (32) и по обе стороны от него. 2. Кабина (4) летательного аппарата по п.1, отличающаяся тем, что спальные места (14) подвешивают со стороны центрального прохода (32) к главной конструкции (18) кабины (4) и со стороны, противоположной проходу, соединяют с этой конструкцией (18). 3. Кабина (4) летательного аппарата по п.2, отличающаяся тем, что в качестве несущих элементов ...

МЕДИЦИНСКИЙ ПУНКТ ДЛЯ КАБИНЫ ВОЗДУШНОГО СУДНА, КОНСТРУКТИВНО СОВМЕЩЕННЫЙ С КУШЕТКОЙ

... 1. Медицинский пункт для салона воздушного судна, выполненный конструктивно совместно с кушеткой (2), предназначенной для размещения пациента в лежачем положении, отличающийся тем, что содержит: ! систему водоснабжения, ! систему электроснабжения, ! зону размещения тележки, рассчитанную, по меньшей мере, на одну тележку (12), ! по меньшей мере, одну тележку (12), расположенную в зоне размещения тележки и снабженную ящиками для хранения медицинской аппаратуры, и ! дверцу обеспечения доступа (56) к каждой тележке (12), оборудованную средствами блокировки и обеспечивающую возможность доступа к ящикам указанной тележки. ! 2. Медицинский пункт по п.1, отличающийся тем, что каждая дверца доступа (56) обеспечивает возможность доступа к ящикам соответствующей тележки (12) со стороны зоны, предназначенной для размещения пассажиров. ! 3. Медицинский пункт по п.2, отличающийся тем, что он оборудован средствами удержания (52, 54), препятствующими перемещению тележки (12) в направлении зоны, соседней ...

ШАРНИРНЫЙ УЗЕЛ ПОЛКИ

СЕКЦИЯ ФЮЗЕЛЯЖА САМОЛЕТА И СОДЕРЖАЩИЙ ЕЕ САМОЛЕТ

... 1. Секция фюзеляжа самолета, которая содержит ! каркас фюзеляжа с множеством ребер, расположенных с промежутками друг от друга в продольном направлении фюзеляжа самолета; ! внешнюю обшивку, которая установлена на внешнем каркасе (2) фюзеляжа; ! причем в конструкции (4) внешней обшивки предусмотрен по меньшей мере один дверной проем (5), который при помощи по меньшей мере одного компонента каркаса фюзеляжа, разделен вертикально на множество открытых областей. ! 2. Секция фюзеляжа самолета по п.1, у которой дверной проем разделен при помощи по меньшей мере одного из множества ребер на множество открытых областей (7). ! 3. Секция фюзеляжа самолета по п.2, у которой по меньшей мере одно ребро подразделяет по меньшей мере один дверной проем (5) на множество открытых областей (7), отделенных друг от друга при помощи указанного ребра. ! 4. Секция фюзеляжа самолета по п.2, у которой по меньшей мере одно ребро (3) проходит главным вертикально через по меньшей мере один дверной проем ! 5. Секция ...

УСИЛЕННАЯ КОМПОЗИТНАЯ СЛОИСТАЯ ПАНЕЛЬ

... 1. Композитная слоистая панель (1), включающая в себе по меньшей мере одну сердцевину (2), помещенную между внутренним листом (3) и внешним листом (4), каждый из которых содержит группу волокнистых слоев (5, 6, 7, 8) из композитного материала, отличающаяся тем, что часть указанных слоев внутреннего листа и/или внешнего листа проходит по меньшей мере частично через указанную сердцевину, в зоне где она имеет разрыв, совместно образуя при этом по меньшей мере одно поперечное средство (9) усиления, идущее от внутреннего листа к внешнему листу композитной слоистой панели. ! 2. Панель по п.1, отличающаяся тем, что указанное поперечное средство (9) усиления выполнено по меньшей мере из одного слоя (7, 8), проходящего без разрывов от внешнего листа к внутреннему листу. ! 3. Панель по п.1, отличающаяся тем, что она имеет изогнутый участок. ! 4. Панель по п.3, отличающаяся тем, что указанное поперечное средство (9) усиления находится на указанном изогнутом участке. ! 5. Панель по п.4, отличающаяся ...

УСТРОЙСТВО ДЛЯ ПРИМЕНЕНИЯ КИСЛОРОДНЫХ МАСОК

... 1. Картридж для использования с коллектором, при этом коллектор имеет проход, поддерживающий обмен текучей средой с источником дыхательной смеси, причем картридж содержит: торцевую стенку; по меньшей мере одну боковую стенку, идущую от торцевой стенки и заканчивающуюся на дистальном конце рядом с отверстием; эластичный элемент, определяющий камеру в картридже, причем камера поддерживает обмен текучей средой с проходом, когда картридж подсоединен к коллектору, а эластичный элемент имеет выпускное отверстие; узел маски, размещенный в картридже, при этом узел маски имеет рукав, соединенный с выпускным отверстием эластичного элемента; при этом давление на эластичный элемент, вызываемое потоком дыхательной смеси в камеру, заставляет маску выталкиваться из картриджа через отверстие на дистальном конце по меньшей мере одной боковой стенки. 2. Картридж по п.1, дополнительно содержащий фланец, допускающий зацепление с защелкивающим элементом на коллекторе. 3. Картридж по п.1, в котором эластичный ...

ПОТОЛОЧНАЯ СЕКЦИЯ БАГАЖНИКА ДЛЯ САМОЛЁТОВ И САМОЛЁТ

КРЕПЕЖНОЕ УСТРОЙСТВО

... 1. Устройство (1) для свободного от колебаний закрепления встраиваемых элементов (2), в частности стеновых или половых элементов (3) в самолетах, на несущей конструкции (4), содержащее крепежный элемент (5), выполненный на одном конце (6) для фиксации на несущей конструкции (4), а на противоположном конце (7) - для размещения встраиваемых элементов (2), причем противоположный конец (7) крепежного элемента (5) установлен с возможностью перемещения в соединяемой с размещаемыми встраиваемыми элементами (2) распорной втулке (21) и выполнен для фиксации на них, и, по меньшей мере, один демпфирующий элемент (8), расположенный между несущей конструкцией (4) и встраиваемыми элементами (2), отличающееся тем, что конец (6) крепежного элемента (5), образованного болтом (11) с головкой (13) и резьбой (12), образован ножкой (6′) или выполнен с возможностью соединения с ножкой (6′), которая выполнена для установки с возможностью перемещения в расположенном на несущей конструкции (4) шинном профиле (14 ...

УЗЕЛ ДЛЯ СИДЕНИЯ

... 1. Узел (1) для сидения для салона самолета, содержащий неподвижный корпус (41), кресло (2) со спинкой (42), расположенной в неподвижном корпусе, и частью для сидения (43), тележку (56), связанную с частью для сидения кресла (2), причем тележка выполнена с возможностью приведения ее в движение для перемещения части для сидения между убранным положением и раздвинутым положением, причем часть для сидения (43) и спинка (42) выполнены с возможностью их взаимодействия таким образом, что при перемещении части для сидения между убранным и выдвинутым положениями обеспечивается перемещение спинки между, по существу, вертикальным и откинутым положениями, с нахождением спинки, по существу, внутри корпуса, при этом во время нахождения спинки в откинутом положении и нахождении части для сидения в раздвинутом положении, спинка и часть для сидения образуют, по существу, плоскую поверхность. 2. Узел по п.1, в котором спинка (42) соединена одним своим концом с частью для сидения (43). 3. Узел по любому ...

LUFTFAHRZEUG MIT TRAGFLUEGELN UND EINEM RUMPF

SAUERSTOFFVERSORGUNGSEINHEIT MIT EINEM SAUERSTOFFGENERATOR ZUM EINBAU IN FLUGGERAETE.

Oxygen supply unit for building into the ceiling of the passenger compartment of large jumbo jets over each row of seats comprises casing with a carrier frame to which a deep drawn plasticshell holding four half masks is fixed. The oxygen generator is fixed by clips to a web and the four masks are suspended by their leads from the mount.

Sauerstoffmaske

Die Erfindung betrifft eine Sauerstoffmaske (1) für die Sauerstoffnotversorgung von Passagieren in einem Flugzeug, mit einem Träger (12), an welchem ein Atembeutelanschluss (5) für einen Atembeutel (11), ein Einatemventil (3) und ein Ausatemventil (4) vorgesehen sind, wobei der Träger (12) mindestens zwei schwenkbar zueinander angeordnete Trägerteile (14, 15, 16) aufweist.

Magnetabscheider zur Abscheidung ferromagnetischer Partikel aus einem Absaugluftstrom

Magnetabscheider (1) zur Abscheidung ferromagnetischer Partikel aus einem Absaugluftstrom, mit einem Gehäuse (8) und zumindest einem in dem Gehäuse (8) angeordneten Magneten (6), an dem der Absaugluftstrom vorbeigeführt wird, wobei das Gehäuse (8) einen Gehäuseeinlass (2) und einen Gehäuseauslass (3) zur Montage an eine Rohrleitung eines Absaugluftstromes aufweist, wobei eine Querschnittsfläche (A1) des Gehäuseeinlasses (2) kleiner ist als eine Querschnittsfläche (A2) im Gehäuse (8), dadurch gekennzeichnet, dass mehrere Magnete (6) versetzt zueinander im Gehäuse (8) angeordnet sind und dass im Gehäuseeinlass (2) zwei Leitelemente (4.1) angeordnet sind, welche den Absaugluftstrom in drei Teilströme aufteilen und in Richtung Magnete (6) lenken.

System für die Sauerstoffnotversorgung von Passagieren in einem Flugzeug

Erfindungsgemäß wird ein System für die Sauerstoffnotversorgung von Passagieren in einem Flugzeug bereitgestellt, mit zumindest einer primären Sauerstoffmaske und zumindest einer sekundären Sauerstoffmaske, welche in einem Fach oberhalb eines Sitzes im Flugzeug angeordnet und jeweils mittels eines Schlauches mit einer Sauerstoffquelle verbunden sind, wobei die zumindest eine primäre Sauerstoffmaske derart in dem Fach angeordnet ist, dass sie vor der zumindest einen sekundären Sauerstoffmaske aus dem Fach herausfällt, wenn sich eine Klappe des Fachs öffnet, wobei das System mindestens ein Rückhaltebehältnis umfasst, welches in dem Fach angeordnet ist, und in welchem die zumindest eine sekundäre Sauerstoffmaske angeordnet ist, wobei das Rückhaltebehältnis mit einem ersten Verbindungsmittel mit dem Fach und mit einem zweiten Verbindungsmittel mit einer Auslösevorrichtung der Sauerstoffquelle verbunden ist, die mittels der mindestens einen primären Sauerstoffmaske auslösbar ist. Ferner wird ...

Hecknotausgangs- und Steuerungsvorrichtung für ein Flugzeug

Trennwandvorrichtung und Verfahren zur Herstellung einer Trennwandvorrichtung

Die Erfindung geht aus von einer Trennwandvorrichtung, insbesondere für ein Fahrzeug (10a), mit zumindest einer Rahmeneinheit (12a; 12b: 12c), welche zumindest in einem montierten Zustand zumindest einen Trenneinheitenaufnahmebereich (14a) definiert, und welche zumindest einen Rahmenabschnitt (16a; 16b; 16c) aufweist. Es wird vorgeschlagen, dass der Rahmenabschnitt (16a; 16b; 16c) entlang einer in dem Rahmenabschnitt (16a; 16b; 16c) und entlang des Rahmenabschnitts (16a; 16b; 16c) verlaufenden Rahmenmittellinie (18a; 18c) betrachtet zumindest zwei Rahmenquerschnitte (20a, 22a; 20b, 22b; 20c, 22c) aufweist, welche wesentlich verschieden voneinander sind.

Mehrzweck-Flugzeuge mit Mehrzweck-Unterdecks und Verfahren zu deren Herstellung

Verstaubarer Klapptisch

Klapptisch für ein Fahrzeug mit einer Tischplatte (38), die aus einer Verstaustellung mit vertikaler oder steil geneigter Tischoberfläche in eine Gebrauchsstellung mit horizontaler Tischoberfläche bewegbar ist, indem sie zuerst aus ihrer Verstaustellung nach oben gezogen und dann um eine horizontale Schwenkachse in die Gebrauchsstellung geklappt wird, in der sie über eine die Tischplatte (38) tragende Halterung (1) übersteht, wobei die Tischplatte (38) in der Verstaustellung in einem in der Halterung (1) ausgebildeten Staufach (10) versenkt ist, das an seinem oberen Ende eine Öffnung (32) zum Herausziehen der Tischplatte (38) aufweist, dadurch gekennzeichnet, dass diese Tischplatte (38) im stauraumseitigen horizontalen Randbereich mit zwei seitlich überstehenden Zapfen (48) versehen ist, die mit an den vertikalen Schmalseiten des Staufaches (10) ausgebildeten Führungsschienen (50) verschiebbar im Eingriff stehen und die nach dem Herausziehen der Tischplatte (38) aus dem Staufach (10) in ...

Multi-link support shelf for folding table frames has individual interconnected segments extending into rigid free supporting surface but with quick release for emergency

The multi-link shelf comprises a plate of individual segments (1) connected together through force or keyed engagement and able to roll up or concertina in a guide and extend into a rigid free-supporting surface. The segments can be extended mechanically or manually and can be spread out on a folding table frame which itself comprises movable interconnected individual parts. The multi-link plate can be rapidly released in emergency cases to return to its stowage position and prevent injury to personnel.

Fahrzeugrumpf und Verfahren zur Montage eines Fahrzeugrumpfs

Die Erfindung betrifft einen Fahrzeugrumpf (10). Der Fahrzeugrumpf (10) weist eine Fahrzeugprimärstruktur (11) und eine Fahrzeuginneneinrichtung (12) sowie eine Kopplungsvorrichtung (19) zum Befestigen der Fahrzeuginneneinrichtung (12) an der Fahrzeugprimärstruktur (11) auf. Die Kopplungsvorrichtung (19) ist zum Erzeugen eines Magnetfeldes (21a) ausgeführt, um die Fahrzeuginneneinrichtung (12) berührungslos an der Fahrzeugprimärstruktur (11) zu befestigen. Die Erfindung betrifft ferner ein Verfahren zur Montage eines Fahrzeugrumpfs (10) sowie ein Bauwerk.

Beleuchtungseinrichtung und Interieurteil mit Beleuchtungseinrichtung

Die erfindungsgemäße Beleuchtungseinrichtung für ein Luftfahrzeug umfasst ein Trägermodul, einen flächigen, am Trägermodul befestigten Lichtleiter mit einer Vielzahl von Auskoppelpunkten und mehrere Lichtquellen zur Beleuchtung des Lichtleiters. Der flächige Lichtleiter ist abgedeckt mit einer transluzenten Haptikschicht, die auf einer Sichtseite des Lichtleiters befestigt ist, die wiederum von einer Dekorschicht bedeckt ist. Als zusätzliches Beleuchtungselement umfasst die Beleuchtungseinrichtung einen strangförmigen Lichtleiter, der über eine eigene Lichtquelle verfügt und mit der Dekorschicht über eine Halteeinrichtung verbunden ist. Damit ergibt sich eine flache Anordnung, die leicht in Interieurteile integriert werden kann und gleichzeitig eine großfläche Beleuchtung ermöglicht. Dabei können mittels des strangförmigen Lichtleiters zusätzliche Lichteffekte integriert werden. Indem die Beleuchtungseinrichtung von der Dekorschicht bedeckt ist, bleibt im ausgeschalteten Zustand die Beleuchtungseinrichtung ...

Panel und Panelanordnung

Bei einem Panel (4) für eine Passagierkabine eines Passagierflugzeuges, mit einem von einer Sichtseite (14) des Panels (4) zurückversetzten Aufnahmeraum (8) für eine Flächenleuchte (6), sind im Aufnahmeraum (8) zwei, sich in einer Längsrichtung (18) des Panels (4) erstreckende Aufnahmeprofile (16a,b) für die Flächenleuchte (6) zu deren Befestigung am Panel (4) angeordnet, wobei das Panel (4) an jedem der Aufnahmeprofile (16a,b) einen Fortsatz (20a,b) aufweist, der dem Aufnahmeprofil (16a,b) zur Sichtseite (14) hin vorgelagert ist und sich über das Aufnahmeprofil (16a,b) hinaus um eine Überdeckungsbreite (B) in den Aufnahmeraum (8) hinein erstreckt.Bei einer Panelanordnung (2) mit dem Panel (4) und mit der Flächenleuchte (6), sind die Flächenleuchte (6) und das Aufnahmeprofil (16a,b) geometrisch aneinander angepasst.

Innenverkleidungsanordnung für eine Flugzeugkabine

Dargestellt und beschrieben ist eine Innenverkleidungsanordnung für eine Flugzeugkabine, wobei die Innenverkleidungsanordnung ein erstes seitliches Deckenelement (1), ein zweites seitliches Deckenelement (11) und ein Winkelelement (3) mit einem ersten Schenkel (5) und einem zweiten Schenkel (7), die sich unter einem Winkel voneinander weg erstrecken, aufweist, wobei das zweite seitliche Deckenelement (11) nach oben und zu einer ersten Seite versetzt zu dem ersten seitlichen Deckenelement (1) angeordnet ist, wobei das Winkelelement (3) derart angeordnet ist, dass sich der erste Schenkel (5) zu der ersten Seite hin an das erste seitliche Deckenelement (1) anschließt, so dass das freie Ende des ersten Schenkels (5) dem zur ersten Seite weisenden freien Ende des ersten seitlichen Deckenelements (1) gegenüberliegt, und dass sich der zweite Schenkel (7) hin zu dem zweiten seitlichen Deckenelement (11) erstreckt, wobei das freie Ende (25) des zweiten Schenkels (7) in Richtung der ersten Seite ...

Verbundanordnung sowie Verfahren zur Fertigung der Verbundanordnung

Der Erfindung liegt die Aufgabe zugrunde, eine kostengünstige, gewichts- und bauraumoptimierte Verbundanordnung zur Kühlung von elektrischen und/oder elektronischen Verbrauchern bereitzustellen. Es wird eine Verbundanordnung 1 vorgeschlagen, mit mindestens einem elektrischen und/oder elektronischen Verbraucher 2, mit mindestens einem Wärmeabgabekörper zur Kühlung des mindestens einen Verbrauchers 2, so dass die von dem Verbraucher 2 produzierte Wärme Q zumindest teilweise an eine Umgebung der Verbundanordnung 1 abgegeben wird oder abgebbar ist, mit einem Träger 3, wobei der Träger 3 in einer flächigen Erstreckung eine Auflagefläche aufweist, auf der der mindestens eine Wärmeabgabekörper als wärmeleitende Folie 4 flächig aufliegt.

Schnittstellenelement, Flugzeuginnenausstattungsbauteil und Verfahren zur Montage eines Flugzeuginnenausstattungsbauteils

Schnittstellenelement (10) zur Verbindung von an einem Flugzeuginnenausstattungsbauteil (12) vorgesehenen ersten Abschnitten einer Mehrzahl von Flugzeugversorgungssystemen mit entsprechenden zweiten Abschnitten der Flugzeugversorgungssysteme, welches umfasst: – eine an dem Flugzeuginnenausstattungsbauteil (12) befestigbare Trägerstruktur (14), die eine Platte (16) sowie die Platte (16) tragende Füße (18) umfasst, wobei die Platte (16) mit einer Mehrzahl von Aussparungen (20, 22) versehen ist, und wobei die die Platte (16) tragenden Füße (18) dazu eingerichtet sind, die Trägerstruktur (14) derart an dem Flugzeuginnenausstattungsbauteil (12) zu befestigen, dass die Platte (16) in einem Abstand von dem Flugzeuginnenausstattungsbauteil (12) angeordnet ist, und – eine Mehrzahl von Anschlusselementen (26, 52), die jeweils mit einem an dem Flugzeuginnenausstattungsbauteil (12) vorgesehenen ersten Abschnitt eines Flugzeugversorgungssystems verbindbar und jeweils über eine an der Platte (16) der ...

Equipmenthalter mit optionaler Rasterfunktion

Es wird ein Equipmenthalter (1) mit optionaler Rasterfunktion zum Positionieren eines ersten Kabinenbauteils (9) eines Luftfahrzeugs in Bezug auf ein zweites Kabinenbauteil (11) und zum Befestigen der zwei Kabinenbauteile (9, 11) miteinander vorgestellt. Der Equipmenthalter (1) weist ein Befestigungselement (3), ein Fixierelement (5) und eine Positionsbestimmungsvorrichtung (7) auf. Das Befestigungselement (3) ist dabei ausgestaltet, den Equipmenthalter (1) an dem ersten Kabinenbauteil (9) zu befestigen. Das Fixierelement (5) ist dabei ausgestaltet, eine Position des Equipmenthalters (1) in Bezug zu dem zweiten Kabinenbauteil (11) zu fixieren. Ferner ist die Positionsbestimmungsvorrichtung (7) ausgestaltet, die Position des Equipmenthalters (1) in Bezug auf das zweite Kabinenbauteil (11) diskontinuierlich durch ein Positionssignal anzugeben.

System und Verfahren zur Montage von Flugzeugsystemkomponenten in der Crown Area eines Flugzeugs

Ein System (10) zur Montage von Flugzeugsystemkomponenten (28, 58) in der Crown Area eines Flugzeugs umfasst ein erstes Längsträgerelement (12), ein zweites Längsträgerelement (14) sowie ein das erste Längsträgerelement (12) mit dem zweiten Längsträgerelement (14) verbindendes Brückenelement (16). Das System ist derart in der Crown Area eines Flugzeugs montierbar, dass sich das erste und das zweite Längsträgerelement (12, 14) im Wesentlichen parallel zu der Längsachse L des Flugzeugs erstrecken. An dem ersten und/oder dem zweiten Längsträgerelement (12, 14) ist eine Mehrzahl von Kabelkanälen (26) zur Aufnahme von elektrischen Leitungen (28) ausgebildet.

Aircraft`s cabin module, has pallet forming floor element of cabin compartment, where pre-installed component e.g. seat, is pre-installed onto pallet, and quick release fastener securing pallet to floor structure

The cabin module (16, 17, 18, 19, 20, 21, 22) has a pallet forming a floor element of a cabin compartment (1), where a pre-installed component e.g. seat, is pre-installed onto the pallet. A quick release fastener secures the pallet to a floor structure of the compartment, and is disposed on a bottom side of the pallet. A structure of the fastener transfers a load imparted by the component from the pallet directly into a seat rail. A wall panel is installed onto the pallet to form a peripheral wall assembly, and a sidewall is subsequently fastened onto the pallet. An independent claim is also included for a cabin compartment comprising a set of cabins.

Internal lighting system for a helicopter uses many bright white light emitting diodes

An internal lighting system for a helicopter comprises bright white LEDs. Independent claims are also included for the following: (a) a system as above using LEDs of various colors which together give white or a near-white color; and (b) a system as above using optical fibers to illuminate the cockpit and passenger areas.

Vorrichtung zum Aufbewahren von Notausrüstungsgegenständen in einem Fahrzeug

Vorrichtung zum Aufbewahren mindestens eines Notausrüstungsgegenstands, aufweisend mindestens einen oberhalb von Passagiersitzen (4) positionierten Behälter (10) mit jeweils einer Zugriffsöffnung (16) und mindestens einem Verschlusselement (12) zum Verschließen der Zugriffsöffnung (16), wobei in dem Behälter mindestens ein Notausrüstungsgegenstand gehaltert ist, der mit einem Zugelement verbunden ist, welches bei geöffnetem Verschlusselement (12) aus der Zugriffsöffnung (16) ragt und wobei ein fernbedienbarer Verriegelungsmechanismus (22) zum Öffnen und Schließen des Verschlusselements (12) an dem Behälter (10) angeordnet ist.

Rumpfsegment und Verfahren zur Herstellung des Rumpfsegments

Rumpfsegment (2) eines Flugzeugrumpfes, mit einer kabinenseitigen Innenhaut (4) und einer Außenhaut (6), die einen Kern (8) begrenzen, dadurch gekennzeichnet, dass Leitungskanäle (20, 22) zur Systemintegration in den Kern (8) integriert sind, wobei der Kern (8) aus einem Schaummaterial gebildet ist und die Materialhärte des Kerns (8) ausgehend von einem innenhautseitigen Bereich in Richtung der Außenhaut (6) zunimmt.

Climbing module for e.g. long range aircraft, has climbing device e.g. staircase, partially covering entrance in one position and lying with its upper end on bed plate in another position for permitting climbing up and/or down of persons

The module (1) has a side wall (11) with an entrance (13) having a bed plate (14), and a climbing device (20) e.g. staircase or ladder, moveable between two positions using a displaceable bearing (50). The climbing device partially covers the entrance in one of the positions and lies with its upper end on the bed plate in the other position. The climbing device permits the climbing up and/or climbing down of persons to and/or from the entrance. The bearing has a displacing device that runs parallel to the side wall and orthogonal to the plate.

System und Verfahren zur Bedienung einer Vielzahl von Servicepositionen

System (10) zur Bedienung einer Vielzahl von Servicepositionen (15), die einer Vielzahl von Einrichtungselementen (20) zugewiesen sind, mit:- einer Vielzahl von Serviceeinheiten (25), wobei die Anzahl der Serviceeinheiten (25) die Anzahl der zu bedienenden Servicepositionen (15) überschreitet, und- einer Steuereinheit (30), wobei die Steuereinheit (30) ausgestaltet ist, jeweils eine Steuerinformation einschließlich einer Identifikation hinsichtlich eines Einrichtungselements (20) zu empfangen und auf Basis der Identifikation eine vorbestimmte Serviceeinheit (25) zu steuern,wobei die Identifikation die Angabe einer absoluten oder relativen Position des Einrichtungselements (20) beinhaltet und die Steuereinheit (30) ausgestaltet ist, aus der absoluten oder relativen Position eine Zuweisung zu der wenigstens einen Serviceeinheit (25) abzuleiten,ferner mit einer mit dem Einrichtungselement (20) verknüpften Bedieneinheit (85), wobei die Bedieneinheit (85) ausgestaltet ist, Signale zur Bestimmung ...

Luftschwenkduese fuer Belueftungsventilator fuer Flugzeug- und Fahrzeug-Passagiere

Travel environment control

A system and method for controlling the travel environment for a passenger on an aircraft utilises data obtained from an existing source of stored data and information received from one or more sensor inputs. The stored data includes information on the passengers itinerary. The one or more sensor inputs provide information on the physiological state of the passenger and/or environmental conditions in the vicinity of the passenger. One or more outputs are provided to control the passengers travel environment based on the passenger data and the one or more sensor inputs. A system and method of dynamic in-flight event scheduling is also described, in which a dynamic event schedule is generated based on the retrieved data, the dynamic event schedule including at least one event associated with at least one action output.

Luminous means, cable harness and interior trim element

A stowable table for an aircraft passenger seat unit

Improvements in or relating to aircraft

... 730,969. Freight carrying aircraft. BLACKBURN & GENERAL AIRCRAFT, Ltd., BRUMBY, H., and WARBURTON, D. S. May 19, 1953 [May 21, 1952], No. 12877/52. Class 4. An aircraft has a freight compartment along the side walls of which are channel-section supporting rails intermediate the floor and ceiling, whereby bulky articles such as motor cars on special carriers, goods containers, cattle pens, sets of passenger seats or floor units all terminating in rollers may be raised to the level of the rails and slide therealong to be carried thereby. A deep fuselage 3, having a tail-carrying boom 4, has channel section supporting rails 16, 17 secured to the inside walls thereof, the open sides of the channels facing inwards to accommodate rollers mounted on the supporting arms 46 of loading platforms 43 or the like. A lift is located in the door end of the fuselage and comprises rails 21, 22, matching the rails 16, 17, respectively raised and lowered by screw jacks so that a platform 43 may be loaded ...

TABLE-LIKE SUPPORT INSTALLATION

Locking device

CRASHWORTHY COCKPIT ARRANGEMENT

A crashworthy helicopter cockpit having a pyrotechnic system actuated by a stroking pilot seat for repositioning the upper portion of the cyclic control stick upon a severe or crash landing that is independent of aircraft electric and hydraulic systems.

A pair of passenger accommodation cubicles

A connecting device

A connecting device is provided in aircraft for attaching of built-in elements such as galley and lavatory walls, storage cabinets and the like to structural parts of the airframe. The connecting device meets the special requirements of aircraft construction, reliably prevents corrosion at the structure and at the same time allows for an adjustment for balancing tolerances. The connecting device is constructed such that the individual elements of the connecting device can be combined to each other, that the built-in elements can be adjusted in their position regarding the x-, y-, and z-directions, that as desired space can be provided above the floor level and that the connection bores of the structure are provided with sealing rings.

A CONNECTING DEVICE

Tamper detectable container

A container 1 comprises a receptacle 2 with an opening 3. In one embodiment, the container 1 is suitable for use on a commercial passenger aircraft as a life vest stowage device. A Radio-Frequency Identification (RFID) tag 24 is mounted on a tag holder 16 comprising first and second parts 17, 18 that are separable from one another. The container 1 has a closure flap 5 moveable to cover an opening 3 of the container 1 along with first and second tag receiving holes 12, 13. The closure flap 5 has a sling 14 in which the RFID tag 24 and tag holder 16 can be located with the first part 17 of the tag holder 16 inserted in the first tag receiving hole 12 and the second part 18 of the tag holder 16 inserted in the second tag receiving hole 13. Moving the closure flap 5 to the unfolded configuration moves the sling 14 away from the first and second tag receiving holes 12, 13 and causes a frangible part 28 of the RFID tag 24 to break and the RFID tag 24 to cease functioning.

An aircraft instrumentation system

Cross bin illumination system

An illumination system for an aircraft passenger cabin has a first illumination source (58) positioned between a ceiling structure and a first row of stowage bins. A first light direction assembly (62,66) is positioned between the ceiling structure and the first row of stowage bins. The first light direction assembly is used to direct emitted light from the first illumination source onto a face of a luggage bin of a second row of stowage bins. A second light direction assembly (68) is also positioned between the ceiling structure and the first row of stowage bins and is used to direct emitted light from the first illumination source into a passenger cabin. A second illumination source (60) is positioned between the ceiling structure and the first row of stowage bins to illuminate the ceiling structure.

Control module unit for services systems for a vehicle

An accommodation unit for a passenger vehicle

A vehicle seat arrangement

A seating arrangement 200 comprising a pair of seats 210 disposed alongside and secured to each other wherein each seat comprises a backrest portion 222, and a seat pan portion 224. The pair of seats face at an acute angle to each other; the backrest portions of the respective seats are nearest the vertex of the acute angle than the seat pan portions. The seat pan portion of each seat may be separated from each other and an armrest located between the seat pan portions. A utility surface 216 may be located between the seat pan portions. The utility surface may be supported by a base structure; movable between a raised position and a lowered position. The utility surface may provide an armrest when in the raised position. The utility surface, when in the lowered position, may define a continuous support surface with the seat pans of each adjacent seat. A secondary seat pan may be provided, positioned intermediate of and spanning between the seat pans of the two seats when in a first position ...

Switch mechanism for an electrically adjusted screen mount

An electrically adjustable screen mount, such as one found in the seat of a motor vehicle for supporting a display screen, comprises a control mechanism operable by a user to select between a first automatic operation for stowing and deployment of the display screen, and a second, user adjustable operation for adjustment of the deployed position of the display screen, wherein the first automatic operation effects movement between the stowed position and the last used deployment position. Adjustment back and forth of the of the screen may be accompanied by a movement upward or downward, with an upward movement when the top of the screen tilts away from the user, and downward movement when the top of the screen tilts towards the user. This can compensate for tilting of the surface to which the screen mount is attached, such as a seat-back. A switch (figures 7A-7D) for controlling the various operations is also disclosed.

A soft detachable interior trim component for an aircraft cabin

A soft interior trim component for an aircraft cabin, for example a headboard cover (10, figure 1) for a lie-flat seat, has a soft layer of foam 24 the front of which is covered by a cover (40, figure 2). The component is attached to a surface to be covered by rear attachment means 26, 28-32 which enable the component to be easily removed for replacement and/or cleaning. The attachments may comprise a double-sided adhesive tape 26 and a series of clips or plugs such as fir-tree fasteners 28-32 which can be inserted into respective female connector portions in the surface to be covered. The foam may comprise a closed cell fluoropolymer, and said cover may also be used on bulkheads, dividers, toilet or galley walls, and sidewall panels.

Passenger accomodation cabin for a vehicle

An aircraft suite

Lighting module for aircraft galley with variable brightness and colour

An aircraft lighting module 1, particularly for use in aircraft galleys, has at least one light source, for example LEDs 3a, 3b, 3c, 3d, a controller 6, and a control panel, for example a touch sensitive surface 5a, 5b. A command from the control panel, such as a discrete command or a variable command, causes a change in the brightness level and the colour of emitted light. Also disclosed is an aircraft lighting module, particularly for use at aircraft passenger seats, where the brightness level is automatically controlled, for example according to the time of day. A data port 8 and transceiver 9 may be provided to allow the module to transmit and receive data from other modules or a separate control panel. The module may, at full brightness, emit white light at 2500 lux or more, which may reduce tiredness or jet-lag in passengers.

Security apparatus for aircraft

In an aircraft, a cubicle 1 is provided near the front of the aircraft interior, from within which a guard can control access to the aircraft flight deck 7. One or more further cubicles can be provided elsewhere in the aircraft. ...

Dispenser for Volatile Materials

Aircraft overhead sign

Aircraft-cabin-trim panel, seat monument, and associated method

An aircraft cabin trim panel 10 has: a structural foam body 12, with opposing first and second surfaces and a first stiffness; plastic sheeting 14 covering the majority of the first surface, having a thickness less than 1.5mm. The majority of the second surface is exposed and has a number of elongate recesses, each with an elongate aluminium reinforcement 16, stiffer that the foam body, located in it. Each reinforcement has major surfaces perpendicular to the second surface, and a curved minor surface imparting non-flatness on the foam body when adhered to it. The first surface has an area of at least 0.18 m2 and a thickness between 6-12mm. The panel may be used in aircraft seat monuments. The panel may be formed by taking a foam body of the required dimensions; machining the recesses in the second surface; securing the plastics sheeting to the first surface; cutting reinforcements from an aluminium sheet and adhering them into the recesses. The location of each recess may be determined ...

DEVICE TO THE SUPPLY OF OXYGEN FOR THE PASSENGERS OF AN AIRPLANE AND A PRINTING MODULATOR FOR SUCH A DEVICE

AIRPLANE SEAT

AIRCRAFT CAB DEVICE CONTROL

AIRPLANE DOOR WITH OVER WIDTH

AIRPLANE INTERIOR ARRANGEMENT

ATTACHMENT SYSTEM FOR THE FAST SOLVABLE ATTACHMENT OF INTERIOR COMPONENTS IN THE CAB OF AN AIRCRAFT

BEFESTIGUNGSEINRICHTUNG

The invention relates to a device (1) for fixing fittings (2), in particular wall or floor elements (3) in airplanes, to a structure (4) such that no vibrations are generated, comprising a fixing element (5) which is designed on one end (6) for fixing to the structure (4) and on the opposite end for receiving the fittings (2). The opposite end (7) of the fixing element (5) is movably mounted in a spacer sleeve (21) which can be connected to the fittings (2) to be received and which comprises an elongated hole-shaped cross-section, and said opposite end is designed for fixing to the fittings. At least one damping element (8) is provided for arranging between the structure (4) and the fittings (2). The spacer sleeve (21) has an elongated hole-shaped cross-section, and the one end (6) of the fixing element (5) is formed by a stand (6') or can be connected to a stand (6'), said stand (6') being designed for movably mounting in a rail section (14) that lies on the structure (4).

ARRANGEMENT, CONSISTING OF AN AIR LINE AND A TENDER UNIT

VEHICLE INTERIOR FITTINGS.

AIRPLANE

TRANSITION STAIRS BETWEEN AN UPPER ONE AND A LOWER LEVEL OF AN AIRPLANE, AND THEREBY EQUIPPED AIRPLANE

FOLDING CONTAINER MECHANISM

CONTAINER FOR EMERGENCY OXYGEN MASKS

ARRANGEMENT FOR SUPPLYING PASSENGERS IN A PASSENGER CAB, IN PARTICULAR IN AN AIRPLANE

Cabin module

A cabin module (20) deployable inside a vehicle so as to form at least a portion of an interior of the vehicle. The cabin module comprises a main body (22) and a plurality of external walls (24, 26). One or more of the plurality of external walls are moveable with respect to the main body (22). The module has a closed configuration for storage outside the vehicle, in which the plurality of external walls define at least a part of a first form factor of the module. The module has an open configuration for operational deployment in the vehicle, in which the plurality of external walls (24, 26) define at least a part of a second form factor of the module. The cabin module is reversibly changeable between the closed configuration and the open configuration by movement of the one or more external walls (24, 26). The first form factor is different from the second form factor.

STRETCHER LOADING ASSEMBLY

Method and apparatus for reducing heat release and smoke density

A seating system and a passenger accomodation unit for a vehicle

Control module unit for services systems for a vehicle

CONTROL MODULE UNIT FOR SERVICES SYSTEMS FOR A A cabin service system may include a control module unit 12, a pair of power rails 28, the power rails 28 being configured to provide mechanical attachment and electrical power to the control module unit 12, and a plurality of cabin services 16, wherein the control module is communicatively coupled to the plurality of cabin services 16 to provide control of the plurality of cabin services 16. The control module unit 12 may include a plurality of communication ports 24, and a plurality of relays 34 coupled to at least one communication port of the plurality of communication ports 24, wherein each communication port of the plurality of communication ports 24 corresponds to at least one cabin service of the plurality of cabin services 16, and wherein each relay of the plurality of relays 34 provides discrete control of an associated cabin service of the plurality of cabin services 16. 10 14 CABIN 716a9 CONTROL SERVICE J12 CABIN r16b2 18 12 SERVICE ...

Seating array for an aircraft cabin

A seating array for an aircraft cabin comprises a plurality of passenger modules, wherein each module (2): is defined by first and second end walls extending substantially transversely to a longitudinal centreline of the aircraft cabin, the end walls connected by at least one sidewall which defines an entrance to the module; includes a seat assembly and an ottoman (8), the ottoman (8) being spaced in a longitudinal direction of the array from the seat assembly (7); has at least one door assembly moveable from a stowed position in which the entrance is unobstructed by the door assembly to a deployed position in which the entrance is at least partially obstructed by the door assembly; and is wider adjacent the seat assembly than adjacent the ottoman (8). The plurality of passenger modules is divided into at least two columns of modules, each column including at least two modules, the at least two columns being separated by an aisle (3). At least one pair of substantially transversely adjacent ...

Demountable comfort modules for passenger aircraft

Floor rising cabin table

A SEATING SYSTEM AND A PASSENGER ACCOMODATION UNIT FOR A VEHICLE

A passenger seat assembly for a vehicle, particularly an aircraft, which is adapted to provide self-contained, individual seating and sleeping accommodation for a passenger, said seat assembly comprising: supporting structure (42) for supporting said assembly off the floor of a vehicle; one or more movable passenger-bearing, structural components (71,72); and means for connecting said movable, structural components to said structure such that said components can be selectively moved between a seat configuration, in which a plurality of passenger-bearing surfaces on said one or more structural, movable components (71,71) or said supporting structure form a seat for the passenger, and a bed configuration, in which a plurality of said bearing surfaces (47,48,67,74,76) are disposed substantially coplanarly and substantially contiguously to form a bed for the passenger; characterised in that at least one of said movable components (72) is double- sided, comprising first and second opposite sides ...

FUSELAGE SEGMENT AND METHOD FOR MANUFACTURING THE FUSELAGE SEGEMENT

Disclosed is a segment (2) of an aircraft fuselage, comprising an outer skin (6) and an inner skin (4) which are disposed at a distance from each other using a core (8). Ducts (20, 22) for installing systems are integrated into the core (8). A method for producing such a fuselage segment (2) is also disclosed.

AIRCRAFT

A SEATING SYSTEM AND A PASSENGER ACCOMODATION UNIT FOR A VEHICLE

A passenger seat assembly for a vehicle, particularly an aircraft, which is adapted to provide self-contained, individual seating and sleeping accommodation for a passenger, said seat assembly comprising: supporting structure (42) for supporting said assembly off the floor of a vehicle; one or more movable passenger-bearing, structural components (71,72); and means for connecting said movable, structural components to said structure such that said components can be selectively moved between a seat configuration, in which a plurality of passenger-bearing surfaces on said one or more structural, movable components (71,71) or said supporting structure form a seat for the passenger, and a bed configuration, in which a plurality of said bearing surfaces (47,48,67,74,76) are disposed substantially coplanarly and substantially contiguously to form a bed for the passenger; characterised in that at least one of said movable components (72) is double- sided, comprising first and second opposite sides ...

CIRCUIT FOR SUPPLYING OXYGEN TO AIRCRAFT PASSENGERS

... ²²²² Un circuit de fourniture d'oxygène à des passagers d'un aéronef en cas de ²dépressurisation accidentelle de la cabine. Le circuit comprend un régulateur ²de ²pression motorisé adapté pour réguler la pression dans une première ligne en ²aval du ²régulateur de pression, la première ligne étant en communication fluidique ²avec un ²réservoir d'oxygène sous pression pour fournir de l'oxygène à des masques de ²passagers. Le régulateur régule la pression en suivant un signal de consigne ²élaboré ²par une unité électronique de commande en fonction d'un signal de pression ²cabine ²reçu d'un premier capteur de pression et en fonction d'un signal de pression ²régulée ²reçu d'un second capteur de pression disposé dans la première ligne en aval du ²²régulateur de pression.² ...

MEDICAL UNIT FOR AN AIRCRAFT CABIN ASSOCIATED WITH A BERTH

Ce bloc médical est associé à une couchette (2) destinée à recevoir un patient en position allongée, et comporte : une alimentation en eau ; une alimentation électrique ; une zone de stationnement pour au moins un chariot (12) ; au moins un chariot (12) disposé dans la zone de stationnement et comportant des tiroirs dans lesquels se trouve du matériel médical ; et un volet d'accès correspondant à chaque chariot (12), muni de moyens de verrouillage, et permettant l'accès aux tiroirs de celui-ci.

COCKPIT EQUIPPED WITH A LATERAL STICK OPERABLE BY A SINGLE HAND AND SEAT FOR SAID COCKPIT

ILLUMINATED STOWAGE BIN ASSEMBLIES WITHIN VEHICLES

A stowage bin assembly of a vehicle includes one or more interior light-emitting elements that are configured to illuminate a baggage retaining chamber of the stowage bin assembly. The stowage bin assembly is within an interior cabin of the vehicle.

LUMINAIRE AND LUMINAIRE MODULE

In the case of a luminaire (2) for an interior (4) of a vehicle (6), comprising a main body (8) for securing to the vehicle (6), comprising at least one light source (10) secured to the main body (8), at least one of the light sources (10) is a matrix LED (12), wherein the matrix LED (12) comprises at least two mutually independently drivable LED pixels (14), and the LED pixels (14) are integrated on an LED chip. A matrix LED (12) is used as a light source (10) in a luminaire (2). A luminaire module (46), comprising at least one luminaire (2), wherein at least one of the luminaires (2) is a luminaire (2) according to the invention comprising a control input (44), and comprising a transducer (48) connected to the control input (44), contains a control and evaluation unit (49) for driving at least one of the matrix LEDs (12) via the control input (44) depending on the transducer (48).

ADDRESS ALLOCATION TO PSUS, SERVICE ARRANGEMENT AND PASSENGER CABIN

In a method for allocating a respective address (Aa-e) to a plurality of PSUs (20a-e) of a service arrangement (12) for a passenger cabin (4) of an aircraft (2), a start command (40) is transmitted to all PSUs (20a-e), a respective coding value (Pa-e) of a coding parameter (P) is determined at an installation position (22a-e) of the respective PSU (20a-e), a respective waiting time (Wa-e) is determined from the coding value (Pa-e) according to a time rule (42), a response (Ra-e) is transmitted to a head unit (26) on expiry of the respective waiting time (Wa-e) and an address (Aa-e) is allocated to the responding PSU (20a-e) in response to the reception of the response (Ra-e). A service arrangement (12) for a passenger cabin (4) of an aircraft (2), with a coding means (14) extending along an extension line (16) in an installation space (18) for a plurality of PSUs (20a-e) and having different coding values (Pa-e) of a coding parameter (P) at different installation positions (22a-e) for PSUs ...

CASING FOR CONNECTING ELECTRICAL LINES PRINTED ON A FOIL TO A VOLTAGE SUPPLY

A casing for connecting electrical lines printed on a foil to a voltage supply is provided. The casing comprises a space, terminal pads and a block. The casing has an opening between a first wall of the space and a first outer side of the casing. The terminal pads are at least partially arranged on a second outer side of the casing. The block is configured to move between a first position within the space and a second position within the space. The block is configured to press the foil against a second wall of the space when the block is in the first position. The block is configured to establish an electrical connection between the electrical lines printed on the foil and the terminal pads when the block is in the first position. The space is configured to receive the foil through the opening when the block is in the second position.

INTERIOR SPACE MANAGEMENT SYSTEM FOR AN AIRCRAFT, AIRCRAFT HAVING SAID INTERIOR SPACE MANAGEMENT SYSTEM, AND METHOD FOR CONTROLLING SAID INTERIOR SPACE MANAGEMENT SYSTEM

GP 665 CA RT/ND/dk ABSTRACT In passenger aeroplanes, baggage compartments for holding passengers' baggage are usually arranged above the rows of seats. It is the object of the invention to propose an interior space management system which is characterized by improved management of the aeroplane interior. For this purpose, an interior space management system (1) for an aircraft (2) is proposed, the aircraft (2) having a stowage compartment arrangement (6), the stowage compartment arrangement (6) having a plurality of stowage compartment sections (7), each for holding one or more baggage items (8), and having a control unit (16), the control unit (16) being designed to control and/or manage a distribution of interior regions of an interior space (3) of the aircraft (2), and the control unit (16) being designed to control and/or manage an occupancy of the stowage compartment sections (7) on the basis of historical data of the aircraft (2) and/or on the basis of baggage data of the baggage ...

Модуль вертолетный для эвакуации больного особо опасными инфекциями

Полезная модель относится к области медицинской техники, предназначенной для эвакуации больного особо опасными инфекциями при ликвидации эпидемиологических последствий стихийных бедствий, техногенных катастроф и чрезвычайных биолого-социальных ситуаций. Модуль выполнен на базе вертолета Ка-226 и содержит герметично исполненный салон, который выполнен из материала, стойкого к воздействию дезинфекционных средств. Модуль содержит транспортировочный изолирующий бокс и оборудование для дезинфекции изолирующего бокса и защитной одежды личного состава. В качестве оборудования для дезинфекции используют генератор горячего или холодного тумана. Мебель модуля изготовлена из материалов, устойчивых к повреждениям и коррозии, агрессивным дезинфицирующим средствам и химическим препаратам, ультрафиолетовому облучению. Технический результат полезной модели направлен на создание модуля для эвакуации больного особо опасными инфекциями на базе вертолета. 3 з.п. ф-лы, 1 ил. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 176 563 U1 (51) МПК A61G 3/00 (2006.01) A61L 2/07 (2006.01) B64D 11/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК A61G 3/00 (2006.01); A61L 2/07 (2006.01); B64D 11/00 (2006.01) (21)(22) Заявка: 2017126735, 25.07.2017 (24) Дата начала отсчета срока действия патента: Дата регистрации: 23.01.2018 (45) Опубликовано: 23.01.2018 Бюл. № 3 Адрес для переписки: 410005, г. Саратов, ул. Университетская, 46, РосНИПЧИ "Микроб" (73) Патентообладатель(и): Федеральное казенное учреждение здравоохранения "Российский научно-исследовательский противочумный институт "Микроб" Федеральной службы по надзору в сфере защиты прав потребителей и благополучия человека ("РосНИПЧИ "Микроб") (RU) R U 1 7 6 5 6 3 U 1 2406476 C2, 20.12.2010. RU 42023 U1, 20.11.2004. US 6691952 B2, 17.02.2004. (54) МОДУЛЬ ВЕРТОЛЕТНЫЙ ДЛЯ ЭВАКУАЦИИ БОЛЬНОГО ОСОБО ОПАСНЫМИ ИНФЕКЦИЯМИ (57) Реферат: Полезная модель относится к области изолирующего бокса и защитной ...

Transformable luggage storage compartment for an aircraft cabin

A storage compartment is provided for a transportation means, for mounting in an overhead region. The storage compartment includes, but is not limited to a universal housing module and a transformable container module. Various container modules, in particular fixed bins and pivot bins, can be installed in the universal housing module without this requiring any alteration of the housing module. The transformable container module can be converted within the housing module from a state as a fixed container to a state as a movable chute.

Vehicle Seating Apparatus

The invention comprises a vehicle and seating arrangement having a central hub with four sides surrounded by four seats. The seats are arranged adjacent a respective side of the hub and facing substantially parallel to the side of the hub. In at least one embodiment, the arrangement provides access for each passenger to the aisle.

Modular display assembly

Described are display assemblies having a display coupled to a passenger seat back, a video shroud coupled to the passenger seat back and with an inner opening positioned adjacent the display, wherein a gap is positioned between an outer edge of the display and an edge of the inner opening, and an adaptor having a lip and coupled to the video shroud, wherein the lip is positioned adjacent the gap. A portion of the lip may surround at least the outer edge of the display and/or may overlap a portion of the video shroud.

Access control method for certain user targeted base station, base station apparatus and mobile communication management apparatus

In a mobile communication system including Home eNBs, information on mobile stations permitted to access each Home eNB are registered, and the permitted mobile stations are connected to the Home eNB at substantially the same time as the registration of the access permission. In order to control access to a user targeted base station, the information on mobile stations permitted to access the user targeted base station is supplied to the user targeted base station. The information on the mobile stations is transmitted to a mobile communication management apparatus. The mobile station registration is stored in the mobile communication management apparatus in association with the user targeted base station. When the mobile station has entered a location registration area covering the user targeted base station or exists in the location registration area, the mobile communication management apparatus transmits connection information for the user targeted base station to the mobile station.

Adapter and method for installing monuments

A tie-down adapter for attaching a monument, such as an aircraft monument, to a floor structure, such as an aircraft cargo compartment floor. The tie-down adapter includes a base and a stud protruding from the base. The base includes a plurality of fastener through holes configured to align with an existing threaded hole pattern in the cargo compartment floor. The stud is configured to penetrate a mount opening of an attachment bracket on an aircraft monument to be attached. The stud has a threaded shaft configured to receive a fastener for fixing the tie-down adapter to the monument attachment bracket. The tie-down adapter can be provided in a system, and used in a method for mounting aircraft monuments to a cargo compartment floor.

Passenger service unit, passenger service channel and means of transport

The invention relates in particular to a passenger service unit 1 for aircraft cabins. The passenger service unit 1 comprises a plurality of service functions implemented on the basis of functional electronic units. The functional electronic units are accommodated without cabling on a common circuit board 3.

Ceiling panel having curtain rail in a transport cabin

A ceiling panel is configured for attaching a curtain in a cabin of a transportation device with an attachment unit, a mounting unit, and a curtain attachment unit. The ceiling panel is configured to integrate the attachment unit, the attachment unit is configured to attach the mounting unit to the ceiling panel, the mounting unit is configured to attach the curtain attachment unit, and the curtain attachment unit is configured to support the curtain.

Convertible monuments

A monument is provided for a cabin of transportation, for example a lavatory monument, a kitchen or galley monument or a storage monument to be fitted in an aircraft, in a helicopter, in a ship or boat, in a train or in a caravan or trailer. A mounting system is also provided with one or several monuments and transportation with a monument installed therein. The monument for the cabin of the transportation includes, but is not limited to a flexible attachment element for attaching the monument to the cabin of the transportation means. The flexible attachment element is designed in such a manner that attachment of the monument can take place in a region of relative positions of the monument relative to the cabin of the transportation.

Announcement information presentation system, announcement information presentation apparatus, and announcement information presentation method

An announcement information presentation is provided that apparatus includes a reception part, a decision part and a display part. The reception part is configured to receive an operational status information from an operating system of a movable vehicle. The operating system is configured to store the operational status of the movable vehicle. The decision part is configured to decide which announcement information to be presented to a crew member based on the operational status information received by the reception part. The display part is configured to present to the crew member the announcement information decided by the decision part.

Passenger seat assembly

Described are passenger seat assemblies having at least one seat back support and at least one seat pan coupled to the at least one seat back support. The passenger seat assemblies may also include at least one pair of armrests coupled to the at least one seat back support, a seat support structure having at least one seat pan mounting surface and a framework, wherein the at least one seat pan is coupled to the at least one seat pan mounting surface, and/or at least one headrest pivotally coupled to the at least one seat back support with at least one pair of extensions coupled to the at least one headrest or the at least one seat back support.

Method and device for presenting information by means of an autostereoscopic 3d display in a passenger cabin of an aircraft or spacecraft

A method for presenting information by means of an autostereoscopic 3D-display in a passenger cabin of an aircraft or spacecraft, comprising the following steps: provision of the autostereoscopic 3D-display in a predetermined portion of the passenger cabin; provision of a first item of information by means of the autostereoscopic 3D-display such that this information can be detected from a first seat in the passenger cabin; simultaneous provision of a second item of information, which is different from the first item of information, by the autostereoscopic 3D-display such that this second item of information can be detected from a second seat in the passenger cabin. A display device for implementing a method of this type. A passenger cabin for an aircraft or spacecraft comprises a display device of this type. An aircraft or spacecraft having a display device of this type or having a passenger cabin of this type.

Oxygen module

The present disclosure provides a flexible oxygen supply system which can easily be adapted to different seat layouts and which is significantly improved with regard to test and maintenance possibilities. An oxygen module according to the present disclosure generally comprises an oxygen source, a mask and a tube between the oxygen source and a mask. The oxygen module further comprises fastening elements for fastening in a supply duct of an aircraft, and a locking element by means of which the cover of the oxygen module can be locked.

Systems and methods for a virtual terrain display

Embodiments of the present invention provide improved systems and methods for providing a virtual terrain display. In one embodiment, a method comprises identifying a location within an enclosure. The location is referenced against an external environment containing the enclosure. The method also comprises identifying a portion of a structure of the enclosure. The portion of the structure exists between the location and the external environment and blocks a view of the external environment. The method also comprises generating a display depicting a view of the external environment from the location; and applying a translucent structure representation to the display. The structure representation is a visual depiction of the portion of the structure and appearing in front of the depicted view without blocking the depicted view of the external environment.

Passenger service unit

The invention relates to a passenger service unit, in particular for an aircraft passenger cabin, comprising at least one passenger service panel with fastening elements for fastening the panel to an interior component or framework of the aircraft, at least one electric component for passenger entertainment or information mechanically attached to the passenger service panel, at least one electrical connecting terminal for electrical connection of said at least one electric component and an electrical connection for supplying electrical energy and/or transmitting information to said at least one electric component. A further aspect of the invention is a method of producing a passenger service panel. Furthermore the invention relates to method for providing information or entertainment to passengers of an aircraft. A further aspect of the invention is an aircraft, in particular an aircraft passenger cabin, comprising a passenger service unit.

Display device adjustment system, and adjustment method

A system controller comprises a normal mode and a maintenance mode as its control modes, and switches the mode so that electronic control buttons are assigned the functions of calling a crew member, onboard communications, switching seat lighting on or off at each seat, etc., in normal mode, and the picture quality and brightness of a large monitor are adjusted in maintenance mode.

Vehicle galley

A modular integrated galley in a passenger vehicle, including a mounting rack in the form of a vertical wall including upper, middle and lower storage areas, at least one storage slot extending laterally between the middle and lower storage areas for storing a work surface therein, and a latch for ejecting the work surface at least partially from the slot into a position for being further extended into a fully deployed position by a user. An elongate hinge that extends vertically along a mounted edge of the doors and is adapted for allowing the door to move 180 degrees of travel between its closed and open positions is also disclosed.

HIGH PRIVACY PASSENGER AIRCRAFT CABIN ARRANGEMENT

An aircraft that includes a cabin that has a floor, side walls, a ceiling and an interior, a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough, a first door positioned fore of the first class section, an economy class section positioned in the interior and aft of the first class section, and a longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section. An economy class passenger that enters through the first door travels down the second aisle to enter the economy class section and never enters the first class section. 1. An aircraft comprising:a cabin having a floor, side walls, a ceiling and an interior,a first class section positioned in the interior that includes a longitudinally extending first aisle extending therethrough,a first door positioned fore of the first class section,an economy class section positioned in the interior, wherein at least a portion of the economy class section is positioned aft of the first class section, anda longitudinally extending second aisle that extends parallel to the first aisle and that does not extend through the first class section,wherein an economy class passenger that enters through the first door travels down the second aisle to enter the economy class section.2. The aircraft of further comprising a longitudinally extending wall that separates the second aisle from the first class section.3. The aircraft of wherein the longitudinally extending wall extends from the floor to the ceiling.4. The aircraft of wherein the longitudinally extending wall includes an offset portion.5. The aircraft of wherein the longitudinally extending wall includes a vertically extending floor portion claim 4 , the offset portion claim 4 , and a vertically extending ceiling portion.6. The aircraft of wherein the ceiling comprises an oxygen mask compartment claim 5 , wherein the floor portion of the ...

SUPPLY SYSTEM FOR SUPPLYING PASSENGERS IN A PASSENGER COMPARTMENT OF A VEHICLE

A supply system for supplying passengers in a passenger compartment of a vehicle, in particular an aircraft, includes a supply line and a number of supply modules which, for supplying the passengers, are connectable to the supply line. The supply modules are displaceable relative to one another along the supply line, the supply line having one or a plurality of supply openings by which the connection between the supply line and the supply modules can be established, each supply module furthermore being assigned at least one screen which is arranged in such a manner on the service supply line that it is displaceable along the supply line and can cover a part of the one supply opening or of the plurality of supply openings which is not used for the connection of a supply module to the supply line. 2. Supply system according to claim 1 ,each screen being displaceable relative to at least one adjacent supply module.3. Supply system according to claim 1 ,each screen being arranged in a manner at least sectionally overlapping with at least one adjacent supply module.4. Supply system according to claim 1 ,each supply module having a projection which is designed to limit the displacement of at least one adjacent screen along the supply line.5. Supply system according to claim 1 ,which has at least one guide arrangement for guiding the supply modules along the supply line.6. Supply system according to claim 1 ,the supply line comprising a hollow profile for conducting air, which profile has a circumferential surface with air outlet openings, and each supply module having at least one connecting opening for fluidic connection to at least one air outlet opening of the hollow profile.7. Supply system according to claim 6 ,the screens being of air-sealing design.8. Supply system according to claim 1 ,which furthermore has a cover extending in a longitudinal direction, with an outer surface facing away from the passenger compartment and with an inner surface facing the passenger ...

LUGGAGE STORAGE COMPARTMENT FOR AN AIRCRAFT, AND AIRCRAFT COMPRISING THE LUGGAGE STORAGE COMPARTMENT

Luggage storage compartment for an aircraft, comprising a housing and a luggage container being mounted pivotably in the housing about a pivot axis A, and being transferrable with a first pivoting motion S from a closed position G into an open position Ö and the luggage storage compartment being opened, and being transferrable with a second pivoting motion S from the open position Ö into the closed position G and the luggage storage compartment being closed, the luggage storage compartment having a pivoting apparatus, comprising a cable winding device with a winding roll and with a winding medium, the pivoting apparatus comprising a drive device with a drive motor for driving the winding roll, an axis of rotation D of the winding roll running in the same direction as and/or parallel to the pivot axis A of the luggage container. 1. A luggage storage compartment for an aircraft ,comprising a housing and a luggage container, the luggage container being mounted pivotably in the housing about a pivot axis (A),{'b': 1', '2, 'the luggage container being transferrable with a first pivoting motion (S) from a closed position (G) into an open position (Ö) and the luggage storage compartment being opened, and the luggage container being transferrable with a second pivoting motion (S) from the open position (Ö) into the closed position (G) and the luggage storage compartment being closed,'}{'b': 1', '2, 'the luggage storage compartment having a pivoting apparatus, which is designed to transfer the luggage container into the open or closed position (Ö; G) by execution of the first or second pivoting motion (S; S),'}the pivoting apparatus comprising a cable winding device with a winding roll and with a winding medium,the pivoting apparatus comprising a drive device with a drive motor for driving the winding roll,wherein axis of rotation (D) of the winding roll runs in the same direction as and/or parallel to the pivot axis (A) of the luggage container.2. The luggage storage ...

BAGGAGE HOLDER FOR AN AIRCRAFT AND AIRCRAFT HAVING THE BAGGAGE HOLDER

Baggage compartment for an aircraft, wherein the baggage compartment comprises a housing and a baggage holder , wherein the baggage holder is swivel-mounted about a swivel axis A in the housing , wherein, the swivel axis A intersects, in its longitudinal extent, a holder side wall of the baggage holder and/or a housing side wall of the housing , wherein the baggage holder 3 can be moved from a closed position G into an open position Ö with a first swivel movement S and the baggage compartment is opened and wherein the baggage holder can be moved from the open position Ö into the closed position G with a second swivel movement S and the baggage compartment is closed, wherein the baggage compartment comprises a drive device having at least one drive motor , wherein the drive device is designed to drive the baggage holder during the first and/or second swivel movement S; S and to open or close the baggage compartment , wherein the drive device is connected to the holder side wall on one side and to the housing side wall on the other side. 1. A baggage compartment for an aircraft , comprising a housing and a baggage holder , wherein the baggage holder is swivel-mounted about a swivel axis (A) in the housing ,wherein, the swivel axis (A) intersects, in its imaginary longitudinal extent, a holder side wall of the baggage holder and/or a housing side wall of the housing,{'b': 1', '2, 'wherein the baggage holder can be moved from a closed position (G) into an open position (Ö) with a first swivel movement (S) and the baggage compartment is opened and wherein the baggage holder can be moved from the open position (Ö) into the closed position (G) with a second swivel movement (S) and the baggage compartment is closed,'}wherein the baggage compartment comprises a drive device having at least one drive motor,{'b': 1', '2, 'wherein the drive device is designed to drive the baggage holder during the first and/or second swivel movement (S; S) and to open or close the baggage ...

BAGGAGE COMPARTMENT FOR AN AIRCRAFT AND AIRCRAFT HAVING THE BAGGAGE COMPARTMENT

Baggage compartment for an aircraft, wherein the baggage compartment comprises a housing and a baggage holder wherein the baggage holder is swivel-mounted in the housing wherein the baggage holder can be moved from a closed position G into an open position Ö with a first swivel movement S and the baggage compartment is opened and wherein the baggage holder can be moved from the open position Ö into the closed position G with a second swivel movement S and the baggage compartment is closed, wherein the baggage compartment exhibits a swivelling device which is designed to move the baggage holder into the open or closed position Ö; G by performing the first or second swivel movement S S wherein the swivelling device comprises a cable winch mechanism having a winding roller and a drive mechanism having a drive motor wherein the drive motor is designed as an external rotor motor wherein a rotor shaft of the external rotor motor is disposed coaxially to the winding roller 1. A baggage compartment for an aircraft ,wherein the baggage compartment comprises a housing and a baggage holder, wherein the baggage holder is swivel-mounted in the housing,{'b': 1', '1', '2, 'wherein the baggage holder can be moved from a closed position (G) into an open position (Ö) with a first swivel movement (S) and the baggage compartment () is opened and wherein the baggage holder can be moved from the open position (Ö) into the closed position (G) with a second swivel movement (S) and the baggage compartment is closed,'}{'b': 1', '2, 'wherein the baggage compartment exhibits a swivelling device, which is designed to move the baggage holder into the open or closed position (Ö; G) by performing the first or second swivel movement (S; S),'}wherein the swivelling device comprises a cable winch mechanism having a winding roller and a drive mechanism having a drive motor,wherein the drive motor is designed as an external rotor motor and wherein a rotor shaft of the external rotor motor is disposed ...

Tie bar for purposes of connecting equipment fitting of an equipment module, in particular an overhead compartment, to a structure fitting of a fuselage cell structure of an aeronautical vehicle

A tie bar for connecting an equipment fitting of an equipment module to a structure fitting of a fuselage cell structure. At each end the tie bar has a fork head each with a fork head hole for a bolt. The spacing between the fork heads can be continuously adjusted. A captive bushing is utilized for sound and vibration decoupling. The bushings which are a press fit in the fork head holes can no longer fall out during the handling of the tie bars 10 . The dimensions of the bushings made of plastic are adapted to the respective application scenario by a tolerance calculation and guarantee an effective sound and vibration decoupling between the structure fitting and the equipment fitting.

AIRCRAFT NOSE AND NOSE LANDING GEAR BAY STRUCTURE

An aircraft nose structure includes a fuselage, a floor for a pressurized space and a nose landing gear bay arranged under the floor, on the opposite side to the space. The bay includes walls that form a pressure barrier, of which there are two lateral panels mechanically secured to the floor by load-reacting members, an upper panel adjacent to the floor and extending between the lateral panels, and a rear panel extending between the upper panel and the fuselage. 1. An aircraft nose structure comprising:a fuselage;a floor for a pressurized space; anda nose landing gear bay arranged under the floor, on the opposite side to said pressurized space and comprising a plurality of walls forming a pressure barrier,wherein said pressure-barrier walls comprise at least first and second lateral panels mechanically secured to said floor by at least one load-reacting member.2. The aircraft nose structure according to claim 1 , wherein said pressure-barrier walls comprise at least one upper panel adjacent to said floor and extending between said lateral panels.3. The aircraft nose structure according to claim 2 , wherein said floor comprises at least first and second crossmember for reinforcing said upper panel.4. The aircraft nose structure according to claim 3 , wherein said floor comprises claim 3 , between said crossmembers claim 3 , a plurality of load-reacting webs extending between said lateral panels and said fuselage.5. The aircraft nose structure according to claim 4 , wherein each of said plurality of webs comprises a flange secured to one of said lateral panels.6. The aircraft nose structure according to claim 2 , wherein said pressure-barrier walls comprise claim 2 , between said lateral panels claim 2 , a rear panel extending between said upper panel and said fuselage.7. The aircraft nose structure according to claim 3 , wherein said lateral panels comprise a reinforcing upright claim 3 , and wherein said load-reacting member is a component respectively fixed to one ...

BOARDING AID

A computing unit allocates boarding paths, available for boarding a transport unit, in particular an aircraft, to passengers of the transport unit. An associated method allocates boarding paths, available for boarding the transport unit to passengers of the transport unit. A computer program carries out the method, and a directing system directs passengers of the transport unit along boarding paths available for boarding the transport unit. The computing unit is configured to form two or more changeable seat groups from a plurality of seats provided in the transport unit and to allocate the boarding paths, available for boarding the transport unit, to the two or more seat groups formed. 1. Computing unit for allocating boarding paths , available for boarding a means of transport , in particular an aircraft , to passengers of the means of transport , the computing unit being configured to form two or more changeable seat groups from a plurality of seats provided in the means of transport and to allocate the boarding paths , available for boarding the means of transport , to the two or more seat groups formed.2. Computing unit according to claim 1 , the computing unit being configured to allocate in each case exactly one claim 1 , in particular the shortest claim 1 , of the boarding paths to each of the two or more seat groups formed.3. Computing unit according to claim 1 , the computing unit being configured to carry out claim 1 , repeatedly claim 1 , in particular periodically claim 1 , the formation of the two or more seat groups and the allocation of the boarding paths to the two or more seat groups formed.4. Computing unit according to claim 1 , the computing unit being configured to carry out the formation of the two or more seat groups and/or the allocation of the boarding paths to the two or more seat groups formed on the basis of information about the passengers and/or information about the plurality of seats.5. Computing unit according to claim 4 , the ...

Cargo Compartment with Robot, Aircraft, Freight Storage Device

Conventional aircraft offer an inadequate solution for handling freight items. The present invention significantly improves the handling of freight items. Inter alia, for this the cargo compartment of an aircraft is equipped with a robot with at least one robot arm, wherein the robot arm comprises a receiver tool to receive freight items and is arranged displaceably on a ceiling construction of the cargo compartment.

AIRCRAFT RADIO SYSTEM

An aircraft radio system comprising a plurality of radios interconnected by a digital communications network, each radio having a transceiver and a dedicated processor platform, the aircraft radio system being configured to cause the dedicated processor platforms to constitute a virtual processing environment for the aircraft radio system. There is also an aircraft radio system comprising a plurality of discrete radios interconnected by a digital communications network, each radio having a transceiver, a dedicated processor platform and a server configured to support communications over the network using PPPoE, Point to Point Protocol over Ethernet, to provide a common digital interface between an aircraft domain and the radios for plural types of communication. 1. An aircraft radio system comprising a plurality of radios interconnected by a digital communications network , each radio having a transceiver and a dedicated processor platform , the aircraft radio system being configured to cause the dedicated processor platforms to constitute a virtual processing environment for the aircraft radio system.2. A system according to claim 1 , wherein at least one of the dedicated processor platforms is dedicated to two or more of the transceivers.3. A system according to claim 1 , wherein two or more of the dedicated processor platforms are grouped in a module separate from the transceivers.4. A system according to claim 1 , wherein the network is a deterministic AFDX claim 1 , Avionics Full Duplex Ethernet claim 1 , network claim 1 , or another deterministic network.5. A system according to claim 1 , wherein the network is an Ethernet network.6. A system according to claim 1 , wherein the virtual processing environment complies with CORBA claim 1 , Common Object Request Broker Architecture claim 1 , or Real-Time CORBA.7. A system according to claim 1 , wherein at least one of the radios employs Software Defined Radio techniques.8. A system according to claim 1 , wherein ...

INFLIGHT CATERING APPARATUS

The present invention discloses a tray cart for serving refreshments in an airplane. The tray cart having: a load bearing railing coupled with a fuselage portion of the airplane, the railing stretching from a first end of the airplane to a second end over an aisle portion of the airplane; and a trolley for carrying the refreshments, the trolley being suspended from the railing by means of one or more suspension wires, the trolley being slidable over the railing by means of one or more geared wheels. The trolley is suspended to a predetermined length above a floor of the aisle portion of the airplane, the suspension length permitting removal of the refreshments placed in the trolley by an attendant without having to bend down. 1. A tray cart for serving refreshments in an airplane , the tray cart comprising:a. a load bearing railing coupled with a fuselage portion of the airplane, the railing stretching from a first end of the airplane to a second end over an aisle portion of the airplane; andb. a trolley for carrying the refreshments, the trolley being suspended from the railing by means of one or more suspension wires, the trolley being slidable over the railing by means of one or more geared wheels.2. The tray cart as claimed in wherein the trolley is suspended to a predetermined distance above a floor of the aisle portion of the airplane claim 1 , the suspension length permitting removal of the refreshments placed in the trolley by an attendant without having to bend down.3. The tray cart as claimed in wherein the trolley is slidable over the railing from the first end of the airplane to the second end and from the second end of the airplane to the first end.4. The tray cart as claimed in wherein the trolley comprises:a. at least one locking means for locking the trolley in a desired position on the railing; andb. a releasing means for releasing the trolley from the locked position.5. The tray cart as claimed in further comprising a motor and gear system for ...

PIVOT BIN ASSEMBLY

A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft. The pivot bin assembly includes an upper housing that includes a strongback and first and second side panels, a bucket that cooperates with the upper housing to define a bin interior, a first pivot mechanism operatively associated, with the first side panel and the bucket, and a second pivot mechanism operatively associated, with the second side panel and the bucket. The first and second pivot mechanisms are axially aligned along and are rotatable about a pivot axis such that the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position. 1. A pivot bin assembly configured to receive luggage and be positioned in the interior of an aircraft , the pivot bin assembly comprising:an upper housing that includes a strongback and first and second side panels,a bucket that cooperates with the upper housing to define a bin interior,a first pivot mechanism operatively associated with the first side panel and the bucket, anda second pivot mechanism operatively associated with the second side panel and the bucket, wherein the first and second pivot mechanisms are axially aligned along and rotatable about a pivot axis, and wherein the bucket pivots about the pivot axis with respect to the upper housing between an open position and a closed position.2. The pivot bin assembly of wherein the bucket includes a bottom and first and second opposing sides claim 1 , wherein when the pivot bin assembly receives luggage in the bin interior claim 1 , the luggage is positioned on the bottom of the bucket claim 1 , whereby the bucket is load bearing.3. The pivot bin assembly of wherein the first and second side panels include a bottom edge and the first and second sides of the bucket include a top edge claim 2 , and wherein claim 2 , in the closed position claim 2 , at least a portion of the top edge of the first side of the bucket abuts ...

Portable User Control Device and Method for Vehicle Information Systems

A personal user control device suitable for use in cooperation with information systems, such as vehicle information systems, and methods for manufacturing and using same. The personal user control device provides a user-friendly interface system for interacting with the information system. Unlike conventional control devices, the user interface system includes no dedicated buttons and provides a customizable environment for interacting with the information system. When in communication with the information system, the personal user control device can automatically detect system status information, such as available system functionality, available viewing content, and/or a current system operation mode, of the information system and provides a user interface system that instinctively adapts for use with the information system in light of the detected system status information. The personal user control device thereby provides a versatile and intuitive manner for interacting with the information system.

AIRCRAFT CREW CABIN CHANGING AREA

An aircraft crew cabin rest area that is formed between the aircraft galley and a console, or between any two aircraft monuments, utilizing special folding and extendible doors and specialized locking means. 1. A collapsible changing area for an aircraft galley , comprisinga base wall;first and second doors attached via hinges to the base wall, the hinges permitting the first and second doors to pivot about the hinges from a stowed position against the base wall to an engaged position against an adjacent monument;the first and second doors each comprising an inner panel connected to the base wall and having a projection on an outer surface, and an outer panel having a horizontal slot on an inner surface that receives the projection of the inner panel to establish a sliding connection with the inner panel that allows extension of the outer panel from the inner panel for variable length, the outer panel having a main section and an angled distal skirt that cooperates with the main section and the base wall to enclose the inner panel when the door is rotated against the base wall;a manually operated locking unit for locking the first door to an adjacent monument;whereby an enclosed space is formed between the base wall, the first door, the second door, and the adjacent monument, that is locked using said manually operated locking units from inside the enclosed space.2. The collapsible changing area of claim 1 , further comprising a second locking mechanism outside the enclosed space for releasing the door from the adjacent monument.3. The collapsible changing area of claim 2 , wherein the second locking mechanism is not manually operated but requires a tool.4. The collapsible changing area of wherein the angled section of the outer panel overlaps the adjacent monument to prevent a line of sight into the enclosed space.5. The collapsible changing area of wherein the manually operated locking unit comprises a hook that couples to a complimentary component of the ...

FOLDABLE AIRCRAFT PASSENGER LAP TABLE

A foldable lap table including a first table leaf joined along a first hinge to a second table leaf, the first hinge folding in a first direction, and a third table leaf joined along a second hinge to a fourth table leaf, the second hinge being a linear extension of the first hinge and folding in a second direction opposite the first, wherein the third table leaf is further joined to the first table leaf along a third hinge and the fourth table leaf is further joined to the second table leaf along a fourth hinge such that the respective hinges and leaves are arranged to permit unison movement of the leaves when the lap table is folded and unfolded. 1. A foldable lap table , comprising:a first table leaf joined along a first hinge to a second table leaf, the first hinge folding in a first direction;a third table leaf joined along a second hinge to a fourth table leaf, the second hinge being a linear extension of the first hinge and the second hinge folding in a second direction opposite the first direction;the third table leaf further joined to the first table leaf along a third hinge and the fourth table leaf further joined to the second table leaf along a fourth hinge such that the respective hinges and leaves are arranged to permit unison movement of the leaves when the lap table is folded and unfolded.2. The foldable lap table of claim 1 , wherein the first claim 1 , second claim 1 , third and fourth hinges are living hinges formed by a top layer contiguous among the first claim 1 , second claim 1 , third and fourth table leaves.3. The foldable lap table of wherein the first claim 2 , second claim 2 , third and fourth table leaves each include one or more layers.4. The foldable lap table of claim 3 , wherein the one or more layers include an intermediate layer adhered to the top layer and a bottom layer adhered to the intermediate layer.5. The foldable lap table of claim 3 , wherein the second table leaf is a mirror image of the first table leaf about the first ...

Integrated aircraft galley and appliance operating system

An aircraft galley power and control system is disclosed having a plurality of electrical appliances within a monument, the galley control system including a control panel removed from the electrical appliances that include controls for operating each of the electrical appliances, The galley also includes a galley controller interface for receiving commands from a display screen on the control panel and communicating the commands to the electrical appliances.

Aircraft seat with shared control architecture

The invention essentially concerns an aircraft seat ( 1 ), comprising control units ( 17.2, 22.2, 27 ), at least one node ( 11 - 15 ) to execute a particular action or function, and a display ( 22.1 ) for viewing video data. Said node ( 11 - 15 ) and said display ( 22.1 ) are capable of being actuated by the control units ( 17.2, 22.2, 27 ). A keyboard ( 17.1 ) for transmitting a command signal addressed to the control units ( 17.2, 22.2, 27 ) is connected to said control units ( 17.2, 22.2, 27 ). The control units are shared between the display ( 22.1 ), the key board ( 17.1 ) and the node ( 11 - 15 ).

LUGGAGE STORAGE COMPARTMENT, AIRCRAFT WITH A LUGGAGE STORAGE COMPARTMENT, AND METHOD FOR OPERATING THE LUGGAGE STORAGE COMPARTMENT

The present invention is directed to a luggage storage compartment for an aircraft having high ease of operation. Specifically, the luggage storage compartment comprises a housing and a housing container, with a drive device for moving the housing container between an open position O and a closed position C, with a closure apparatus for locking and unlocking the housing container in the closed position C, and with a control device for controlling the drive device, the control device being designed to actuate the drive device so that said drive device in a relief cycle guides the luggage container first into a relief region R and then into the closed position C, the closure apparatus being lockable or unlockable in a relieved state in the relief cycle. 1. A luggage storage compartmentwith a housing and with a housing container, the housing container being arranged movably in the housing,with a drive device for moving the housing container between an open position (O) and a closed position (C),with a closure apparatus for locking and unlocking the housing container in the closed position (C), andwith a control device, which is designed to actuate the drive device so that said drive device in a closing cycle moves the housing container in a first direction of movement from the open position (O) into the closed position (C) and in an opening cycle moves the housing container in a second direction of movement from the closed position (C) into the open position (O),whereinthe control device is designed to actuate the drive device so that said drive device in a relief cycle guides the luggage container first into a relief region (R) and then into the closed position (C), the closure apparatus being lockable or unlockable in a relieved state in the relief cycle.2. The luggage storage compartment according to claim 1 , wherein that the control device is designed to actuate an unlocking or a locking of the closure apparatus during the relief cycle.3. The luggage storage ...

AIRCRAFT GALLEY MONUMENT STRUCTURE

An improved monument structure combining an integrated construction system with carbon fiber reinforced composites to form an exoskeleton chassis that significantly reduces the build times, manufacturing skill level requirements, post processing activities, and overall weight of a given aircraft monument. 1. A monument for an aircraft , comprising an above work deck subassembly , a below work deck subassembly , and a rear service wall subassembly , wherein each respective subassembly is formed using carbon fiber reinforced composites (CFRC) pre-impregnated panel skins that combine to form a exoskeleton chassis , the subassemblies reinforced with a unidirectional carbon fiber.2. The monument for an aircraft of claim 1 , wherein the monument is a refrigerated centerline galley.3. The monument for an aircraft of claim 2 , wherein the above work deck galley is formed with an array of compartments sized to house galley inserts (GAINs) in the galley.4. The monument for an aircraft of claim 3 , wherein the compartments are formed using a wet lay process where layers of materials are placed in a mold over a wet lay claim 3 , and then the compartments are reinforced with unidirectional carbon fiber reinforcing plies.5. The monument for an aircraft of claim 4 , wherein a finished molded surface opposite a usual orientation of a lay-up of an above work deck subassembly molding provides an upper section of an air ducting for a chiller in the above work deck.6. The monument for an aircraft of claim 1 , further comprising a pair of channels on an upper surface of the above work deck that each receive a ceiling mount for mounting the monument to an upper portion of an airframe of the aircraft.7. The monument for an aircraft of claim 6 , wherein the ceiling mount is formed of a high strength composite and have orthogonal plates claim 6 , including a first orthogonal plate slides within one of the channels on the upper surface of the above work deck.8. The monument for an aircraft ...

AIRCRAFT INTERIOR CONFIGURATION

An aircraft interior configuration includes a first passageway extending along a longitudinal axis of a fuselage of the aircraft and a second passageway extending along the longitudinal axis. A transitional region is disposed between the first passageway and the second passageway. The transitional region extends perpendicularly to the longitudinal axis, between starboard and port sides of the aircraft. The transitional region is configurable from at least a first configuration to at least a second configuration. 1. An interior configuration for an aircraft , comprising:a first passageway extending along a longitudinal axis of a fuselage of the aircraft;a second passageway extending along the longitudinal axis; anda transitional region disposed between the first passageway and the second passageway;wherein the transitional region extends perpendicularly to the longitudinal axis, between first and second sides of the fuselage, the first and second sides being disposed on opposite sides of the longitudinal axis, andwherein the transitional region is configurable from at least a first configuration to at least a second configuration.2. The interior configuration of claim 1 , wherein:the first passageway and the second passageway are offset from one another in a lateral direction, perpendicular to the longitudinal axis, andthe transitional region defines at least a third passageway, disposed at an angle to the longitudinal axis, connecting the first passageway to the second passageway.3. The interior configuration of claim 1 , wherein the transitional region comprises:at least one stowage area disposed adjacent to at least one of the first and second sides of the fuselage;a stowable table disposed within the at least one stowage area,wherein the stowable table may be deployed to extend perpendicularly to the longitudinal axis into the transitional space to establish a conference table.4. The interior configuration of claim 2 , wherein the transitional region comprises:a ...

BAGGAGE COMPARTMENT FOR AN AIRCRAFT AND AIRCRAFT HAVING THE BAGGAGE COMPARTMENT

The present invention is directed to a baggage compartment for an aircraft, wherein the baggage compartment includes a housing and a baggage container wherein the baggage container is mounted in the housing so as to be pivotable about a pivot axis S, wherein, with a pivoting movement, the baggage container is transferable from an open position into a closed position, having a pulling arrangement wherein the pulling arrangement includes at least one pulling means for transferring a pulling force to the baggage container in order to transfer the baggage container from the open position into the closed position, having a drive arrangement wherein the drive arrangement is realized to transfer the pulling force to the pulling means, wherein the drive arrangement has a linear drive with a sliding device 1. A baggage compartment for an aircraft , wherein the baggage compartment includes a housing and a baggage container , wherein the baggage container is mounted in the housing so as to be pivotable about a pivot axis (S) ,wherein, with a pivoting movement, the baggage container is transferable from an open position into a closed position,including a pulling arrangement, wherein the pulling arrangement includes at least one pulling means for transferring a pulling force to the baggage container in order to transfer the baggage container from the open position into the closed position,having a drive arrangement, wherein the drive arrangement is realized to transfer the pulling force to the pulling means,whereinthe drive arrangement has a linear drive with a sliding device which is movable in a first linear direction (R), wherein the at least one pulling means is coupled to the sliding device such that the moving of the sliding device in the first linear direction (R) transfers the pulling force to the at least one pulling means and the baggage container is transferred from the open position into the closed position.2. The baggage compartment according to claim 1 , wherein ...

AIRLINE TROLLEY DRAWER

A drawer for an airline trolley, which has a generally rectangular tray, is closed by a lid. The lid has a flap which is openable, and the drawer has a lock unit with which the flap engages. The lock unit is lockable by a breakable seal. The flap can be hinged about a line extended across the lid at a position forward of the back of the tray. The flap can be connected to the sides of the tray by webs which fold under the flap in its closed position, the webs preventing access to the interior of the tray under the lid. The flap can have a catch at its forward end which engages in a lockable chamber on the front of the drawer, a breakable seal being insertable into the chamber to engage the catch. 1. A drawer for an airline trolley which comprises a substantially rectangular tray with a base , sides , front and back , the sides having means for cooperation with the inside of the trolley for allowing the drawer to slide therein , wherein the drawer includes a lid which closes top of the tray , wherein the lid comprises at least one flap which is openable , and wherein the drawer has a lock unit with which the flap engages , the lock unit being lockable by means of a breakable seal.2. A drawer for an airline trolley according to claim 1 , wherein the flap is hinged about a line extended across the lid at a position forward of the back of the tray.3. A drawer for an airline trolley according to claim 1 , wherein the flap is connected to the sides of the tray by webs which fold under the flap in its closed position claim 1 , the webs preventing access to the interior of the tray under the lid.4. A drawer for an airline trolley according to claim 1 , wherein the flap has a catch at its forward end which engages in the lock unit on the front of the drawer claim 1 , a breakable seal being insertable into the lock unit to engage the catch.5. A drawer for an airline trolley according to claim 4 , wherein the flap has a forward part which folds over onto the front of the tray ...

AUTOMATED STORAGE CABINET FOR TROLLEYS, AND AIRCRAFT INCORPORATING SUCH A CABINET

The present invention relates to an automated storage cabinet for trolleys. It includes a device for automatically handling a single trolley with a handling basket including a vertical plate perpendicular to the waiting area, vertically movable between the floor of the waiting area and any one of the levels of the trolley storage cabinet, and two side flanks, connected to the vertical plate and provided with structure for supporting, on either side, two opposite sides of a trolley in the waiting area and for transferring the supported trolley through an opening of the predetermined compartment. The handling device can include structure for inserting the trolley into or extracting the trolley from the predetermined compartment. 2. Automated cabinet according to claim 1 , characterized in that the vertical plate is mounted on motor means claim 1 , configured in order to confer a vertical movement upon the vertical plate.3. Automated cabinet according to claim 1 , characterized in that the means for transferring the supported trolley through an opening of the predetermined compartment comprise motor means for allowing the transfer of the trolley between a position situated between the side flanks and the predetermined compartment or vice versa.4. Automated cabinet according to claim 3 , characterized in that said motor means are actuated under the control of a control unit cooperating with sensors of displacement of moving parts and of the means of control in particular for selecting a predetermined compartment.5. Automated cabinet according to claim 2 , characterized in that the vertical movement motor means of the vertical plate are duplicated on each side of the vertical plate in such a way that the control unit connected to horizontality sensors of the trolley controls said horizontality.6. Automated cabinet according to claim 4 , characterized in that the means for supporting claim 4 , on either side claim 4 , two opposite sides of a trolley comprise a plurality ...

AIRCRAFT GALLEY CHILLED AIR DISTRIBUTION SYSTEM

A chilled air distribution system for an aircraft galley service cart, comprising a first plenum on an upper surface of the service cart for directing chilled air over said cart. The cart bay door also includes a pair of diverting curved vanes along a vertical surface to divert air from one surface, such as a front door, to an adjacent surface such as a side wall. The side walls may be provided with a pair of rub strips for guiding air to the rear of the cart, where a return plenum vacuums and recirculates the chilled air back to the first plenum. 1. A chilled air distribution system for an aircraft galley service cart , comprising:a service cart having a front door, a pair of side walls, an upper surface, a lower surface, and rear wall;a first plenum on an upper surface for directing chilled air over said cart;a pair of diverting curved vanes along a vertical surface to divert air from one surface to an adjacent surface;a pair of rub strips on the adjacent surface for guiding air to another adjacent surface; anda return plenum for recirculating the chilled air to the first plenum.2. The chilled air distribution system of claim 1 , wherein one of the pair of rub strips is castellated.3. The chilled air distribution system of claim 1 , wherein one of the pair of rub strips is non-castellated.4. The chilled air distribution system of claim 1 , where the pair of diverting curved vanes divert air flowing over the front door of the service cart to the side walls of the service cart.5. The chilled air distribution system of claim 4 , where the pair of diverting curved vanes are spaced apart to allow some air to pass therebetween.6. The chilled air distribution system of claim 1 , wherein the return plenum includes a plurality of spaced apart holes for air to pass through via suction.7. The chilled air distribution system of claim 6 , wherein a number of spaced apart holes is selected to control the flow of air about the service cart. This application claims priority from ...

Aircraft galley chiller system

A modular chiller for an aircraft galley beverage cart compartment is disclosed characterized by a cassette that inserts into the galley compartment above the beverage cart and houses an air return duct, a heat exchanger, a fan, and an air supply outlet. The chiller further includes a control valve for controlling the amount of air passing through the heat exchanger, and an electronic control box for control over the chiller, where the cassette is disposed between the beverage cart and a galley work deck.

AIRCRAFT SYSTEM COMPONENT CARRIER MODULE AND SYSTEM, AND MOUNTING METHOD

An aircraft system component carrier module includes a carrier element which is arc-shaped at least in sections and is configured, when the module is mounted in an aircraft, to extend at least in some sections substantially in the direction of the ribs of an aircraft structure over at least a section of a crown area of an aircraft cabin. The module includes a transverse carrier element which is configured, when the module is mounted in an aircraft, to extend in the crown area of an aircraft cabin substantially perpendicularly to a longitudinal axis of the cabin. The module further includes a structure holder for fastening the module to the aircraft structure, an aircraft system component holder for fastening at least one of the aircraft system components to the module and an attaching device, connected to the transverse carrier element, for attaching an aircraft luggage compartment to the module. 1. Aircraft system component carrier module having:a carrier element which is arc-shaped at least in some sections and is configured, when the aircraft system component carrier module is mounted in an aircraft, to extend at least in some sections substantially in the direction of the ribs of an aircraft structure over at least a section of a crown area of an aircraft cabin,a transverse carrier element which is configured, when the aircraft system component carrier module is mounted in an aircraft, to extend in the crown area of an aircraft cabin substantially perpendicularly to a longitudinal axis of the aircraft cabin,a structure holder for fastening the aircraft system component carrier module to the aircraft structure,an aircraft system component holder for fastening at least one aircraft system component to the aircraft system component carrier module andan attaching device, connected to the transverse carrier element, for attaching an aircraft luggage compartment to the aircraft system component carrier module.2. Aircraft system component carrier module according to ...

Passenger service system with improved air guidance

A passenger service system includes an individual ventilation arrangement and/or a lighting arrangement, wherein at least one air nozzle of the individual ventilation arrangement and/or at least one reading lamp of the lighting arrangement is/are disposed in the region of a service surface of the passenger service system, The service surface of the passenger service system includes a substantially flat portion as well as a buckled portion, which is curved convexly relative to the substantially flat portion and extends along a longitudinal axis (L P ) of the passenger service system.

Passenger aircraft overhead bin system and method

A luggage overhead bin system and method for a passenger cabin of an aircraft. A plurality of stowage compartments approximates an amount of passenger seats. A compartment number is labeled on each stowage compartment, wherein one or more of the compartment numbers are the same as a passenger seat number. An access control system capable of being overridden by a flight crew controls access to each stowage compartment. A locking mechanism locks and unlocks the stowage compartment in response to the access control system. Further included is a credential given to the passenger for enabling the passenger to provide the input to the lock, wherein the input is compared to an access control list within the control panel for the authentication. The above system allows for a fare structure which differentiates for travel fare with and without a carry-on piece of luggage ba d on use of the overhead compartment.

SECURED VESTIBULE TO THE COCKPIT OF AN AIRCRAFT AND AIRCRAFT EQUIPPED WITH SUCH AN ACCESS DOOR

The invention relates to a secure access airlock enabling the communication between several rooms of an aircraft, the secure airlock being installed in an area of the aircraft between a first room and at least one second room, characterized in that it includes two mobile partitions provided in the form of portions of concentric cylinders, each of the partitions being capable of being moved, separately from one another, about a common axis, so as to provide a single opening therebetween which makes it possible to access either of the rooms, the two partitions being capable of moving over two concentric cylinders having different diameters.

Fuselage Segment For A Fuselage Of An Aircraft, Aircraft Fuselage and Aircraft

A fuselage segment for an aircraft fuselage includes a wall with a closed cross section, a first cabin floor, a second cabin floor, and a cargo hold floor. The first cabin floor, the second cabin floor, and the cargo hold floor are vertically spaced apart from each other and connected to the wall. A first passenger region is arranged above the first cabin floor, a second passenger region is arranged above the second cabin floor, and a cargo region is arranged above the cargo hold floor. The cargo region is dimensioned in such a manner that for at least four passenger seats a maximum of 1 mof cargo hold volume is provided. In this manner an existing aircraft fuselage can be designed in a demand-oriented manner so that it can accommodate two or more passenger regions. 1. A fuselage segment for an aircraft fuselage , comprisinga wall with a closed cross section,a first cabin floor,a second cabin floor, anda cargo hold floor,wherein the first cabin floor, the second cabin floor and the cargo hold floor are vertically spaced apart from each other and connected to the wall,wherein a first passenger region is arranged above the first cabin floor, wherein a second passenger region is arranged above the second cabin floor, and wherein at least one cargo region is arranged above the cargo hold floor,{'sup': '3', 'wherein the cargo region is dimensioned in such a manner that for at least four passenger seats a maximum of 1 mof cargo hold volume is provided.'}2. The fuselage segment of claim 1 , wherein the total volume of the cargo region is less than the volume that corresponds to the maximum volume of baggage relating to all passenger seats.3. The fuselage segment of claim 1 , wherein the fuselage segment comprises a diameter ranging from 6 to 6.5 m.4. The fuselage segment of claim 1 , wherein each passenger region comprises a standing height of at least 1.95 m.5. The fuselage segment of claim 1 , wherein the first passenger region is arranged in an upper region of the ...

TEMPORARY LINING

A temporary lining usable as a decorative protective guard on stowage bins on aircraft, such as passenger stowage bins on commercial aircraft. The temporary lining can have a protective layer, and an adhesive layer bonded to the protective layer. The temporary liner can be adhered to the interior of the stowage bins, and can be removed and replaced when damaged. 1. A method for maintaining an aircraft stowage bin comprising:providing a temporary lining having an adhesive surface and a protective surface;adhering the adhesive surface to the interior of the aircraft stowage bin in sections to guard the aircraft stowage bin with the protective surface; andremoving the temporary lining when it is damaged and replacing it with another section of temporary lining, wherein the adhesive permits the temporary lining to be removed by being lifted away from the interior surface of the stowage bin.2. The method of wherein the temporary lining comprises a protective layer claim 1 , having the protective surface claim 1 , and an adhesive layer bonded to the protective layer claim 1 , the adhesive layer having the adhesive surface facing opposite the protective surface.3. The method of wherein the temporary lining further comprises a sacrificial liner claim 2 , temporarily attached to the adhesive surface claim 2 , which can be peeled away from the adhesive surface before adhering the adhesive surface to the interior of the aircraft stowage bin.4. The method of wherein the protective layer is a vinyl film.5. The method of wherein the protective layer is reverse printed to a customer specification.6. The method of wherein a custom color has been compounded into the protective layer.7. The method of wherein an adhesive of the adhesive layer is water-based.8. The method of wherein the temporary lining is adhered to the stowage bin in a plurality of sections claim 1 , whereby a single section can be removed and replaced when repairing localized damage.9. An aircraft comprising:a ...

AIRCRAFT WITH AFT SPLIT-LEVEL MULTI-DECK FUSEALGE

An aircraft capable of carrying passengers and cargo includes a fuselage, having a crown section and a keel, a first passenger cabin, having a first floor, located in a forward portion the fuselage, and a first cargo deck, located below at least a portion of the first passenger cabin. A split level cabin is located in an aft portion of the fuselage, the split level cabin including an upper second cabin having a second floor above the level of the first floor, and a lower third cabin beneath the upper second cabin and having a third floor below the level of the first floor. A second cargo deck is located in the aft portion of the fuselage and beneath at least a portion of the lower third cabin. The crown section has a substantially constant cross-sectional shape fore-to-aft above the first passenger cabin and the split level cabin, and the keel below the second cargo deck is lowered compared to the keel below the first cargo deck. A modified aircraft having a split level aft cabin and lowered keel, and a method for modifying an aircraft in this way are disclosed. 1. An aircraft capable of carrying passengers and cargo , comprising:a fuselage, having a crown section and a keel;a first passenger cabin, having a first floor, located in a forward portion the fuselage;a first cargo deck, located below at least a portion of the first passenger cabin;a split level cabin, located in an aft portion of the fuselage, the split level cabin including an upper second cabin having a second floor above the level of the first floor, and a lower third cabin beneath the upper second cabin and having a third floor below the level of the first floor; anda second cargo deck, located in the aft portion of the fuselage and beneath at least a portion of the lower third cabin;wherein the crown section has a substantially constant cross-sectional shape fore-to-aft above the first passenger cabin and the split level cabin, and the keel below the second cargo deck is lowered compared to the keel ...

Modular cabin segment, cabin for a vehicle and vehicle with a cabin

A modular cabin segment for a vehicle includes a first lateral segment module that accommodates a first toilet arrangement with at least one toilet compartment and a second lateral segment module, wherein in each case an outer lateral face of the first segment module and of the second lateral segment module is designed to adapt in each case to an inner wall of a cabin of the vehicle so as to correspond to the aforesaid. At least one of the modules includes at least one cabin attendant seat that on one side is held on the at least one module so that it can be pivoted on an axis. In this manner very good integration of many different functions in the manner of a construction kit is achieved in order to be able to accommodate a greater number of passenger seats elsewhere within the limited space provided in a cabin.

Floor panel with integrated cable channel

A floor panel for a floor of a passenger cabin of a mobile platform is provided, which comprises a base body with an integrated cable channel and a cover element covering the cable channel. The base body is realized in the form of a sandwich component including two honeycomb structures, between which the cable channel is arranged. The cover element is firmly attached to the base body, thereby creating a self-supporting floor panel. Since the cover element is firmly attached to the base body, the thickness and weight of the base body may be reduced.

Passenger service unit comprising a ventilaton nozzle and a reading light

The invention relates to a passenger service unit comprising a reading light and a ventilation nozzle. The ventilation nozzle is pivotably mounted within a frame wherein the frame is fixed to the passenger service unit. A ring shape-element is arranged circumferentially around the ventilation nozzle and incorporates a plurality of light means providing a light beam to the passenger. The light means are adjusted by an adjustment means which effects a relative movement of the light means to the ring-shaped element. The ring-shaped element is immovable fixed to the frame.

Platform with Adjustable Support Members

A method and apparatus for forming a platform. In one embodiment, the apparatus comprises a set of support members associated with the structure, and a set of adjustment members. An adjustment member in the set of adjustment members is associated with a corresponding support member in the set of support members. The adjustment member is configured to adjust an angle between the corresponding support member and the structure.

PARTITION WALL FOR AN AEROPLANE CABIN, AND AN AEROPLANE

A standardised/modularised partition wall with a basic sandwich structure for purposes of separating a cabin area of an aeroplane. The partition wall has a multiplicity of defined zones for the flexible positioning of holding fixtures for the connection of accessories such as flat screens, baby carriers, newspaper racks, and similar, and which is dimensioned for a maximum population with accessories. 113-. (canceled)14. A partition wall for the separation of cabin areas of an aeroplane , with a sandwich-type planar structure , comprising:a multiplicity of defined zones which enable a flexible positioning of holding fixtures for purposes of connecting accessories, andthe planar structure being dimensioned for a maximum population with accessories.15. The partition wall in accordance with claim 14 , wherein said accessories comprise at least one of flat screens claim 14 , baby carriers and newspaper racks.16. The partition wall in accordance with claim 14 , wherein the zones are arranged on both a front side and a back side of the partition wall.17. The partition wall in accordance with claim 14 , wherein the zones are individualised for purposes of connecting in each case a particular group of accessories.18. The partition wall in accordance with claim 17 , wherein the zones of one particular group are arranged next to one another in a transverse direction.19. The partition wall in accordance with claim 18 , wherein the zones of one particular group are spaced apart from one another and the respective accessories can be connected across a plurality of zones.20. The partition wall in accordance with claim 14 , wherein at least one stiffener with a hollow profile is integrated into the planar structure.21. The partition wall in accordance with claim 20 , wherein the stiffener extends alongside at least some zones.22. The partition wall in accordance with claim 20 , wherein the stiffener is arranged with a section in a region of a foot attachment section for purposes of ...

Aircraft cabin section

An aircraft region having an aisle which leads into an aircraft door region and via which passengers can leave the aircraft or enter the aircraft. The aircraft region further has at least one monument, wherein one of the side walls of the monument is adjacent to the aisle in such a manner that the side wall forms one of the lateral boundaries of the aisle. A niche is formed in a portion of the side wall of the monument facing the aircraft door, which niche is so configured that it is able to accommodate a standing person wholly or at least for the most part. 1. An aircraft region comprising:an aisle leading into an aircraft door region and via which passengers can leave the aircraft or enter the aircraft;at least one monument, wherein one side wall of the monument is adjacent to the aisle in such a manner that the one side wall forms a lateral boundary of the aisle, and a niche is formed in a portion of the side wall of the monument facing the aircraft door, which niche is so configured that it is able to at least largely accommodate a standing person.2. The aircraft region according to claim 1 , wherein dimensions of the niche are such that a person standing in the niche does not obstruct the passengers as they enter or leave the aircraft via the aisle.3. The aircraft region according to claim 1 , wherein the niche is immediately adjacent to the aircraft door.4. The aircraft region according to claim 1 , wherein the monument has a reduced width in the region of the niche.5. The aircraft region according to claim 4 , wherein the monument has an L-shaped footprint which claim 4 , starting from the aircraft door region claim 4 , extends along the aisle into an interior of the aircraft and then bends in order to extend along a longitudinal axis of the aircraft in a direction towards a middle of the aisle.6. The aircraft region according to claim 1 , wherein a width of the monument along the aisle is at least substantially constant.7. The aircraft region according to ...

PSU POD ASSEMBLY AND METHOD FOR USING SAME

A PSU pod assembly that is configured to be positioned in the interior of an aircraft. The PSU pod assembly includes a PSU pod that includes a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior and a panel positioned above and connected to the PSU pod. The PSU pod includes at least first and second reading lights positioned within the pod interior that are configured to shine light below the housing and cabin lights positioned on or in the housing that are configured to shine light above the housing. The panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft. 1. A PSU pod assembly configured to be positioned in the interior of an aircraft , the PSU pod assembly comprising: a housing that includes a top, a bottom and first, second, third and fourth sides that cooperate to define a pod interior,', 'at least first and second reading lights positioned within the pod interior and configured to shine light below the housing, and', 'cabin lights positioned on or in the housing and configured to shine light above the housing,, 'a PSU pod that includes'}a panel positioned above and connected to the PSU pod, wherein the panel includes connectors that are configured to secure the PSU pod assembly to a component within the aircraft.2. The PSU pod assembly of further comprising a lens assembly positioned adjacent the cabin lights.3. The PSU pod assembly of wherein the housing includes at least one vent opening defined therein.4. The PSU pod assembly of wherein the housing includes at least first and second reading light openings defined therein claim 3 , and wherein the first and second reading lights are aligned with and configured to shine light through the first and second reading light openings claim 3 , respectively.5. The PSU pod assembly of wherein the housing is spaced from the panel claim 2 , and wherein the cabin lighting is positioned between ...

SEAT SHELL AND INTEGRATED OVERHEAD STORAGE BIN

A lounge assembly configured to be positioned in the interior of an aircraft. The lounge assembly includes a first seat shell configured to at least partially surround a passenger seat, and an overhead storage bin assembly. The overhead storage bin assembly includes first and second posts configured to be secured to a floor of the aircraft, and an overhead bin housing supported by the first and second posts. The overhead bin housing includes at least a first overhead storage bin that is positioned generally above the first seat shell. 1. An aircraft comprisinga fuselage having an inner side wall and a floor,at least a first seat having an upper portion, wherein the first seat is secured to the floor,at least a first laterally extending overhead storage bin positioned generally above the upper portion of the first seat, andsupport structure secured to the floor and supporting the first overhead storage bin,wherein the first overhead storage bin has an open and a closed configuration, wherein the first overhead storage bin opens toward the front or the rear of the aircraft.2. The aircraft of further comprisinga second seat having an upper portion, wherein the second seat is secured to the floor and is adjacent the first seat,a second laterally extending overhead storage bin positioned generally above the upper portion of the second seat and adjacent the first overhead storage bin, andsupport structure secured to the floor and supporting the second overhead storage bin,wherein the second overhead storage bin has an open and a closed configuration, wherein the second overhead storage bin opens toward the front or the rear of the aircraft.3. The aircraft of wherein the first and second overhead storage bins are not secured to the inner side wall.4. A lounge assembly configured to be positioned in the interior of an aircraft claim 2 , the lounge assembly comprising:a first seat shell configured to at least partially surround a passenger seat, and first and second posts ...

PASSENGER SUITE SEATING ARRANGEMENT WITH MOVEABLE VIDEO MONITOR

A passenger suite seating arrangement including a first passenger suite including a first seat and a first video monitor fixed in position directly forward of the first seat, and a second passenger suite including a second seat facing the first seat and laterally offset relative thereto, the second suite including a second video monitor configured to move parallel to a viewing angle of a passenger seated in the second seat to selectively connect and divide the first and second suites. 1. A passenger suite seating arrangement , comprising:a first passenger suite including a first seat and a first video monitor fixed in position directly forward of the first seat; anda second passenger suite including a second seat facing the first seat and laterally offset relative thereto along a longitudinal axis of the first and second passenger suites, the second passenger suite including a second video monitor configured to move between first and second positions to connect and divide the first and second passenger suites.2. The seating arrangement of claim 1 , wherein the second video monitor moves parallel to a viewing angle of a passenger seated in the second seat claim 1 , and wherein the first and second passenger suites share a desk positioned therebetween divided by the second video monitor when the second video monitor is positioned directly forward of the second seat.3. The seating arrangement of claim 1 , wherein the first and second passenger suites nest to form a column aligned parallel to a longitudinal axis of an aircraft.4. The seating arrangement of claim 1 , further comprising a third passenger suite laterally adjacent the second passenger suite claim 1 , the third passenger suite including a third seat adjacent the second seat claim 1 , the second and third seats facing in the same direction.5. The seating arrangement of claim 4 , further comprising a partition positioned between the second and third seats claim 4 , the partition moveable between a deployed ...

CENTRE PEDESTAL FOR AIRCRAFT COCKPIT AND AIRCRAFT COMPRISING SUCH A PEDESTAL

The invention relates to an aircraft cockpit centre pedestal for the attachment of control and instrumentation equipment for this aircraft, wherein the centre pedestal includes an equipment module including controls connected to at least one first electrical connector, and a single-piece frame including an upper face provided with a recess including at least one second electrical connector installed at the bottom of the recess and connected to computers onboard this aircraft in which this equipment module is installed, the at least one first electrical connector of the equipment module being inserted into at least one second electrical connector so as to connect the controls of the equipment module and these onboard computers. The invention also relates to an aircraft including such a pedestal. 1. Aircraft cockpit centre pedestal for the attachment of control and instrumentation equipment for this aircraft , wherein the centre pedestal comprises:an equipment module comprising controls connected to at least one first electrical connector,a single-piece frame comprising an upper face provided with a recess comprising at least one second electrical connector located at the bottom of the recess and connected to computers onboard this aircraft in which this equipment module is installed, the at least one first electrical connector of the equipment module being inserted into at least one second electrical connector so as to connect the controls of the equipment module and these onboard computers.2. Centre pedestal according to claim 1 , in which the connection wiring of the equipment module is multiplexed wiring.3. Centre pedestal according to claim 1 , in which the first electrical connectors claim 1 , centralised on the front face of the equipment module claim 1 , are inserted in second electrical connectors installed at the bottom of the recess.4. Centre pedestal according to claim 1 , in which the single-piece frame is made from a composite sandwich.5. Centre pedestal ...

UTILIZATION FOR AIRCRAFT AIRSTAIR SPACE AND FUEL CELL SYSTEM INTEGRATION

Embodiments of the present invention provide improved space utilization concepts for aircraft, and particularly to using under floor space created by the envelope designed to house an airstair system. For example, this space may be used to house and integrate one or more fuel cell system(s) and/or components, such as hydrogen tanks and/or the fuel cell body, such that the fuel cell system can deliver useful byproducts to support various aircraft functions. Additionally or alternatively, the space may be used to store other components. 1. An aircraft having an airstair envelope with the airstairs uninstalled or removed , comprising:a. one or more components of a fuel cell system installed in the airstair envelope; andb. a service panel in the aircraft passenger deck floor to provide access to the airstair space from within the aircraft.2. The aircraft of claim 1 , further comprising one or more of a trash compactor claim 1 , a trash storage claim 1 , a chiller claim 1 , or an inverter positioned in the airstair envelope.3. The aircraft of claim 1 , further comprising one or more of extra pillows claim 1 , blankets claim 1 , beverage items claim 1 , or food storage items positioned in the airstair envelope.4. The aircraft of claim 1 , wherein one or more hydrogen tanks are stored in the airstair envelope.5. The aircraft of claim 1 , wherein a fuel cell body is stored in the airstair envelope and wherein hydrogen tanks are stored remotely claim 1 , with the fuel cell body and at least one hydrogen tank being fluidly connected.6. The aircraft of claim 1 , wherein hydrogen tanks are stored in an overhead space above an aircraft galley.7. The aircraft of claim 1 , wherein the aircraft has a passenger deck floor claim 1 , wherein one or more components of the fuel cell system generate heat claim 1 , and wherein the heat generated is used to heat portions of the passenger deck floor claim 1 , without the need for a separate heated floor panel.8. The aircraft of claim 1 , ...

CABIN SEGMENT, CABIN AND VEHICLE WITH A CABIN

A cabin segment for a vehicle includes two or more parking spaces, arranged side by side and separated from each other by at least one intermediate wall, for accommodating serving trolleys, and furthermore a vehicle attendant seat which on one side is held on one of the at least one intermediate walls so as to be pivotable on an axis. The vehicle attendant seat is pivotable to an in-use position and to an out-of-the-way position. The in-use position and the out-of-the-way position are situated apart by 90° or more relative to the pivoting of the vehicle attendant seat. This makes possible particularly efficient use of space without having to forego parking spaces or a vehicle attendant seat. 1. A cabin segment for a vehicle , comprising:at least first and second parking spaces, arranged side by side and separated from each other by at least one intermediate wall, for accommodating serving trolleys, anda vehicle attendant seat which on one side is held on the at least one intermediate wall so as to be pivotable on an axis,wherein the vehicle attendant seat is pivotable to an in-use position and to an out-of-the-way position,wherein the in-use position and the out-of-the-way position are situated apart by 90° or more relative to the pivoting of the vehicle attendant seat.2. The cabin segment of claim 1 , wherein the in-use position and the out-of-the-way position are situated apart by substantially 180°.3. The cabin segment of claim 1 , further comprising a locking means for locking the vehicle attendant seat in the in-use position.4. The cabin segment of claim 1 , further comprising at least one storage compartment claim 1 , arranged above the parking spaces claim 1 , for accommodating objects.5. The cabin segment of claim 1 , wherein the vehicle attendant seat comprises a removable or fold-away headrest.6. The cabin segment of claim 1 , wherein the first parking space comprises a first receiving opening that extends so as to be largely parallel to a width of the ...

Pivoting display device used in aircraft

A pivoting device especially useful in aircraft passenger cabins that can pivot a monitor between stowed and open positions, the pivoting device including a forward/reverse rotatable driving motor. An electromagnetic brake holds the monitor in stowed and opened positions A power unit powers the motor and the electromagnetic brake. A controller controls the pivoting movement of the monitor. The power unit includes a rectifier circuit that transforms AC to a DC, a step-up circuit that steps up the transformed voltage, a voltage regulator that adjusts the transformed voltage to a prescribed DC voltage, and a retraction power retention circuit including a capacitor. When no source voltage is detected while the monitor is in its opened state, the capacitor supplies the power to a voltage regulator of the power circuit, deactivates the electromagnetic brake and reverse rotates the motor to drive the monitor to its stowed position.

OVERHEAD SPACE UTILIZATION DEVICE

One particular overhead space utilization device, adapted for installation in a hull structure, incorporates at least one berth module with first and second berth portions, first and second intermediate support members, and first and second coupling members. Each berth module has two opposing berth members with a walkway therebetween. The first and second intermediate support members each has a first end pivotably coupled to the corresponding one of the first and second berth portions, and a second end configured to be pivotably coupled to the hull structure. The first and second coupling members are configured to pivotably couple the second berth portions to the hull structure. The first and second coupling members and the second berth portions are configured to be positioned outboard of the first berth portion. 1. An overhead space utilization device adapted to install in a hull structure , the device comprising:at least one berth module having a first berth portion and a second berth portion, the berth module having two opposing berth members and a walkway therebetween;first and second intermediate support members, each having first and second ends, the first end pivotably coupled to the corresponding one of the first and second berth portions, respectively, and the second end configured to be pivotably coupled to the hull structure; andfirst and second coupling members configured to pivotably couple the second berth portion of the first and second berths, respectively, to the hull structure, wherein, the first and second coupling members and the second berth portion are configured to be positioned outboard of the first berth portion.2. The device of wherein the walkway is pivotably coupled to the first and second berth portions.3. The device of wherein the intermediate support member and the first and second coupling members are configured to inhibit berth module movement along an axis substantially parallel to a yaw axis of the vessel.4. The device of claim 1 , ...

Device for securing a mobile device in an aircraft cabin

A device for securing a mobile device in an aircraft cabin includes a first connection element having a bar receiving member. The device further has a second connection element which includes a bar which is suitable for co-operating with the bar receiving member of the first connection element, the bar being moveable between an unlocking position and a locking position, in which the bar of the second connection element is able to be brought into engagement with the bar receiving member of the first connection element. 1. A device for securing a mobile device in an aircraft cabin , comprising:a first connection element comprising a bar receiving member, anda second connection element comprising a bar which is suitable for co-operating with the bar receiving member of the first connection element, the bar being moveable between an unlocking position and a locking position, in which the bar of the second connection element is able to be brought into engagement with the bar receiving member of the first connection element.2. The device according to claim 1 , wherein the bar of the second connection element comprises a first bar element and a second bar element which is movable relative to the first bar element between a first position and a second position claim 1 , the second bar element being located in its first position in the unlocking position of the bar claim 1 , being moveable into its second position in order to enable a movement of the bar from its unlocking position into its locking position and claim 1 , in the locking position of the bar claim 1 , being moveable into its first position again in order to bring the bar into engagement with the bar receiving member of the first connection element.3. The device according to claim 1 , wherein at least one of the first and the second connection element comprises a base member having a substantially L-shaped cross-section.4. The device according to claim 2 , wherein the bar receiving member of the first connection ...

Locking assembly for locking an aircraft interior structure to an internal mounting frame in an aircraft cabin

The invention relates to a locking assembly for locking an aircraft interior structure ( 13 ) to an internal mounting frame ( 2 ) comprising: a sliding element ( 1 ) which is suitable for insertion in the internal mounting frame ( 2 ), a height adjustment assembly, comprising a lower and an upper height adjustment part ( 4, 5 ). The assembly further comprises a fitting ( 6 ) attachable to the aircraft interior structure, having a recess wherein a projection ( 19 ) of the upper height adjustment part ( 5 ) is received, wherein the fitting ( 6 ) can be moved with respect to the projection ( 19 ) in a plane defined by X r - and Y r -directions. Further provided is a locking bolt ( 11 ) received in the upper height adjustment part ( 5 ) for locking the fixation element ( 9 ), the fitting ( 6 ), and the height adjustment parts ( 4, 5 ) to the sliding element ( 1 ).

Self-Locking Joints for Panel Structures and Methods of Fabricating the Same

There is provided in an embodiment a method of fabricating a self-locking joint in a panel structure. The method provides a panel structure having at least two face sheets and a core portion sandwiched therebetween. The method further fabricates in a first portion of the panel structure at least one mortise opening having self-locking end portions. The method further fabricates on a second portion of the panel structure at least one tenon extension having flexible self-locking members. The method further interlocks the flexible self-locking members of the at least one tenon extension with the self-locking end portions of the at least one mortise opening to form a self-locking joint in the panel structure.

SUN SCREEN

The present invention relates to an apparatus, method and system for protecting the occupants of vehicles and aircraft from sun glare. 1. An apparatus for screening the sun from the occupants of a vehicle , said apparatus comprising:A mesh material to block a portion of the incident solar rays from entering the passenger compartment of the vehicle,Said mesh material being sufficiently flexible to conform to any vehicle window shape, yet sufficiently firm to retain its solar ray blocking abilities,Said mesh material having a coating places thereon giving said mesh material the ability to have an erasable message written thereon.2. The apparatus of claim 1 , wherein said mesh material also has solar photo-voltaic capable materials affixed thereon for additional portable electrical power supply.3. The apparatus of claim 1 , wherein said apparatus is used as an in vehicle work station divider.4. The apparatus of claim 1 , wherein said apparatus is used as a privacy screen for passengers in aircraft.5. The apparatus of claim 1 , wherein said mesh material is capable of having electroluminescent materials added thereto for in vehicle passenger entertainment and education.6. A method for screening the sun from the occupants of a vehicle claim 1 , said method comprising:Having a mesh material to block a portion of the incident solar rays from entering the passenger compartment of the vehicle,Said mesh material being sufficiently flexible to conform to any vehicle window shape, yet sufficiently firm to retain its solar ray blocking abilities,Said mesh material having a coating places thereon giving said mesh material the ability to have an erasable message written thereon.7. The method of claim 6 , wherein said mesh material also having solar photo-voltaic capable materials affixed thereon for additional portable electrical power supply.8. The method of claim 6 , wherein said method is used as an in vehicle work station divider.9. The method of claim 6 , wherein said method ...

WATER MANAGEMENT SYSTEM

Embodiments of the present invention provide a water management system for use on board a passenger transport vehicle. The water management system may be used to address and manage excess humidity, water leaks, or any other instance when water or other liquid may collect at a certain location. The disclosure provides a system for managing excess water and for optionally delivering the water to another location. The removal location may be a disposal outlet or it may be a beneficial use of the collected water on-board the vehicle. 1. A water management system for use on-board a passenger transport vehicle , comprising:(a) a water collection device comprising one or more areas for receiving moisture or water;(b) a conduit between the water collection device and a removal location to which the moisture or water is to be removed, through which there is created a pressure differential to cause the moisture to be pulled into and through the conduit; and(c) a valve to control passage of moisture or water through the conduit.2. The water management system of claim 1 , wherein the collection device comprises a tube.3. The water management system of claim 2 , wherein the tube comprises one or more perforations claim 2 , openings claim 2 , or holes into which moisture flows.4. The water management system of claim 1 , wherein the collection device comprises a mat.5. The water management system of claim 4 , wherein the mat comprises one or more perforations claim 4 , openings claim 4 , or holes into which moisture flows.6. The water management system of claim 1 , wherein the one or more areas for receiving moisture comprise perforations or openings.7. The water management system of claim 1 , wherein the water collection device claim 1 , the conduit claim 1 , or both are heated for freeze protection.8. The water management system of claim 1 , wherein at least a portion of the water collection device is coated with claim 1 , impregnated with claim 1 , or associated with an anti- ...

AIRCRAFT SMART CABIN CONTROL

A touchless system for an aircraft cabin is disclosed. The system includes machine-readable codes placed on passenger seats and other aircraft surfaces that may be scanned and linked to cabin control systems through an application installed on personal portable electronic devices. The system also includes a communication system linked to the personal portable electronic devices via the application and linked to the cabin control systems that facilitates the control of one or more control systems by the personal portable electronic device. One of the cabin control systems is configured as an overhead storage container configured with a gesture sensing system, allowing the storage lid to be opened through specific gestures. 1. A system comprising:a first machine-readable code disposed on a first surface of an aircraft cabin, wherein the first machine-readable code is scanned by a portable electronic device, generating first scanned data; a receiver;', 'a transmitter;', 'at least one processor; and', receive the first scanned data from the portable electronic device;', 'receive an identification input from the portable electronic device;', 'determine, based on the first scan data and the identification input, a user identification;', 'receive a first input message from the portable electronic device; and', 'send a control message to one or more control systems based on the user identification and the first input message; and, 'a memory coupled to the at least one processor, the memory including instructions stored upon that, when executed by the at least one processor, causes the at least one processor to], 'a communication unit in communication with the portable electronic device comprising receiving the first scanned data;', 'receiving the identification input;', 'sending the first scanned data and the identification input to the communication unit; and', 'sending the first input message to at least one of the communication unit or the one or more control systems., ' ...

A stowage device of emergency equipment for aircraft crewmember

A stowage device of emergency equipment for aircraft crewmember, the stowage device comprising a housing, the housing extends along a longitudinal direction and has side walls, a back wall and an opening opposite to the back wall, the side walls and the back wall define an internal space adapted to stow a respiratory mask in a stowage position, the side walls extend along the longitudinal direction up to a front edge delimiting the opening. One of the side walls is an adjustable wall. The housing comprises a frame and a movable element. The movable element is mounted on the frame and is movable between a retracted position and a protruding position. The movable element comprises a main movable panel and the adjustable wall includes the main movable panel.

LIGHT AND LIGHTING SYSTEM

A light for an interior of a vehicle contains at least two light modules that are disposed in series along a profile line and are mounted on a supporting structure in the vehicle. Each two adjacent light modules are attached to each other in regions. All light modules together form a light strip, which is attached to the supporting structure with exactly one first region, wherein a second region is movably supported on the supporting structure. 1. A light for an interior of a vehicle that contains at least two light modules , wherein in an installed state (E) the light modules are mounted on a supporting structure in the vehicle , and the light modules are disposed in series along a profile line , and wherein in the installed state (E) ,each two adjacent light modules are attached to each other in regions in a fixed relative mutual position (G),wherein all light modules that are mutually attached to each other together form a light strip,the light strip is attached with exactly one first region to the supporting structure in a fixed relative position (F) to the supporting structure, andat least one second region of the light strip is movably supported on the supporting structure in a variable relative position (V) to the supporting structure.2. The light according to claim 1 , wherein in the installed state (E) each of the light modules comprises at least the first region or one of the second regions.3. The light according to claim 1 , wherein the light contains exactly one first mounting arrangement that is designed for the attachment of the first region to the supporting structure claim 1 , and contains a respective second mounting arrangement that is designed for respective movable support of a respective second region on the supporting structure claim 1 , and contains respective joining arrangements that are designed for mutual attachment of the regions of the light modules to each other.4. The light according to claim 3 , wherein the first mounting arrangement ...

Deployable handle system for a vehicle

A handle system for a vehicle is disclosed and includes a support structure defining a handle. The support structure is movable between a stowed position where the handle is inaccessible by a passenger and a deployed position where the handle is accessible by the passenger. The handle system also includes an actuator operably coupled to the support structure and configured to move the support structure between the stowed position and the deployed position. The handle system further includes one or more sensors configured to obtain data indicative of vehicle motion and a controller. The controller is configured to determine the vehicle exceeds a threshold rate of movement based on the data obtained by the one or more sensors. In response to determining the vehicle exceeds the threshold rate of movement, the controller instructs the actuator to move the support structure from the stowed position into the deployed position.

Overhead Payload Module With Integrated Stowbins

In an example, an overhead payload module is described. The overhead payload module comprises a ceiling assembly, an aisle floor assembly, a first payload assembly attached to the ceiling assembly and the aisle floor assembly to form a first side of the overhead payload module, and a second payload assembly attached to the ceiling assembly and the aisle floor assembly to form a second side of the overhead payload module. The first payload assembly comprises a first payload module and a first overhead stowbin module structurally integrated with the first payload module and having a first stowage area configured to receive stowbins. The second payload assembly is positioned opposite the first payload assembly to form an aisle therebetween and comprises a second payload module and a second overhead stowbin module structurally integrated with the second payload module and having a second stowage area configured to receive stowbins. 1. An overhead payload module for installation in an aircraft , the overhead payload module comprising:an aisle floor assembly; a first payload module,', 'at least one first blade fitting attached to an exterior of the first payload module, and', 'a first overhead stowbin module structurally integrated with the first payload module and having a first stowage area configured to receive stowbins; and, 'a first payload assembly attached to the aisle floor assembly to form a first side of the overhead payload module, wherein the first payload assembly comprises a second payload module,', 'at least one second blade fitting attached to an exterior of the second payload module, and', 'a second overhead stowbin module structurally integrated with the second payload module and having a second stowage area configured to receive stowbins,, 'a second payload assembly attached to the aisle floor assembly to form a second side of the overhead payload module, wherein the second payload assembly is positioned opposite the first payload assembly to form an ...

PASSENGER SEATING ARRANGEMENT

A passenger seating arrangement for a vehicle cabin comprising a plurality of seat units, wherein the seat units in one column are arranged one behind another in a longitudinal direction of the vehicle cabin, wherein at least one of the forward facing seat units is arranged in a front row section of the vehicle cabin and is followed by at least one angled seat unit in the same column. Further, a vehicle cabin having such a passenger seating arrangement is provided. 1. A passenger seating arrangement for a vehicle cabin comprising a first set of a plurality of seat units , wherein:the seat units of the first set of the plurality of seat units in a first column are arranged one behind another in a longitudinal direction of the vehicle cabin,each seat unit of the seat units of the first set of the plurality of seat units comprises a side bordering an aisle of the vehicle cabin,each seat unit of the seat units of the first set of the plurality of seat units comprises at least one console and one seat arranged adjacent to the console,each seat unit of the seat units of the first set of the plurality of seat units is adjustable between at least a seating position and at least a bed position,each seat unit of the seat units of the first set of the plurality of seat units is one of a forward facing seat unit, wherein at least a longitudinal axis of the seat is parallel to a longitudinal axis of the vehicle cabin, and is one of an angled seat unit, wherein at least the longitudinal axis of the seat is angled relative to the longitudinal axis of the vehicle cabin, andwherein at least one of the forward facing seat units is arranged in a front row section of the vehicle cabin and is followed by at least one angled seat unit in a same column.2. The passenger seating arrangement according to claim 1 , wherein the forward facing seat unit is arranged in at least a very first front row of the front row section.3. The passenger seating arrangement according to claim 1 , wherein ...

SEAT UNIT AND PASSENGER SEATING ARRANGEMENT PROVIDED WITHIN A VEHICLE CABIN

A seat unit for a passenger seating arrangement provided within a vehicle cabin, wherein—the seat unit comprising at least a forward facing seat and at least a console arranged adjacent to the seat and a wall structure, wherein the seat unit is configured to link—the forward facing seat arranged in front of the wall structure, and—an angled seat arranged behind the wall structure, wherein the console provides a footwell for a passenger of the angled seat. 1. A seat unit for a passenger seating arrangement provided within a vehicle cabin , the seat unit comprising:at least a forward facing seat; andat least a console arranged adjacent to the forward facing seat and a wall structure,wherein the seat unit is configured to link the forward facing seat arranged in front of the wall structure and an angled seat arranged behind the wall structure, and wherein the console provides a footwell for a passenger of the angled seat.2. The seat unit according to claim 1 , wherein the seat unit is configured to link the forward facing seat arranged in front of the wall structure and either an angled seat or a forward facing seat arranged behind the wall structure claim 1 , and wherein the console provides a footwell for the passenger of either the angled seat or the forward facing seat.3. The seat unit according to claim 1 , wherein the console is configured as a transition module to allow a transition between the forward facing seat and the angled seat.4. The seat unit according to claim 1 , wherein the wall structure comprises a transition module to allow a transition between the forward facing seat and the angled seat.5. The seat unit according to claim 1 , wherein the wall structure is configured to accommodate a monitor for the passenger of the angled seat.6. The seat unit according to claim 5 , wherein the transition module is configured such that the monitor is arranged substantially perpendicular to a longitudinal axis of the angled seat.7. The seat unit according to claim ...

Stowage carousel and method of storing cargo for use with an aircraft

A stowage carousel for handling cargo aboard an aircraft is provided including a revolving conveyor having an inner ring facing a passenger cabin of the aircraft and an outer ring facing a fuselage of the aircraft. Stowage compartments are associated with the revolving conveyor. The stowage compartments are configured to receive the cargo. The stowage compartments are rotatable within the aircraft with the revolving conveyor. The revolving conveyor is situated within the aircraft partially in the passenger cabin and partially in at least one of an upper crown and a lower lobe of the aircraft.

DROP DOWN OVERHEAD GALLEY STOWAGE SYSTEM

An aircraft overhead stowage system for a cross-aisle galley complex. The aircraft overhead stowage system includes a stowage compartment housing disposed above a ceiling of the galley complex that is supported above the ceiling by a stowage support structure. A first stowage compartment and a second stowage compartment are each movably engaged with and disposed inside the stowage compartment housing, and each stowage compartment is movable between a stowed position and a deployed position relative to the stowage compartment housing using a vacuum system. A vacuum generator that creates a vacuum force is mounted on the stowage compartment housing, and a plurality of vacuum bellows connected to each stowage compartment are in fluid communication with the vacuum generator. The vacuum system causes the stowage compartments to move between the stowed position and the deployed position. Vacuum-driven and manually-driven latching assemblies and removable extensions for each stowage compartment are also provided. 1. An aircraft overhead stowage system for a cross-aisle galley complex , the system comprising:a stowage compartment housing disposed above a ceiling of a cross-aisle galley complex, the stowage compartment housing being supported above the ceiling by a stowage support structure;a first stowage compartment and a second stowage compartment each movably engaged with and disposed inside the stowage compartment housing, each stowage compartment movable between a stowed position and a deployed position relative to the stowage compartment housing; a vacuum generator that creates a vacuum force, the vacuum generator mounted on the stowage compartment housing; and', 'a plurality of vacuum bellows connected to each stowage compartment and in fluid communication with the vacuum generator, wherein each of the vacuum bellows contracts in response to a negative pressure caused by the vacuum force, and wherein each of the vacuum bellows expands in response to a venting of the ...

AIRPLANE SEAT DEVICE

An airplane seat device includes at least one airplane seat element implementing at least a portion of a table-less airplane seat, with at least one deposit and/or storage element which is embodied separate from the airplane seat element; the airplane seat element comprising at least one interface via which the deposit and/or storage element can be connected to the airplane seat element if required. 1. An airplane seat device with at least one airplane seat element implementing at least a portion of a table-less airplane seat , with at least one deposit and/or storage element which is embodied separate from the airplane seat element; the airplane seat element comprising at least one interface via which the deposit and/or storage element can be connected to the airplane seat element if required.2. The airplane seat device according to claim 1 , wherein the interface comprises at least one force-fit and/or form-fit element claim 1 , via which the deposit and/or storage can be connected to the airplane seat element.3. The airplane seat device according to claim 2 , wherein the force-fit and/or form-fit element of the interface is embodied as a recess claim 2 , which the deposit and/or storage element is insertable into.4. The airplane seat device according to claim 1 , wherein the airplane seat element is embodied as a backrest.5. The airplane seat device according to claim 1 , wherein the deposit and/or storage element is provided to be mounted to the airplane seat element tool-lessly.6. The airplane seat device at least according to claim 3 , wherein the deposit and/or storage element comprises at least one interface which can be coupled to the interface of the airplane seat element.7. The airplane seat device according to claim 1 , wherein the deposit and/or storage element is embodied as a serving element.8. The airplane seat device according to claim 1 , wherein the deposit and/or storage element comprises at least one receptacle for a drink vessel.9. The airplane ...

Galley Monument For An Aircraft And Aircraft

A galley monument for an aircraft has a shelf structure, a pull-out member supported on the shelf structure so as to be able to be moved between an insertion position and a deployment position and has a carrier plate, and a display device supported on the pull-out member and having a display. A first surface of the carrier plate in the deployment position of the pull-out member is located in a deployment plane and protrudes with respect to the shelf structure and is located in the insertion position at least partially inside the shelf structure. The display device in the deployment position of the pull-out member can be pivoted about a centre of rotation between a storage position, in which the display device extends parallel with the deployment plane, and a position for use, in which the display device extends transversely relative to the deployment plane. 1. A galley monument for an aircraft comprising:a shelf structure;a pull-out member supported on the shelf structure and configured to be moved between an insertion position and a deployment position and having a carrier plate, wherein a first surface of the carrier plate in the deployment position of the pull-out member is located in a deployment plane and protrudes with respect to the shelf structure and is located in the insertion position at least partially inside the shelf structure; anda display device supported on the pull-out member and having a display;wherein the display device in the deployment position of the pull-out member is configured to be pivoted about a centre of rotation between a storage position, in which the display device extends parallel with the deployment plane, and a position for use, in which the display device extends transversely relative to the deployment plane.2. The galley monument according to claim 1 , wherein the centre of rotation is arranged in a first end region of the carrier plate and wherein the first end region of the carrier plate in the deployment position of the pull ...

AIRCRAFT SEAT, AIRCRAFT SEAT ARRANGEMENT WITH AN AIRCRAFT SEAT AND AIRCRAFT WITH AN AIRCRAFT SEAT ARRANGEMENT

An aircraft seat with a voltage supply port associated only with the aircraft seat and/or a data port associated only with the aircraft seat, a voltage supply unit, associated with the aircraft seat and including a voltage input and a voltage output, each of which is connected to another of the voltage supply ports, a switching circuit associated only with the aircraft seat and hooked up between the voltage output and the voltage supply port and/or between the data port and a data network, with which each of the voltage supply port or each of the data port can be activated or deactivated. A control unit is associated only with the aircraft seat and connected to the switching circuit, and a near-field communication reading device connected to the control unit and associated only with the aircraft seat for wireless reception of signals from an external near-field communication sending device, wherein the reading device can receive signals from a predetermined group of predetermined near-field communication signals, and the reading device and control unit adapted for the control unit to activate at least one of the voltage supply ports and/or at least one of the data ports only upon reception of one of the signals by the switching circuit in dependence on the received signal. 1. An aircraft seat , comprising:at least one voltage supply port associated only with the aircraft seat and/or at least one data port associated only with the aircraft seat;a voltage supply unit, which is associated with the aircraft seat and which comprises a voltage input for connection to an onboard voltage network of an aircraft and at least one voltage output, each of which is connected to another one of the voltage supply ports;a switching circuit associated only with the aircraft seat and hooked up between the at least one voltage output and the at least one voltage supply port and/or between the at least one data port and a data network, with which each of the at least one voltage supply ...

PASSENGER COMMUNICATION SYSTEM

A communication system for a vehicle seat includes a visual indicator having a lighting mechanism configured to display a plurality of colors, a control portion electrically connected to the visual indicator, and a plurality of modes. Each mode may be associated with one of the plurality of Selection of one of the plurality of modes causes the control portion to signal the lighting mechanism to display the color associated with the selected mode. 1. A communication system for a vehicle seat , the communication system comprising:a visual indicator comprising a lighting mechanism configured to display a plurality of colors;a control portion electrically connected to the visual indicator; anda plurality of modes, wherein:each mode is associated with one of the plurality of colors; andselection of one of the plurality of modes causes the control portion to signal the lighting mechanism to display the color associated with the selected mode.2. The communication system of claim 1 , wherein the visual indicator displays a distinct visual indicia for each mode and the visual indicator comprises an LED light.3. The communication system of claim 1 , wherein the plurality of modes comprises a Do Not Disturb mode wherein the visual indicator illuminates as a solid red light.4. The communication system of claim 1 , wherein the plurality of modes comprises a Wake Me for Meals/Beverage mode wherein the visual indicator illuminates as a solid blue light.5. The communication system of claim 1 , wherein the plurality of modes comprises at least three of a Do Not Disturb mode claim 1 , a Wake Me for Meals/Beverage mode claim 1 , a Need Assistance mode claim 1 , a Wake Me for Duty-Free mode claim 1 , a Medical Emergency mode claim 1 , and a Vacant Seat mode.6. The communication system of claim 1 , wherein the visual indicator is disposed on an upper surface of a seatback.7. The communication system of claim 6 , wherein the visual indicator further comprises an auxiliary light disposed ...

Integrated Aircraft Signage, Lighting, and Display System

An integrated aircraft lighting and display panel includes high-density arrays of micro-scale light-emitting diodes (LED) set into arrays (e.g., linear, two-dimensional, freeform) to form tiles, the LED tiles combined and interconnected to form LED panels conformable to any interior surface within an aircraft cabin. The PCB and LED arrays may be set into structural layers corresponding to overhead panels, side panels, bin panels, divider panels, doorway panels, galley and monument panels, or other interior structural panels of the aircraft. The LED arrays may be activated by an onboard video processor and local panel-level controllers to provide cabin lighting, indicate aircraft signage, display high-resolution image or video graphics, or simultaneously blend any combination thereof, either on command or in response to detected conditions. 1. An integrated aircraft signage , lighting , and display system , comprising: at least one video processor configured to a) generate streaming image content and b) retrieve stored streaming image content from at least one data storage unit in communication with the video processor;', 'and', 'at least one sender card configured to generate a video signal by encoding the streaming image content;, 'at least one video processing unit (VPU) coupled to a power supply of an aircraft and in communication with at least one of a master controller of the aircraft, a network of the aircraft, and a data interface of the aircraft, the VPU comprising a driver unit including at least one control processor configured to a) receive at least a portion of the encoded video signal and b) generate control input based on the received portion; and', 'at least one panel interface coupled to the power supply and to the control processor, the panel interface configured to supply at least one of operating power and the control input to at least one light emitting diode (LED) panel in communication with the PCU;, 'one or more panel control units (PCU) in ...

SEAL ASSEMBLY FOR A GALLEY DOOR OF A GALLEY AND METHOD OF ASSEMBLING A GALLEY WITH A SEAL ASSEMBLY

A seal assembly for use with a door within a frame of a galley of an aircraft includes a seal configured to be movably coupled to the door and a seal holder holding the seal. The seal assembly includes a biasing mechanism coupled to the seal holder and configured to hold the seal in an open position by applying a biasing force to the seal holder. An activation mechanism is operably coupled to the seal holder that overcomes the biasing force to move the seal from the open position to a sealed position. 1. A seal assembly for use with a door within a door frame of a galley of an aircraft , the seal assembly comprising:a seal configured to be movably coupled to the door;a seal holder holding the seal;a biasing mechanism coupled to the seal holder, the biasing mechanism configured to hold the seal in an open position by applying a biasing force to the seal holder; andan activation mechanism operably coupled to the seal holder, the activation mechanism configured to overcome the biasing force to move the seal from the open position to a sealed position.2. The seal assembly of claim 1 , wherein the seal includes a seal interface at a bottom of the seal claim 1 , the seal holder positioning the seal below a bottom of the door.3. The seal assembly of claim 1 , wherein the seal includes a seal interface at a side edge of the seal claim 1 , the seal holder positioning the seal interface at the door frame below a bottom of the door.4. The seal assembly of claim 1 , wherein the seal holder is configured to be pivotably coupled to the door and rotated between the open position and the sealed position.5. The seal assembly of claim 1 , wherein the seal holder is configured to be linearly actuated between the open position and the sealed position in a direction perpendicular to a seal interface of the seal.6. The seal assembly of claim 1 , wherein the seal holder includes a hinge claim 1 , the seal holder being rotated about the hinge.7. The seal assembly of claim 1 , wherein the ...

HYBRID WASTE TUBE ASSEMBLY

The present technology is directed to a conductive hybrid waste tube system that comprises tube bodies, tube end fittings, O-rings, coupling sleeves, end fitting adapters and couplings. The tube bodies and tube end fittings are attached and constitute a tube section. O-rings are installed between flanges on the end fittings and the sleeve positioned over the end fittings of adjoining tube sections. If the tubes end fittings are of different designs, an end fitting adapter may be used along with an additional O-ring to provide pressure sealing. The coupling is installed over the completed assembly to prevent the joint from separating. The O-rings/sleeve combination provides the ability for the tube sections to translate and rotate relative to each other while the coupling prevents the joint from excessive translation. 1. A hybrid waste tube assembly , comprising:electrically conductive metal tube segments that each have a first radial engagement surface adjacent to an open end portion;tubular, electrically conductive, non-metallic end fittings each having a second radial engagement surface, each end fitting being fixedly connected to the open end portion of a respective one of the tube segments in an overlapping configuration with the second radial engagement surface engaging the first radial engagement surface; anda clamping assembly connected to the end fittings on adjacent, axially aligned tube segments, the clamping assembly sealably interconnecting the end fittings with adjacent tube segments aligned to contain and allow a flow of material therethrough, the clamping assembly having an electrically conductive bridge engaging the adjacent end fittings and maintaining electrical continuity across the adjacent tube segments and end fittings.2. The assembly of wherein the first radial engagement surface is an exterior surface defining an outer diameter of the tube segment claim 1 , and the second radial engagement surface is an interior surface defining an inner ...

FRICTION STOP DEVICE

Deployment apparatus () including a deployment object (), a deployment arm () with a first end () coupled to the deployment object and a second end () having a pivot (), and a hinge assembly () rotatably attached to the pivot of the deployment arm. The hinge assembly () includes an enclosure () and a friction stop device () disposed within the enclosure such that the friction stop device includes a friction portion () configured to be pressed against a lateral surface of the pivot () of the deployment arm such that the friction portion provides a predetermined torque. The predetermined torque may be calculated based on maintaining a deployed angle of the deployment arm () such that the deployment object () is held in a raised deployed position. 1. A deployment apparatus comprising:a deployment object;a deployment arm with a first end coupled to the deployment object and a second end having a pivot; anda hinge assembly rotatably attached to the pivot of the deployment arm, the hinge assembly comprising an enclosure and a friction stop device disposed within the enclosure, the friction stop device comprising a friction portion configured to be pressed against a lateral surface of the pivot of the deployment arm such that the friction portion provides a predetermined torque.2. The deployment apparatus of claim 1 , wherein the predetermined torque is calculated based on maintaining a deployed angle of the deployment arm such that the deployment object is held in a raised deployed position.3. The deployment apparatus of claim 1 , wherein the friction portion is disposed axially with respect to a rotational axis at the second end of the deployment arm.4. The deployment apparatus of claim 1 , wherein the friction stop device further comprises a first backing plate bonded to the friction portion.5. The deployment apparatus of claim 1 , wherein the friction stop device further comprises one or more Belleville washers configured to maintain a compression load on the friction ...

LIGHTED CUP HOLDER FOR SEATING ARRANGEMENTS

A method and apparatus include attaching a lighted cup holder to a seating arrangement. The lighted cup holder includes a cup holder body and a light-producing light source, with the cup holder body being attached to the seating arrangement and having a cup receptacle therein, the light-producing source being disposed within the cup receptacle for illuminating the receptacle. A light-sensitive element operatively connected to the light source selectively controls production of light by the light source in such a manner that illumination of the cup holder is provided only under conditions where visibility is reduced to the point that it becomes difficult to locate the cup holder. The light-sensitive element is mounted on a master lighted cup holder and controls illumination of the master lighted cup holder and one or more slave lighted cup holders operatively connected to the master lighted cup holder. 17-. (canceled)8. A chair comprising a cup holder apparatus , the cup holder apparatus comprising at least one cup holder having a cup holder body adapted for attachment to the chair , wherein the cup holder body has a lower end , a top end , and a cup holding receptacle therebetween , and a flange extending at the top end of the cup holder body , wherein the flange comprises two or more control switches mounted thereon or attached thereto , wherein one of the two or more control switches is operatively connected to a light source for control thereof and one of the two or more control switches is operatively connected to a component of the chair for control thereof.9. The chair of claim 8 , wherein the component of the chair is a powered reclining mechanism.10. The chair of claim 8 , wherein the light source is a light emitting diode (LED).11. The chair of claim 10 , wherein the light emitting diode (LED) illuminates the cup holder apparatus.12. The chair of claim 8 , wherein the flange extends outwardly from the top end of the cup holder body.13. The chair of claim 8 ...

SLIM AIRCRAFT MONUMENT WITH DEPLOYABLE WORKSTATION

A slim aircraft monument is installable in an aircraft cabin adjacent to an aisle and has an upper portion, a lower portion, and a middle portion between the upper and lower portions. The monument includes a storage compartment accessible from a first side and a door on an adjacent side, the door deployable into the adjacent aisle or cabin space to reveal folding interconnected panels also deployable into the cabin space. The interconnected panels unfold into a horizontal workspace and, beneath the workspace, a series of vertically stacked storage bays capable of accommodating storage drawers and a cart bay configured for temporary accommodation of a half-size galley cart. 1. An aircraft monument , comprising: at least one storage compartment accessible from a first side;', 'at least one door disposed on a second side of the monument, the door configured to deploy into the cabin space from a closed position to an open position; and', 'a plurality of interconnected panels deployable between a folded position substantially parallel to the door and an unfolded position within the cabin space and adjacent to the door, the plurality of interconnected panels in the unfolded position comprising:', 'a substantially horizontal worksurface;', 'one or more bays vertically stacked below the worksurface, each bay configured to accept a storage drawer; and', 'a cart space below the worksurface and adjacent to the one or more bays, the cart space configured for partially enclosing a galley cart., 'a monument installable in a cabin of an aircraft and proximate to a cabin space, the monument having an upper portion, a lower portion, and a middle portion between the upper and lower portions, the monument comprising2. The aircraft monument of claim 1 , further comprising:at least one cabin attendant seat mounted to the door and deployable for occupancy by a crewmember when the door is in the closed position.3. The aircraft monument of claim 1 , wherein the cabin space is adjacent to ...

SYSTEM FOR GUIDANCE OF A ROBOT THROUGH A PASSENGER CABIN OF AN AIRCRAFT

A system for guidance of a robot through a passenger cabin of an aircraft on at least a part of a defined system of paths including a robot, having at least one secondary coil, a field of coils including N primary coils being integrated in the floor of the passenger cabin of an aircraft, the arrangement of the primary coils defining a system of paths of the robot, and a control system for positioning of and energy provision to the robot including a command unit for sending instructions to the robot, so that the robot can reach a specific position of the defined system of paths. 1. A system for guidance of a robot through a passenger cabin of an aircraft on at least a part of a defined system of paths , comprising:a robot, having at least one secondary coil;a field of coils comprising a plurality of N primary coils being integrated in a floor of the passenger cabin of an aircraft, an arrangement of the primary coils defining a system of paths of the robot; anda control system for positioning of and energy provision to the robot comprising:a command unit for sending instructions to the robot, so that the robot can reach a specific position of the defined system of paths;wherein the primary coils which correspond to the specific position of the system of paths can be dynamically activated, with a result that a magnetic field for guiding the robot is generated,wherein the at least one secondary coil has a radio-based transmitting/receiving system, andwherein each of the N primary coils has a radio-based transmitting/receiving system, and wherein, when the at least one secondary coil is at least partially above one of the primary coils, energy and/or data can be bidirectionally transmitted to and from the at least one secondary coil of the robot in a contactless manner via at least one respective primary coil by the radio-based transmitting/receiving system.2. The system for guidance of a robot according to claim 1 , further comprising at least one interface for ...

MOTION-ADAPTING DISPLAYS WITHIN VEHICLES

A display adaptation system for a vehicle includes a display that is configured to show one or more features. A motion sensor is configured to detect motion of the vehicle. The motion sensor outputs a motion signal indicative of the motion of the vehicle. A motion-compensating control unit is in communication with the display and the motion sensor. The motion-compensating control unit is configured to analyze the motion signal to determine the motion of the vehicle. The motion-compensating control unit is configured to move the feature(s) shown on the display based on the motion of the vehicle. 1. A display adaptation system for a vehicle , the display adaptation system comprising:a display that is configured to show one or more features;a motion sensor that is configured to detect motion of the vehicle, wherein the motion sensor outputs a motion signal indicative of the motion of the vehicle; anda motion-compensating control unit in communication with the display and the motion sensor, wherein the motion-compensating control unit is configured to analyze the motion signal to determine the motion of the vehicle, and wherein the motion-compensating control unit is configured to move the one or more features shown on the display based on the motion of the vehicle.2. The display adaptation system of claim 1 , further comprising a touchscreen claim 1 , wherein the touchscreen includes the display claim 1 , and wherein the one or more features include one or more operating members of the touchscreen.3. The display adaptation system of claim 1 , wherein the motion sensor comprises one or more of an accelerometer or a gyro.4. The display adaptation system of claim 1 , wherein the motion sensor is secured within an interior cabin of the vehicle.5. The display adaptation system of claim 1 , further comprising an impulse response determination control unit in communication with the motion-compensating control unit claim 1 , wherein the impulse response determination control ...

Virtual star illumination in a cabin of an aircraft and cabin attendant signal in such cabin

The invention relates to a display device for an aircraft cabin, comprising a display adapted to display a plurality of stars. A further aspect of the invention is an aircraft cabin comprising such a display device and an aircraft cabin wall compartment comprising a plurality of wall sections and a plurality of light emitting means for individually illuminating each wall section, wherein said wall sections and said light emitting means form such a display device. According to the invention, said display is adapted to display a plurality of stars.

AIRCRAFT SEATING UNIT WITH FIXTURE MEMBER

The invention relates to an aircraft passenger service arrangement comprising one or more passenger service units for arrangement above a passenger seat, and a fixture member. The passenger service arrangement is characterized in that the fixture member is adapted for directly fixing the passenger service unit to a passenger seat in a defined relationship to each other. Further the invention relates to a seating device comprising an aircraft passenger service arrangement. 1. Aircraft passenger service arrangement , comprising:one or more passenger service units for arrangement above a passenger seat and a fixture member,wherein the fixture member is adapted for directly fixing the passenger service unit to a passenger seat in a defined relationship to each other.2. Arrangement as claimed in claim 1 , wherein the passenger service unit comprises an emergency oxygen device.3. Arrangement as claimed in claim 1 ,wherein the passenger service unit comprises any one or more of the following components: a reading light, a cabin attendant call switch and signal, a ventilation nozzle, a passenger entertainment device like a display and/or a loudspeaker.4. Arrangement as claimed in claim 1 ,wherein the fixture member comprises one or more of the following components: a reading light, a cabin attendant call switch and signal, a ventilation nozzle, a passenger entertainment device like a display and a loudspeaker.5. Arrangement as claimed in claim 1 , wherein the fixture member is substantially stiff.6. Arrangement as claimed in claim 1 , wherein the fixture member has a first end and a second end claim 1 , the first end is adapted to be connected to a respective passenger seat and the second end being connected to the passenger service unit.7. Arrangement as claimed in claim 6 , wherein the first end comprises first connecting means to be mountable against a respective passenger seat claim 6 , wherein the first connecting means is a screw means.8. Arrangement as claimed in ...

Apparatus for Providing External Panoramic View Contents for Aircraft During Flight

Provided is an apparatus for providing external panoramic view contents for an aircraft during flight by installing a plurality of cameras in a plurality of windows installed in an aircraft for displaying external panoramic views inside the aircraft while the aircraft flies in order for aircraft passengers to enjoy them. The apparatus includes a shooting unit having a plurality of cameras for shooting aircraft's external panoramic views; a control unit for receiving a plurality of images from the cameras and processing them; and a display unit comprising a single display and a multi-display including a plurality of sub-displays. 1. An apparatus for providing external panoramic view contents for an aircraft during flight , including:{'b': 110', '130', '120, 'a shooting unit ; a display unit ; and a control unit ,'}{'b': 110', '112', '114', '116, 'wherein the shooting unit includes a plurality of cameras , , each of which is installed in each of a plurality of windows installed in an aircraft for shooting its external panoramic views;'}{'b': 130', '132', '134', '134, 'the display unit includes a single display and a multi-display which includes a plurality of sub-displays, wherein the multi-display , having a flexible display, is installed in the space between the windows and the ceiling inside an aircraft cabin; and'}{'b': 120', '110', '130', '110', '130', '112', '114', '116', '134, 'the control unit , being connected to the shooting unit and the display unit , controls the shooting unit and the display unit , receives a plurality of images taken by the cameras , , , thereby, through the multi-display installed in the space between the windows and the ceiling inside the aircraft cabin, and provides the images being taken by the cameras installed in a plurality of the windows adjacent to the corresponding space in the form of a panoramic view.'}2112114116120. The apparatus for providing external panoramic view contents for an aircraft during flight of claim 1 , ...

VEHICLE SEAT POWERED BY FUEL CELL

A seat for passenger vehicles, such as an aircraft seat, that is individually fitted with a fuel cell () positioned in a fuel cell storage portion provided on the seat base, enabling the seat to be fully autonomous and freely placed in the cabin or vehicle independently of any connection to any other seat or to any aircraft power features. Conduits deliver energy, heat, water, oxygen depleted air, or any combination thereof from the fuel cell () to areas of the seat. 1. An individual seat for a passenger transport vehicle , comprising:(a) a seat back, a seat pan, and a seat base,(b) a fuel cell storage portion provided on the seat base,(c) conduits configured to deliver energy, heat, water, oxygen depleted air, or any combination thereof from a fuel cell positioned in the fuel cell storage portion to areas of the seat.2. The individual seat of claim 1 , wherein the seat back claim 1 , the seat pan claim 1 , or both comprise conduits containing a thermal conductor claim 1 , and wherein heat generated from the fuel cell is transferred to the conduits to warm the seat.3. The individual seat of claim 1 , wherein the seat comprises a water mister and wherein water generated from the fuel cell is transferred to the water mister.4. The individual seat of claim 3 , wherein oxygen depleted air from the fuel cell is transferred to the water mister to pressurize the water.5. The individual seat of claim 1 , wherein water and oxygen depleted air from the fuel cell are used to clean an inflight entertainment screen.6. The individual seat of claim 1 , wherein the seat is mounted on-board a passenger aircraft. This application claims the benefit of U.S. Provisional Application Ser. No. 61/612,489, filed Mar. 19, 2012, titled “Seat With Fuel Cell,” the entire contents of which are hereby incorporated by reference.Embodiments of the present invention relate generally to seats, and particularly to seats positioned on-board passenger transport vehicles, that have various features and ...

Self-adjusting door jamb for an aircraft door

The disclosed embodiments relate to an aircraft having an interior door with a self-adjusting door jamb. The self-adjusting door jamb includes a door jamb configured to receive the interior door and a bias mechanism coupled to the door jamb and facilitating movement of the door jamb along an axis. Additionally, an angular translating mechanism coupled to the bias mechanism and facilitating angular displacement of the door jamb relative to the axis.

AIRCRAFT PASSENGER RESTRAINT SYSTEM WITH THREE-POINT SEAT BELT AND STRUCTURAL MOUNTED AIRBAG

An aircraft passenger restraint and protection system including an aircraft seat mounted at an oblique angle to a direction of forward travel, a multi-point seat belt associated with the aircraft seat, and a structural mounted airbag located forward of the aircraft seat. 1. An aircraft passenger restraint and protection system , comprising:an aircraft seat mounted at an oblique angle to a direction of forward travel;a multi-point seat belt associated with the aircraft seat; anda structural mounted airbag located forward of the aircraft seat.2. The aircraft passenger restraint and protection system according to claim 1 , wherein the airbag is configured to deploy in response to a rapid deceleration event and cover an impact zone of a passenger's head and upper body.3. The aircraft passenger restraint and protection system according to claim 1 , wherein the aircraft seat is mounted at an angle from 1 to 90 degrees from a direction of forward travel.4. The aircraft passenger restraint and protection system according to claim 1 , wherein the aircraft seat is mounted at an angle from 15 to 45 degrees from a direction of forward travel.5. The aircraft passenger restraint and protection system according to claim 1 , wherein the multi-point seat belt is a three-point seat belt having a lap belt and a shoulder belt.6. The aircraft passenger restraint and protection system according to claim 1 , wherein the airbag is mounted within a partition wall located forward of the aircraft seat.7. The aircraft passenger restraint and protection system according to claim 1 , wherein the airbag is a passive inflatable restraint triggered to deploy by a battery powered crash sensor configured to fire after a threshold of a dynamic impact is registered by a mechanical crash sensor unit.8. The aircraft passenger restraint and protection system according to claim 1 , wherein the airbag inflates to cover portions of a partition wall directly forward of and to one side of the aircraft seat ...

VEHICLE SEAT COMPRISING INTEGRATED HOLDER FOR ELECTRONIC DEVICES

A vehicle seat includes a backrest, a recess made in the backrest, a holder base fitted to a rear wall of the recess, an upper holder clip which is movably and resiliently mounted in a clip rail extending vertically from top to bottom in the holder base, and a fold-out tray which can be folded out from the recess by two folding hinges which are fitted to the inner side walls of the recess inside the recess. 1. A vehicle seat comprising:a backrest;a recess made in the backrest;a holder base fitted to a rear wall of the recess;an upper holder clip which is movably and resiliently mounted in a clip rail extending vertically from top to bottom in the holder base; anda fold-out tray which can be folded out from the recess by two folding hinges which are fitted to the inner side walls of the recess inside the recess.2. The vehicle seat according to claim 1 , wherein the fold-out tray comprises a tray holder groove which is formed above the lower edge of the fold-out tray either completely or in part claim 1 , and is generally U-shaped.3. The vehicle seat according to claim 2 , wherein the tray holder groove is U-shaped.4. The vehicle seat according to claim 2 , wherein the tray holder groove comprises one or more connection through-openings.5. The vehicle seat according to claim 1 , wherein the recess is a hollow having a rectangular or square cross-sectional area and a predetermined depth in the backrest.6. The vehicle seat according to claim 1 , wherein the upper holder clip is a clamp having a U-shaped latching hook which protrudes forwards from the holder base.7. The vehicle seat according to claim 6 , wherein the holder base further comprises a lower holder clip having a U-shaped latching hook which protrudes forwards from the holder base.8. The vehicle seat according to claim 7 , wherein the lower holder clip is arranged so as to be a horizontal mirror image of the latching hook of the upper holder clip.9. The vehicle seat according to claim 1 , further comprising:a ...

INTEGRATED CENTERLINE LAVATORY GALLEY MONUMENT

A monument configured to be positioned in the interior of an aircraft that includes first, second, third and fourth sides and first and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side. The first and second sides are opposite to one another and the third and fourth sides are opposite to one another. The first lavatory defines a first lavatory interior and includes a first toilet therein and the second lavatory defines a second lavatory interior and includes a second toilet therein. 1. A monument configured to be positioned in the interior of an aircraft , the monument comprising:first, second, third and fourth sides, wherein the first and second sides are opposite to one another and the third and fourth sides are opposite to one another, andfirst and second lavatories spaced apart from one another by at least a portion of a galley storage section that is open to the first side, wherein the first lavatory defines a first lavatory interior and includes a first toilet therein, and wherein the second lavatory defines a second lavatory interior and includes a second toilet therein.2. The monument of wherein the first lavatory includes a door positioned on the third side and the second lavatory includes a door positioned on the fourth side.3. The monument of wherein the galley storage section includes a trolley cart storage area claim 1 , such that a trolley cart stored in the trolley cart storage area is positioned between the first and second lavatories.4. The monument of wherein the galley storage area includes an insert storage strip that is positioned above at least a portion of the first and second lavatories.5. The monument of wherein the insert storage strip is also positioned above the trolley cart storage area.6. The monument of wherein the galley storage section includes a shelf positioned above and at least partially defining the trolley cart storage area.7. The monument of further ...

Aircraft Interior Structure Including Actuatable Panels and a Footwell

An aircraft interior structure may include a primary monument, an auxiliary monument, and a passenger seating section. The primary monument may include one or more storage compartments and a primary panel configured to actuate between a primary panel stowed position and a primary panel deployed position. The auxiliary monument may be spaced a select distance from the primary monument across a floor area of an aircraft cabin, and may include an auxiliary panel configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position. The passenger seating section may include a footwell at least partially within the primary monument and proximate to the one or more storage compartments. The footwell may correspond to an aircraft seat. The aircraft seat may be configured to form a bed surface with at least a portion being within the footwell when the aircraft seat is in a lie-flat position. 1. An aircraft interior structure , comprising:a primary monument, the primary monument including a primary panel and one or more storage compartments, the primary panel being configured to actuate between a primary panel stowed position and a primary panel deployed position;an auxiliary monument spaced a select distance from the primary monument across a floor area of an aircraft cabin, the auxiliary monument including an auxiliary panel, the auxiliary panel being configured to actuate between an auxiliary panel stowed position and an auxiliary panel deployed position; anda passenger seating section proximate to a passenger compartment, the passenger seating section including a footwell, the footwell being at least partially within the primary monument and proximate to the one or more storage compartments, the footwell corresponding to an aircraft seat within the passenger compartment, the aircraft seat being configured to form a bed surface when the aircraft seat is in a lie-flat position, at least a portion of the bed surface being within the ...

SANITIZING GALLEY CART FOR AN INTERNAL CABIN OF A VEHICLE

A galley cart is for use within an internal cabin of a vehicle. The galley cart is configured to be stored within a cart compartment within a galley of the internal cabin. The galley cart includes one or more ultraviolet (UV) light sources configured to emit UV light onto one or more surfaces of one or more components within the internal cabin to sanitize the one or more surfaces. 1. A galley cart for use within an internal cabin of a vehicle , wherein the galley cart is configured to be stored within a cart compartment within a galley of the internal cabin , the galley cart comprising:one or more ultraviolet (UV) light sources configured to emit UV light onto one or more surfaces of one or more components within the internal cabin to sanitize the one or more surfaces.2. The galley cart of claim 1 , wherein the galley cart comprises:a base;wheels extending downwardly from the base;end walls extending upwardly from the base;lateral walls extending upwardly from the base; anda top wall connected to the end walls and the lateral walls opposite from the base,wherein an internal chamber is defined between the base, the end walls, the lateral walls, and the top wall.3. The galley cart of claim 2 , wherein the one or more UV light sources are within the internal chamber.4. The galley cart of claim 3 , wherein one or more of the base claim 3 , the end walls claim 3 , the lateral walls claim 3 , and the top wall include one or more transparent portions that allow the UV light emitted by the one or more UV light sources to pass.5. The galley cart of claim 2 , further comprising:a mount coupled to the one or more UV light sources; andan actuator operatively coupled to the mount, wherein the actuator is configured to move the one or more UV light sources between a stowed position within the internal chamber and an extended position outside of the internal chamber.6. The galley cart of claim 2 , wherein the one or more UV light sources are secured to one or more exterior ...

INTEGRATED CURTAIN SYSTEM AND METHOD

A curtain system may include a track system configured to be mounted to an interior structure of a vehicle. The track system may include three or more track sections oriented in at least two different directions. Each track section may be configured to support at least one curtain suspended from and slidable along the track sections. The track system may include at least one junction fitting interconnecting three or more track sections and allowing movement of a curtain from one of the three or more track sections to either one of two or more other track sections of the three or more track sections. In this regard, the junction fitting and the track sections may define different curtain paths for the curtain. 1. A curtain system for a vehicle interior , comprising: three or more track sections oriented in at least two different directions, at least one of the track sections configured to support at least one curtain suspended from and slidable along the track sections;', 'a junction fitting interconnecting the three or more track sections and allowing movement of the curtain from one of the three or more track sections to either one of two or more other track sections of the three or more track sections; and', 'the junction fitting and the track sections defining different curtain paths for the curtain., 'a track system configured to be mounted to an interior structure of a vehicle and including2. The curtain system of claim 1 , wherein:at least a portion of the track system is suspended from one or more track supports extending downwardly from a cabin ceiling of the vehicle.3. The curtain system of claim 1 , wherein:the junction fitting includes a plurality of fitting legs; andat least one of the fitting legs is oriented in non-perpendicular relation and in non-parallel relation to one or more other fitting legs of the junction fitting.4. The curtain system of claim 1 , wherein:the junction fitting is configured to support two separate curtains in side-by-side ...