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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Применить Всего найдено 5. Отображено 5.
02-02-2012 дата публикации

FUSELAGE STRUCTURE MADE OF COMPOSITE MATERIAL

Номер: US20120025022A1
Автор: Wolfgang Buchs, Gabriele Dreher, Umberto Girard, Steffen Kunze, Thomas Thiess, BUCHS WOLFGANG, DREHER GABRIELE, GIRARD UMBERTO, KUNZE STEFFEN, THIESS THOMAS
Принадлежит: EUROCOPTER DEUTSCHLAND GMBH

A fuselage structure, particularly an aircraft door ( 1 ) of composite material comprising at least one panel ( 2 ) and at least one beam ( 3 ) mounted to each other and the panel ( 2 ) with the panel ( 2 ) being formed of at least one group of composite layers ( 5, 6, 20 ). The at least one beam ( 3 ) is provided at least at one of its respective ends ( 10, 11 ) with a flange ( 13 ) suitable for adhesive engagement with the at least one panel ( 2 ). The at least one group of composite layers ( 5, 6, 20 ) of the panel ( 2 ) is in form locking engagement with this flange ( 13 ) of the beam ( 3 ).

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Номер записи: 1
07-01-2014 дата публикации

Fuselage structure made of composite material

Номер: US0008622346B2
Автор: Wolfgang Buchs, Gabriele Dreher, Umberto Girard, Steffen Kunze, Thomas Thiess, BUCHS WOLFGANG, DREHER GABRIELE, GIRARD UMBERTO, KUNZE STEFFEN, THIESS THOMAS
Принадлежит: Eurocopter Deutschland GmbH, BUCHS WOLFGANG, DREHER GABRIELE, GIRARD UMBERTO, KUNZE STEFFEN, THIESS THOMAS, EUROCOPTER DEUTSCHLAND, EUROCOPTER DEUTSCHLAND GMBH

A fuselage structure, particularly an aircraft door (1) of composite material comprising at least one panel (2) and at least one beam (3) mounted to each other and the panel (2) with the panel (2) being formed of at least one group of composite layers (5, 6, 20). The at least one beam (3) is provided at least at one of its respective ends (10, 11) with a flange (13) suitable for adhesive engagement with the at least one panel (2). The at least one group of composite layers (5, 6, 20) of the panel (2) is in form locking engagement with this flange (13) of the beam (3).

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Номер записи: 2
21-12-2021 дата публикации

Mounting system for a pressure seal of an aircraft door

Номер: US0011203406B2
Автор: Thomas Hackenberg, Thomas Thiess, Dirk Trott
Принадлежит: AIRBUS HELICOPTERS DEUTSCHLAND GMBH

An aircraft door, and, more particularly, to a mounting system for a pressure seal of an aircraft door. A mounting system may include an outer skin, a pressure seal, a clamping component, a pressure seal fastener having a head and a threaded shank, a nut, a mounting support having a clearance hole that is adapted to prevent a rotational and axial movement of the pressure seal fastener, and mounting support fasteners. Mounting support fasteners removably attach the mounting support to the outer skin. The head of the pressure seal fastener is connected to the mounting support such that a rotational and axial movement of the pressure seal fastener is prevented. The nut is removably attached to the threaded shank of the pressure seal fastener, thereby removably clamping the pressure seal between the clamping component and the mounting support.

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Номер записи: 3
27-02-2020 дата публикации

Mounting system for a pressure seal of an aircraft door

Номер: US20200062371A1
Автор: Dirk Trott, Thomas HACKENBERG, Thomas Thiess
Принадлежит: AIRBUS HELICOPTERS DEUTSCHLAND GMBH

An aircraft door, and, more particularly, to a mounting system for a pressure seal of an aircraft door. A mounting system may include an outer skin, a pressure seal, a clamping component, a pressure seal fastener having a head and a threaded shank, a nut, a mounting support having a clearance hole that is adapted to prevent a rotational and axial movement of the pressure seal fastener, and mounting support fasteners. Mounting support fasteners removably attach the mounting support to the outer skin. The head of the pressure seal fastener is connected to the mounting support such that a rotational and axial movement of the pressure seal fastener is prevented. The nut is removably attached to the threaded shank of the pressure seal fastener, thereby removably clamping the pressure seal between the clamping component and the mounting support.

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Номер записи: 4
02-02-2012 дата публикации

Fuselage structure made of composite material

Номер: CA2743372A1
Автор: Gabriele Dreher, Steffen Kunze, Thomas Thiess, Umberto Girard, Wolfgang Buchs
Принадлежит: EUROCOPTER DEUTSCHLAND GMBH

The present invention relates to a fuselage structure, particularly an aircraft door of composite material comprising at least one panel and at least one beam mounted to each other and the panel with the panel being formed of at least one group of composite layers. The at least one beam is provided at least at one of its respective ends with a flange suitable for adhesive engagement with the at least one panel. The at least one group of composite layers of the panel is in form locking engagement with this flange of the beam.

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Номер записи: 5