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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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Мониторинг СМИ

Мониторинг СМИ и социальных сетей. Сканирование интернета, новостных сайтов, специализированных контентных площадок на базе мессенджеров. Гибкие настройки фильтров и первоначальных источников.

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Форма поиска

Поддерживает ввод нескольких поисковых фраз (по одной на строку). При поиске обеспечивает поддержку морфологии русского и английского языка
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Применить Всего найдено 30839. Отображено 100.
05-01-2012 дата публикации

Process of producing light-reflective film and light-reflective film

Номер: US20120002125A1
Автор: Kazuhiro Oki
Принадлежит: Fujifilm Corp

A process for producing a light-reflective film is disclosed. The process comprises (a) applying a curable liquid crystal composition to a first film having a thickness of d 1 ; (b) drying the applied curable liquid crystal composition to form a cholesteric liquid crystal phase; (c) carrying out a curing reaction of the curable liquid crystal composition and fixing the cholesteric liquid crystal phase to form a lower layer; (d) repeating the set of the steps (a)-(c) three or more times on the lower layer to form a light-reflective multilayer having four or more layers of a fixed cholesteric liquid crystal phase; and (e) transferring the light-reflective multilayer, formed on the first film, onto a second film having a thickness of d 2 which is smaller than d 1 ; wherein the first film, fulfilling the condition of formula (1), is used. ( d 1 ) 2 × ( Y 1 ) ( d 3 ) × ( 1 - P 1 ) ≧ 0.0002 ( 1 )

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10-11-2011 дата публикации

Гибкое изделие плоской формы

Номер: RU0000110097U1

1. Гибкое изделие плоской формы, в частности, для облицовки частей внутреннего оборудования транспортных средств, которое, по меньшей мере, частично снабжено тисненым узором, причем лицевая верхняя сторона выполнена из текстильного слоя (1), который плохо поддается тиснению, отличающееся тем, что текстильный слой (1) наклеен на кожаную оболочку (7) и вместе с ней подвергнут тиснению. ! 2. Гибкое изделие плоской формы по п.1, отличающееся тем, что текстильный слой (1) уменьшен по толщине в результате разделения на два слоя. ! 3. Гибкое изделие плоской формы по п.1 или 2, отличающееся тем, что толщина полученного после наклеивания текстильного слоя (1) на кожаную оболочку (7) композитного материала (10) уменьшена с помощью разделения на два слоя. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) 110 097 (13) U1 (51) МПК D06N 7/00 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ, ПАТЕНТАМ И ТОВАРНЫМ ЗНАКАМ (12) ТИТУЛЬНЫЙ ЛИСТ ОПИСАНИЯ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (21)(22) Заявка: 2011105088/05, 14.02.2011 (24) Дата начала отсчета срока действия патента: 14.02.2011 (73) Патентообладатель(и): Др. Инж. х.к. Ф. Порше Акциенгезелльшафт (DE) (45) Опубликовано: 10.11.2011 Бюл. № 31 1 1 0 0 9 7 R U (57) Формула полезной модели 1. Гибкое изделие плоской формы, в частности, для облицовки частей внутреннего оборудования транспортных средств, которое, по меньшей мере, частично снабжено тисненым узором, причем лицевая верхняя сторона выполнена из текстильного слоя (1), который плохо поддается тиснению, отличающееся тем, что текстильный слой (1) наклеен на кожаную оболочку (7) и вместе с ней подвергнут тиснению. 2. Гибкое изделие плоской формы по п.1, отличающееся тем, что текстильный слой (1) уменьшен по толщине в результате разделения на два слоя. 3. Гибкое изделие плоской формы по п.1 или 2, отличающееся тем, что толщина полученного после наклеивания текстильного слоя (1) на кожаную оболочку (7) композитного материала (10) уменьшена с помощью разделения на два слоя. Ñòð.: 1 ru U 1 U 1 ...

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12-09-2019 дата публикации

Крыша транспортного средства

Номер: RU0000192308U1
Принадлежит: АГК ГЛАСС ЮРОП

Полезная модель относится к ламинированной стеклянной крыше автомобиля, обладающей различной светопроницаемостью и обеспечивающей улучшенный комфорт с точки зрения температуры, содержащей два стеклянных листа, т.е. наружный и внутренний стеклянные листы, которые соединены вместе посредством промежуточных слоев из термопластика, сборку пленок устройства на основе взвешенных частиц (SPD) для управления светопроницаемостью, которая встроена в ламинат между двумя стеклянными листами, и систему низкоэмиссионных слоев, расположенных на позиции 4. РОССИЙСКАЯ ФЕДЕРАЦИЯ (19) RU (11) (13) 192 308 U1 (51) МПК B32B 17/10 (2006.01) B62D 25/06 (2006.01) ФЕДЕРАЛЬНАЯ СЛУЖБА ПО ИНТЕЛЛЕКТУАЛЬНОЙ СОБСТВЕННОСТИ (12) ОПИСАНИЕ ПОЛЕЗНОЙ МОДЕЛИ К ПАТЕНТУ (52) СПК B32B 17/10036 (2019.05); B32B 17/10229 (2019.05); B62D 25/06 (2019.05) (21)(22) Заявка: 2019117067, 12.06.2013 (24) Дата начала отсчета срока действия патента: (73) Патентообладатель(и): АГК ГЛАСС ЮРОП (BE) Дата регистрации: 12.09.2019 19.06.2012 BE BE2012/0412 (45) Опубликовано: 12.09.2019 Бюл. № 26 1 9 2 3 0 8 R U (54) КРЫША ТРАНСПОРТНОГО СРЕДСТВА (57) Реферат: Полезная модель относится к ламинированной стеклянной крыше автомобиля, обладающей различной светопроницаемостью и обеспечивающей улучшенный комфорт с точки зрения температуры, содержащей два стеклянных листа, т.е. наружный и внутренний стеклянные листы, которые соединены вместе посредством Стр.: 1 промежуточных слоев из термопластика, сборку пленок устройства на основе взвешенных частиц (SPD) для управления светопроницаемостью, которая встроена в ламинат между двумя стеклянными листами, и систему низкоэмиссионных слоев, расположенных на позиции 4. U 1 U 1 Адрес для переписки: 105064, Москва, а/я 88, "Патентные поверенные Квашнин, Сапельников и партнеры" 1 9 2 3 0 8 (56) Список документов, цитированных в отчете о поиске: US 2010/0165436 A1, 01.07.2010. EP 1200256 A1, 02.05.2002. US 2004124665 A1, 01.07.2004. WO 2011033313 A1, 24.03.2011. Приоритет(ы): (30) Конвенционный ...

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12-01-2012 дата публикации

Snap In Weatherstripping

Номер: US20120009378A1
Принадлежит: GREENSTAR TECHNOLOGIES LLC

A snap in weatherstripping where the backing has a plurality of alternating notched out spaces along each side to facilitate ease of insertion into a channel without the need to slide the weatherstripping longitudinally into the channel. The snap in weatherstripping can be pushed into the channel with a gentle side to side or rolling motion, thus eliminating the difficulties associated with longitudinally sliding a weatherstripping into a channel. The snap in arrangement of the weatherstripping eases replacement, and also accommodates variations in tolerance between the weatherstripping and the channel, making it desirable for replacement of existing degraded weatherstripping.

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19-01-2012 дата публикации

Antistaining sheet

Номер: US20120015165A1
Автор: Noriaki Ogawa
Принадлежит: Daiwabo Holdings Co Ltd, Kanbo Pras Corp

Disclosed is an antistaining sheet including a base material sheet and an antistaining layer formed on the base material sheet. The antistaining layer includes a photocatalyst and a thermoplastic resin to be decomposed by the photocatalyst, and thus has a self-collapsing property. The antistaining layer is stronger in self-collapsing property in the surface portion thereof than in the interior portion.

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26-01-2012 дата публикации

Exhaust system

Номер: US20120017565A1
Автор: Gerd Gaiser
Принадлежит: Individual

A component of an exhaust system for a combustion engine, particularly of a motor vehicle, which at least in part regions includes a self-supporting jacket. The jacket includes a porous, open-pore or closed-pore cellularly constructed foam. The foam is of a self-supporting design. By using such a foam the insulation of the component can be improved.

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26-01-2012 дата публикации

Transparent Multilayered Carbonate Articles and Method to Manufacture Thereof

Номер: US20120019906A1
Принадлежит: Individual

Disclosed is a transparent multilayer article comprising a core layer comprising a thermoplastic carbonate polymer; a first layer comprising a carbonate thermoplastic polymer and an infrared (IR) absorbing additive; and a second layer comprising a thermoplastic carbonate polymer and a ultraviolet (UV) absorbing stabilizer, wherein the first layer does not contain an UV absorbing additive and the second layer does not contain an IR absorbing additive. Disclosed herein too, is a method for manufacturing a transparent multilayer article comprising melt blending a first thermoplastic carbonate polymer composition to produce a core layer; melt blending a second thermoplastic carbonate polymer composition with an IR absorbing additive to produce a first layer; and melt blending a third thermoplastic carbonate polymer composition with an UV absorbing stabilizer; combining the core layer, first layer, and second layer such that the first layer is disposed between the core layer and the second layer such that a first surface of the first layer is in intimate contact with a first surface of the core layer and a second surface of the first layer is in intimate contact with a first surface of the second layer.

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02-02-2012 дата публикации

Self-Tearing Interior Wrap

Номер: US20120025566A1
Принадлежит: Faurecia Interior Systems Inc

A self-tearing wrap and methods for its manufacture are disclosed, the wrap being useful for incorporation onto interior trim panels. The wrap includes an unscored skin such as leather affixed to a foam layer made of an open or closed cell foam material having specific properties. Interior trim panels including the self-tearing leather wrap may include weakened substrates operable to facilitate the deployment of an airbag.

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02-02-2012 дата публикации

Laminated, transparent set of panes, process for producing and bending same, and use thereof

Номер: US20120028015A1
Принадлежит: SCHOTT AG

Laminated, transparent set of panes made of brittle materials and interleaved laminated films, wherein the brittle materials are various glasses, special glasses, glass-ceramics, transparent ceramics and crystalline materials, process for producing and bending the set of panes and films, and its use thereof, as a bulletproof, unbreakable and shockproof glazing with a low weight per unit area.

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16-02-2012 дата публикации

Machinable composite material

Номер: US20120040169A1
Автор: Bruno Boursier
Принадлежит: Hexcel Corp

An assembly that includes a first part composed of a fibrous structure that includes fibers and a cured resin matrix. The fibrous structure has at least one surface and a layer that is located on the surface. The layer includes a discontinuous fiber composite that is composed of randomly oriented short fibers and a cured resin matrix wherein the layer has been machined to provide a machined surface. The assembly also includes a second part that is attached to the first part. The second part includes at least one surface that fits against the machined surface on the first part.

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16-02-2012 дата публикации

Low density coring material

Номер: US20120040173A1
Принадлежит: ILLINOIS TOOL WORKS INC

A low density coring material is described. In one embodiment, the low density coring material consists essentially of: about 40 to about 80 wt % resin; 0 to about 50 wt % monomer; 0 to about 5 wt % dispersion aid; 0 to about 5 wt % accelerator; about 3 to about 7 wt % microspheres; and about 1 to about 5 wt % catalyst; wherein a density of the cured coring material is less than about 5.0 lbs/gal. Composites made using the low density coring material and methods of making composites are also described.

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15-03-2012 дата публикации

Honeycomb packing system, method and apparatus

Номер: US20120065757A1
Принадлежит: SPIDRPAK Inc

A system and method of forming a honeycomb structure includes selecting a desired honeycomb structure shape, forming a plurality of two dimensional sheets into desired two dimensional shapes corresponding to the selected honeycomb structure shape, stacking the plurality of two dimensional sheets, connecting the plurality of two dimensionally shaped sheets along corresponding connection lines and spreading the plurality of sheets apart.

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22-03-2012 дата публикации

Hybrid components with reactive hotmelt adhesives

Номер: US20120070670A1
Принадлежит: EVONIK DEGUSSA GmbH

A description is given of the use of reactive hotmelt adhesives based on copolyamide and further comprising isocyanate and epoxide and also a functionalized polyolefin in hybrid components. These hybrid components find applications in vehicle construction and in aircraft construction, for example.

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29-03-2012 дата публикации

Multilayered cellular metallic glass structures

Номер: US20120077052A1

Multi-layered cellular metallic glass structures and methods of preparing the same are provided. In one embodiment, the cellular metallic glass structure includes at least one patterned metallic glass sheet and at least one additional sheet. The at least one patterned metallic glass sheet may include multiple sheets connected together to form a group of sheets, and the structure may include a group of sheets sandwiched between two outer sheets. The patterned metallic glass sheets may be patterned by thermoplastically forming two- and/or three-dimensional patterns in the metallic glass sheets. The metallic glass cellular structures are useful in a wide variety of applications, including but not limited to blast protection applications, energy absorption applications, structural support applications, biomedical implant applications, heat exchanger applications, thermal management applications, electrical shielding applications, magnetic shielding applications, and debris and radial

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19-04-2012 дата публикации

Porous anti-slip floor covering

Номер: US20120094057A1
Автор: Joel Patrick Bartlett
Принадлежит: Individual

A flooring assembly and method of manufacturing a flooring assembly includes forming a. working surface by depositing a plurality of heated flexible strands of material onto a surface and cooling the plurality of heated flexible strands so that a first end of each strand is directly physically coupled to a first end of at least one other strand in the plurality of strands so that the coupled first ends of the plurality of strands define a plurality of openings and a second end, opposite the first end, of each strand is physically independent from each second end of each of the strands in the plurality of strands so that each second end of each strand is able to move independent of the second end of each other strand. The method further includes providing a mesh underlayment having an upper surface, an opposing lower surface, and defining a plurality of openings spanning from the upper surface to the lower surface and permanently adhering the coupled first ends of the plurality of strands to the upper surface of the underlayment.

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24-05-2012 дата публикации

Part comprising an insert and a plastic sheathing and method for the production thereof

Номер: US20120128919A1
Принадлежит: BASF SE

The invention relates to a component comprising an insert part and plastics jacketing composed of at least two plastics components, where the insert part is enclosed by a first plastics component A and there is a second plastics component B enclosing the first plastics component A. The first plastics component A is composed of: A1: from 10 to 100% by weight of at least one thermoplastic styrene (co)polymer and A2: from 0 to 90% by weight of at least one thermoplastic (co)polyester, in each case based on the polymer content of the first plastics component A, and the second plastics component B is composed of B1: from 50 to 100% by weight of at least one semicrystalline, thermoplastic polyester based on aromatic dicarboxylic acids and on aliphatic or aromatic dihydroxy compounds and B2: from 0 to 50% by weight of at least one thermoplastic styrene (co)polymer, in each case based on the polymer content of the second plastics component B, and where the first plastics component A and the second plastics component B have different constitutions. The invention further relates to a process for the production of the component.

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31-05-2012 дата публикации

Composite airfoil and turbine engine

Номер: US20120134839A1
Принадлежит: Individual

A composite airfoil includes a core that has a three-dimensional network of fibers. The core defines an airfoil section and a root section. A composite skin covers a portion of the core excluding the root section.

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07-06-2012 дата публикации

Wrinkle Control for Composite Tubes

Номер: US20120141705A1
Принадлежит: Boeing Co

In one step of a method of fabricating a composite tube, layers of uncured composite material may be laid over a surface. In another step, spaced-apart strips of at least one of uncured, partially cured, and completely cured composite material may be laid lengthwise over the laid layers of composite material. In still another step, the spaced-apart strips may be compacted against the layers of uncured composite material. In an additional step, the compacted spaced-apart strips and the layers of uncured composite material may be further consolidated and/or cured to form a composite tube.

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14-06-2012 дата публикации

Method for Fabrication of Integrated Lightning Strike Protection Material

Номер: US20120145319A1
Принадлежит: Boeing Co

The invention is directed to an integrated lightning strike protection system adapted for automated placement on a composite structure having a surfacing layer consisting of an organic polymer resin, a conductive layer of an expanded metal foil, an isolation/tack layer, and a carrier paper layer. In another embodiment of the invention, there is provided an integrated lightning strike protection system having an integrated lightning strike protection material consisting of an expanded metal foil encapsulated in organic polymer resin mounted on a carrier paper, and an automated placement machine suitable for placing the material on an aircraft composite part for protection of the composite part from lightning strikes. In another embodiment of the invention, there is provided a method for fabricating a composite structure with lightning strike protection.

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28-06-2012 дата публикации

Dressed headliner for vehicles with a finished perimeter and a method for obtaining it

Номер: US20120161478A1
Принадлежит: Grupo Antolin Ingenieria SA

The invention relates to a dressed headliner for vehicles with a finished perimeter and a method for obtaining it method, without the addition of any adhesive or joining means where the finished perimeter obtained is a high quality finished perimeter with sharp contour.

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28-06-2012 дата публикации

In-mold coated articles having controlled surface morphology and associated methods for manufacturing same

Номер: US20120164381A1
Автор: Brodie Wright, Paul Morgan
Принадлежит: Individual

An in-mold coated article that includes at least one of a controlled surface morphology and a predetermined color which is manufactured via a single- or multi-coat process. The in-mold coated article preferably resembles wood, leather, marble, granite, clay, etcetera. The present invention further provides methods for manufacturing in-mold coated articles using single-coat and/or multi-coat processes as disclosed herein.

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12-07-2012 дата публикации

Multi-layered fuel tubing

Номер: US20120177857A1
Принадлежит: Saint Gobain Performance Plastics Corp

The invention describes a flexible tubular article for transport of volatile hydrocarbons comprising: (a) an inner layer of a polyvinylidene difluoride (PVDF) polymer or a polyvinylidene difluoride copolymer; (b) an intermediate thermoplastic polyurethane (TPU) layer extruded in tubular form over the inner PVDF layer, and (c) a polyvinyl chloride polymer extruded in tubular form over the outside surface of the intermediate layer and being coextensive therewith. The tubular articles of the invention have a maximum permeation rating of 15 g/m 2 /day under SAE J1737 test conditions.

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06-09-2012 дата публикации

Transparent or translucent extruded polyamide

Номер: US20120223453A1
Принадлежит: Arkema Inc

The invention relates to a process for forming an extruded transparent or translucent polyamide article including melt calendering to improve the physical properties and optical clarity. The polyamide article is a sheet, film, or profile.

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13-09-2012 дата публикации

Component comprising an insert part and plastics jacketing, and process for production of the component

Номер: US20120231280A1
Принадлежит: BASF SE

The invention relates to a component comprising an insert part and plastics jacketing composed of at least two plastics components, where the insert part is enclosed by a first plastics component A and there is a second plastics component B enclosing the first plastics component A, where the first plastics component A is composed of: A1: from 5 to 80% by weight, based on the total weight of components A1 and A2, of at least one polyester based on aliphatic and aromatic dicarboxylic acids and on aliphatic dihydroxy compounds; A2: from 20 to 95% by weight, based on the total weight of components A1 and A2, of at least one homo- or copolyester selected from the group consisting of polylactide (PLA), polycaprolactone, polyhydroxyalkanoates, and polyester derived from aliphatic dicarboxylic acids and from aliphatic diols; A3: from 0.05 to 15% by weight, based on the total weight of components A1 and A2, a) of a copolymer which contains epoxy groups and which is based on styrene, on acrylate, and/or on methacrylate, b) of a bisphenol A epoxide, or c) of a fatty acid amide or fatty acid ester, or natural oil containing epoxy groups; and the second plastics component B is composed of B1: from 50 to 100% by weight of at least one semicrystalline, thermoplastic polyester based on aromatic dicarboxylic acids and on aliphatic or aromatic dihydroxy compounds and B2: from 0 to 50% by weight of at least one thermoplastic styrene (co)polymer, in each case based on the polymer content of the second plastics component B.

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20-09-2012 дата публикации

Soundproof material for vehicle

Номер: US20120234626A1
Принадлежит: Takehiro Co Ltd

A first sound absorbing material to be located facing a vehicle room interior side, the air-impermeable material having an air-impermeable film having bonding hot-melts on both sides thereof, and the second sound absorbing material to be located facing a vehicle room exterior side are laminated in this order, and are closely-located between two heating boards and are supplied with hot air to melt hot-melts and thus to make a laminate. The laminate is cold press molded with the first sound absorbing material on a lower mold, and at the same time as the press molding, compressed gas is supplied from an upper mold to apply pressure on the air-impermeable material and thus to compression mold the first sound absorbing material.

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20-09-2012 дата публикации

Moulded trim component for covering an airbag in a motor vehicle

Номер: US20120237712A1
Автор: Peter Thielhorn
Принадлежит: Johnson Controls Technology Co

A molded trim component for covering an airbag in a motor vehicle comprises a support, an intermediate layer, and a decorative layer. The decorative layer is adhesively bonded to the surface of the intermediate layer, at least in the region of a tear-open line of the intermediate layer or at least in the vicinity of the tear-open line.

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04-10-2012 дата публикации

Protective film

Номер: US20120251801A1
Принадлежит: Nexolve Corp

A protective film has a soluble polyimide polymer base layer and an exterior layer directly contacting the base layer exterior surface. The base layer is less than 12 microns thick, and is at least 2 meters long. The exterior layer includes at least one of a fluorinated polymer, a dielectric layer, one or more metallic layers, a metalloid layer, or a plurality of dielectric layers where each dielectric layer has a dielectric layer thickness that varies no more than 3%. The exterior layer or the base layer can also include additives, as desired.

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18-10-2012 дата публикации

Thermal storage medium composition and thermal storage medium

Номер: US20120261607A1
Принадлежит: JSR Corp

[Object] The invention provides a thermal storage medium composition capable of forming a thermal storage medium which is free from phase separation or liquid phase bleeding and is excellent in shape retention properties even at or above the maximum crystal transition temperature of a paraffin compound and further exhibits excellent fluidity when being shaped. [Solution] A thermal storage medium composition includes 100 parts by mass of a hydrogenated diene copolymer and 50 to 4000 parts by mass of a paraffin compound, the hydrogenated diene copolymer being a conjugated diene copolymer that is obtained by hydrogenating a block copolymer which includes a block (A) that contains structural units (a-1) derived from a conjugated diene compound and has a vinyl bond content of not more than 20 mol %, and a block (B) that contains structural units (b-1) derived from a conjugated diene compound and has a vinyl bond content of 30 to 95 mol %, the hydrogenation ratio with respect to the double bonds derived from the conjugated diene compounds being not less than 90%.

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08-11-2012 дата публикации

Panel made of composite material

Номер: US20120282441A1
Принадлежит: Daher Aerospace SAS

A panel is made of composite material comprising a skin made of composite material and having two opposite general sides, and first stiffeners extending over one of the sides of the skin. It is characterised in that it comprises additional stiffeners that are arranged on the side of the skin opposite that bearing the first stiffeners, and which extend in a direction distinct from that of the first stiffeners. The skin and the stiffeners arranged on each side are preferably made integral by co-moulding.

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13-12-2012 дата публикации

Elastomeric Compositions Comprising Reclaimed Vulcanized Elastomer Particles of Broad Size Distribution and Chemically Modified Vulcanized Elastomer Particles

Номер: US20120316283A1
Принадлежит: Individual

Elastomer compositions comprising uncured elastomer and reclaimed elastomer are described. In one embodiment, the compositions comprise reclaimed elastomer material (micronized rubber powder) of broad particle size distribution, which is less expensive than traditional reclaimed elastomer material with narrow particle size distribution. Further, compositions comprising reclaimed elastomer materials with broad particle size distribution perform comparably to those comprising reclaimed elastomer materials with narrow particle size distribution. In other embodiments, the compositions comprise both vulcanized and devulcanized elastomer materials. Advantageously, by using a combination of vulcanized and devulcanized material, it is possible to incorporate a greater percentage by weight of reclaimed material in to an elastomer composition, thus providing additional cost savings while maintaining high levels of mechanical properties. Further, the use of the reclaimed material reduces landfill waste resulting in a more environmentally friendly product.

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10-01-2013 дата публикации

Nylon airbrake tubing constructions

Номер: US20130011595A1
Автор: Nicola Martino
Принадлежит: Parker Hannifin Corp

Single or multilayer tube such as for use as airbrake tubing. At least one of the layers of the tube may be formed of a long-chain polyamide such as nylon 4-10, nylon 6-10, nylon 10-10, nylon 6-12, nylon 10-12, or nylon 12-12, or an alloy thereof.

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17-01-2013 дата публикации

Decorative Decal System for an Aircraft

Номер: US20130015292A1
Принадлежит: Boeing Co

A method and apparatus comprising a layer of material having a decorative graphic and an electrically conductive material in the layer of material. The layer of material is configured to be attached to a surface of an aircraft. The electrically conductive material is configured to cause a current from an atmospheric electrostatic discharge contacting the layer of material to spread out in a desired amount within the layer of material.

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21-02-2013 дата публикации

Non-woven fire barrier mat

Номер: US20130045352A1
Принадлежит: JOHNS MANVILLE

A burnthrough resistant non-woven mat is made of a glass fibers and includes a binder having a vinyl component and a strengthening component. The vinyl component may be, for example, ethylene vinyl chloride, and the strengthening component may be, for example, melamine formaldehyde. The burnthrough resistant non-woven mat may be used in conjunction with an insulation blanket, and may be especially suited to use in insulating aircraft. Methods of making the burnthrough resistant non-woven mat are discussed.

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07-03-2013 дата публикации

Surface Treated Film and/or Laminate

Номер: US20130059120A1
Принадлежит: Avery Dennison Corp

A surface treatment for a protective plastic film and/or laminate is disclosed. Suitably, the surface treatment includes coating a major surface of the plastic film or laminate with a curable coating formulation wherein one or more of the coating ingredients are diffused or migrated at least partially into the plastic film or plastic laminate. The migration of coating ingredients creates a gradual transition layer from the plastic film to the coating layer and leads to unique properties. Optionally, the surface treated plastic film is laminated to a release liner coated with a pressure sensitive adhesive (PSA) to form the aforementioned laminate.

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28-03-2013 дата публикации

High Impact Polymer Layers

Номер: US20130075949A1
Принадлежит: Solutia Inc

Multiple poly(vinyl butyral) layer interlayers that can be used in multiple layer glass panel type applications that require a high level of impact protection, for example in hurricane protection applications or in bullet proof glass applications. This effect is achieved by forming a poly(vinyl butyral) interlayer that has a relatively stiff poly(vinyl butyral) inner layer disposed between two relatively soft outer poly(vinyl butyral) layers, where the stiffness difference is achieved by a plasticizer differential that is achieved at least in substantial part by a residual hydroxyl content difference among the poly(vinyl butyral) layers.

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04-04-2013 дата публикации

Aircraft thermal insulation

Номер: US20130082144A1
Принадлежит: BAE SYSTEMS plc

The invention provides an arrangement and methods for thermally insulating aircraft, particularly but not exclusively for when the aircraft is operating in extremely hot or cold conditions, and describes an aircraft skin construction including a foam-stiffened CFC sandwich panel forming part of the aircraft outer skin mounted to an underlying load bearing aircraft structure, wherein the panel at the mounting to the structure includes two outer layers of CFC material with an inner layer of foam material sandwiched therebetween.

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16-05-2013 дата публикации

Method for Preparing a Modified Ethylene-Vinyl Alcohol Copolymer

Номер: US20130123428A1
Автор: Naoyuki Morooka
Принадлежит: Yokohama Rubber Co Ltd

Ethylene-vinyl alcohol copolymers have superior gas barrier properties, but are inferior in bending fatigue resistance. The present invention improves bending fatigue resistance without reducing the gas barrier property and heat resistance. An ethylene-vinyl alcohol copolymer having an ethylene content of 20 to 50 percent by mole is modified by incorporating 0.01 to 1% mol of a structural unit expressed by the following formula (3): wherein, n indicates an integer of 2 to 5, m indicates an integer of 10 to 20, and R 1 indicates a C 1 to C 20 aliphatic hydrocarbon group provided that R 1 may contain a mercapto group, thioester group, sulfenamide, vinyl group, methacryloxy group, or acryloxy group. The modified ethylene vinyl alcohol copolymer may be used as a gas barrier resin and this gas barrier resin may be shaped or laminated and used in various applications such as in pneumatic tires and hoses.

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20-06-2013 дата публикации

Multilayered sheet

Номер: US20130156984A1
Принадлежит: EI Du Pont de Nemours and Co

This invention is directed to a multilayered sheet comprising a release paper and an inorganic refractory layer coated onto one surface of the release paper wherein the refractory layer has a dry areal weight of from 15 to 50 gsm and a residual moisture content of no greater than 10 percent by weight. The paper comprises a blend of cellulose and cotton fibers and is hydrophilic.

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27-06-2013 дата публикации

Polyurethanes, Articles and Coatings Prepared Therefrom and Methods of Making The Same

Номер: US20130160920A1
Принадлежит: PPG Industries Ohio Inc

The present invention provides polyurethanes including a reaction product of components including: (a) an isocyanate functional urethane prepolymer comprising a reaction product of components including: (i) about 1 equivalent of at least one polyisocyanate; and (ii) about 0.1 to about 0.5 equivalents of at least one diol having 2 to 18 carbon atoms; and (b) about 0.05 to about 0.9 equivalents of at least one branched polyol having 4 to 18 carbon atoms and at least 3 hydroxyl groups; and (c) up to about 0.9 equivalents of at least one polyol different from branched polyol (b) and having 2 to 18 carbon atoms, wherein the reaction product components are essentially free of polyester polyol and polyether polyol; compositions, coatings and articles made therefrom and methods of making the same.

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27-06-2013 дата публикации

Thermoplastic composite prepreg for automated fiber placement

Номер: US20130164498A1
Принадлежит: ADC Acquisition Co

An improved thermoplastic composite prepreg tape is disclosed. The prepreg tape is optimized for high-speed, high quality in-situ consolidation during automated fiber placement. Embodiments of the prepreg tape have uniform dimensions (cross section, width, and thickness), uniform energy absorption, uniform surface roughness, and sufficient resin at the surface to affect a bond between layers.

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08-08-2013 дата публикации

Sound attenuating device using an embedded layer for acoustical tuning

Номер: US20130199871A1
Принадлежит: JANESVILLE ACOUSTICS

The present invention includes a layered acoustical system for sound attenuation in a vehicle including an external decorative layer; a moldable fiber backer adhesively adhered to a back side of the decorative layer, the moldable fiber backer further including an engineered fiber blend including one or more types of thermoplastic fibers and having a first density; a moldable lofted sound absorber and vibration decoupling layer including being made from another engineered fiber blend including one or more types of thermoplastic fibers and having a second density that is less than the first density of the moldable backer, a top side of the vibration decoupling layer being adhesively adhered to the second side of the moldable fiber backer; and an intermediate layer embedded in a location within the vibration decoupling layer to achieve a balance point between transmission loss and sound absorption.

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12-09-2013 дата публикации

Porous anti-slip floor covering

Номер: US20130233228A1
Автор: Joel Patrick Bartlett
Принадлежит: Individual

A marine flooring assembly having a marine vessel having a fixed surface and a floor covering assembly with an underlayment having an upper surface, an opposing lower surface, and defining a plurality of voids extending from the upper surface to the lower surface, the lower surface of the underlayment directly coupled to the fixed surface of the marine vessel, the floor covering assembly also having a working layer disposed on top of the underlayment, the working layer including a plurality of meshed flexible curled strands, each curled strand having at least one portion directly physically coupled to at least one of another curled strand and an upper surface of the underlayment, the plurality of curled strands defining a lower working surface, an upper working surface, and a plurality of openings thereat.

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12-09-2013 дата публикации

Aircraft wing and fiber metal laminate forming part of such an aircraft wing

Номер: US20130233972A1
Принадлежит: Constellium France SAS

Fiber metal laminate ( 4 ) and an aircraft wing ( 1 ) are provided. The laminate comprises metal layers ( 5 ) and fiber reinforced plastic layers ( 6, 7, 6′, 7′; 6″, 1 ″) in between the metal layers ( 5 ) wherein the metal layers ( 5 ) and the fiber reinforced plastic layers ( 6, 7, 6′, 7′; 6″, 1 ″) are bonded together,

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26-09-2013 дата публикации

Pressure Sensitive Adhesive and Adhesive Tape

Номер: US20130251991A1
Принадлежит: 3M Innovative Properties Co

There is provided a pressure sensitive adhesive displaying sufficient adhesive force to the surface of PMMA under a wide range of temperatures including ambient, low, and high temperatures, and also an adhesive tape having an adhesive layer including the pressure sensitive adhesive. There is provided a pressure sensitive adhesive comprising a polymer obtained by polymerizing 100 mass parts of a monomer mixture comprising: a monomer component 1 comprising an acrylate mixture selected from an aliphatic alkyl(meth)acrylate having a carbon number of 4-6 and an aliphatic alkyl(meth)acrylate having a carbon number of 7-12; a monomer component 2 comprising an amide group-containing vinyl monomer; a monomer component 3 comprising an ester of a non-tertial aromatic alcohol and (meth)acrylic acid, or an ester of a non-tertial alicyclic alcohol and (meth)acrylic acid; and a monomer component 4 comprising (meth)acrylic acid.

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03-10-2013 дата публикации

Aluminum alloy composite and method for joining thereof

Номер: US20130256261A1
Принадлежит: Taisei Purasu Co Ltd

The object of the present invention is to strongly join an aluminum alloy part with an FRP prepreg. An object obtained by subjecting an aluminum alloy to a suitable liquid treatment so as to form a surface having large, micron-order irregularities and also fine irregularities with a period of several tens of nanometers, eliminating the presence of sodium ions from the surface and additionally forming a surface film of aluminum oxide, which is thicker than a natural oxide layer, has been found to have a powerful adhesive strength with epoxy-based adhesives. By simultaneously curing an FRP prepreg which uses the same epoxy-based adhesive in the matrix, an integral composite or structure in which FRP and aluminum alloy have been united at a joining strength of unprecedented magnitude is produced.

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10-10-2013 дата публикации

Air vehicle with a slip protecting and gas sealing composite floor

Номер: US20130264423A1
Принадлежит: EUROCOPTER DEUTSCHLAND GMBH

An air vehicle with a slip protecting and gas sealing composite floor ( 1, 10 ) inside a fuselage, particularly a helicopter with a slip protecting and gas sealing composite floor ( 1, 10 ) inside a fuselage. Said slip protecting and gas sealing composite floor ( 1, 10 ) is built up of a profiled elastomer layer ( 2 ) provided at its bottom side with a cross-linking agent, n-layers ( 3 ) of a further component or a variety of different components and partially thermosetting resin covered by a profiled elastomer layer ( 2 ), a honey comb layer ( 4 ) and lower n-layers ( 5 ) of said further component or variety of different components and partially thermosetting resin, said honey comb layer ( 4 ) being sandwiched between said n-layers ( 3 ) and said lower n-layers ( 5 ).

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17-10-2013 дата публикации

Continuous Fiber Reinforced Polyarylene Sulfide

Номер: US20130273280A1
Принадлежит: Ticona LLC

A continuous fiber composite is described and methods for forming the continuous fiber composite. The continuous fiber composite includes a plurality of unidirectionally aligned continuous fibers embedded within a polyarylene sulfide polymer. The continuous fiber composite includes a very high loading of continuous fibers, for instance greater than about 40% by weight of the continuous fiber composite. The continuous fiber composite is formed by reacting a starting polyarylene sulfide with a reactively functionalized disulfide compound in a melt processing unit. Reaction between the starting polyarylene sulfide and the reactively functionalized disulfide compound leads to formation of a reactively functionalized polyarylene sulfide. Upon embedding of the continuous fibers into the reactively functionalized polyarylene sulfide, the reactivity of the polyarylene sulfide can enhance adhesion between the polyarylene sulfide polymer and the fibers.

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24-10-2013 дата публикации

Sandwich-type, structural, composite component including at least one hingedly-connected portion, cargo management system and automotive vehicle load floor utilizing the component

Номер: US20130278003A1
Принадлежит: Global IP Holdings LLC

A sandwich-type, structural, composite component including at least one hingedly connected portion which pivots with reduced or eliminated hinge binding and a cargo management system and vehicle load floor utilizing the component are provided. Elongated first and second interior portions of the component are locally crushed by the press molding to form a living hinge having a pivot axis and an elongated depression, respectively. The component includes an elongated cut-out which extends completely through the component at the elongated depression to obtain a clearance between a first portion of the component hingedly connected to a second portion of the component by the living hinge. The living hinge and the clearance allow pivotal movement of the first portion between different use positions relative to the second portion with reduced or eliminated hinge binding during the pivotal movement about the pivot axis.

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07-11-2013 дата публикации

Protective covers

Номер: US20130294002A1
Принадлежит: Cocoon, Inc.

An enhanced protective cover includes a top and bottom textile layer and an air permeable, moisture-vapor-transmissive, expanded polytetrafluoroethylene membrane layer located between the two textile layers. The cover exhibits an MVTR rating of at least 4000 g/m 2 /day. The protective cover also includes a top layer coating or fibre treatment of a nano-ceramic material designed to increase the durability of the cover and increase the resistance to abrasion and wear while also resisting environmental conditions including exposure to solar radiation, temperature and humidity. Alternatively, the upper layer of the protective cover may incorporate ceramic coated fibers or ceramic co-extruded fibers, or carbon nanotubes. The protective cover may also feature a fire resistant application. The top textile layer may also include a permanent, highly breathable and highly durable electro-static discharge feature added to the inside of the layer by laying down a carbon based printed pattern on the inside of the layer.

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07-11-2013 дата публикации

Sheet material having a concave-convex part, and vehicle panel and laminated structure using the same

Номер: US20130295406A1
Автор: Masaya Takahashi
Принадлежит: Sumitomo Light Metal Industries Ltd

A sheet material ( 1 ) includes a stiffness-increasing concave-convex part ( 20 ). A first reference plane (K 1 ) and a second reference plane (K 2 ) serve as a reference system. Numerous at least substantially (H) shaped first reference areas ( 213 ), each including two parallel longitudinal bar parts ( 214 ) and a latitudinal bar part ( 215 ) that connects center portions the two parallel longitudinal bar parts together, are arrayed with the same orientation in the second reference plane (K 2 ). First areas ( 21 ) respectively protrude from the first reference areas ( 213 ) in the second reference plane (K 2 ) toward the first reference plane (K 1 ). Each first area ( 21 ) includes a first top surface ( 211 ), which is a reduced projection of its first reference area ( 213 ) into the first reference plane (K 1 ), and first side surfaces ( 212 ) that connect the outer periphery of the first top surface ( 211 ) with the outer periphery of the corresponding first reference area ( 213 ).

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21-11-2013 дата публикации

Joint Body of Carbon Fiber-Reinforced Composite Material

Номер: US20130309001A1
Принадлежит: Teijin Ltd

There is provided a joint body including: a reinforcing member having at least one random layer in which a chopped carbon fiber is randomly oriented in a thermoplastic resin, and at least one unidirectional material layer in which a continuous carbon fiber is unidirectionally arranged in a thermoplastic resin; and a reinforced member with an open sectional shape having at least one selected from the group consisting of a random layer and a unidirectional material layer, wherein the reinforcing member and the reinforced member are vibration-welded to form a hollow closed section.

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28-11-2013 дата публикации

Carbon-fiber-reinforced plastic structure

Номер: US20130316128A1
Автор: Hiroyuki Waku
Принадлежит: Mitsubishi Heavy Industries Ltd

A spar ( 2 ) is formed by stacking a signal-line layer ( 52 ), which includes a resin layer ( 521 ) having a plurality of signal lines ( 522 ) embedded therein, on a carbon-fiber prepreg ( 51 ).

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05-12-2013 дата публикации

Constrained-layer damping material

Номер: US20130319791A1
Автор: Gilles Stopin
Принадлежит: AUTONEUM MANAGEMENT AG

A constrained-layer damping material including a bitumen material, a binder material, and a tackifier, wherein the bitumen is a soft grade with a penetration of at least 150 dmm and a ring and ball softening point of greater than about 35° C.

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02-01-2014 дата публикации

Metal-clad hybrid article having synergistic mechanical properties

Номер: US20140004352A1
Принадлежит: Integran Technologies Inc

An article of manufacture includes a substrate having an outer surface clad with a metal construct including one or more continuous metal layers, at least one of which is an amorphous layer or a microcrystalline layer having a grain size below 5000 nm. A bonding layer is provided between the substrate and the layered metallic construct so that the bonding layer is in direct contact with the substrate and with the layered metallic construct. The bonding layer is made of a substantially fully cured resin including at least 10% of a rubber. The layered metallic construct has peel strength greater than 10N/cm. Also provided is a process for making the article including coating an article outer surface with a bonding layer and a layered metallic construct. The bonding layer is substantially fully cured before the layered metal construct is bonded to the article. The coated article is annealed.

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09-01-2014 дата публикации

Nanoreinforced films and laminates for aerospace structures

Номер: US20140011414A1
Принадлежит: Goodrich Corp, Rohr Inc

A composite laminate for use on an external part of an aerospace vehicle has improved ultraviolet resistance and resistance to microcracking from thermal cycling. The laminate comprises a nanoreinforcement film, a support veil, and a composite layer. The laminate also can have a lightning strike protection layer and an external paint and primer. The nanoreinforcement film can comprise carbon nanomaterial and a polymer resin, and the composite layer has one or more layers of a reinforcement and a polymer resin. The carbon nanomaterial can be carbon nanofibers, and the nanoreinforcement film can have an areal weight of less than about 100 g/m2. The carbon nanomaterial can also comprise carbon nanofibers and carbon nanotubes.

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30-01-2014 дата публикации

Adhesive sheet material application device and method

Номер: US20140027037A1
Принадлежит: Geek Wraps Inc

According to one aspect of the present invention, an adhesive sheet material application device is disclosed, which includes a roller support bar, a handle, and a roller, where the handle and the roller are connected to the roller support bar, a portion of the handle is parallel to the roller, and the roller is rotatable. In another aspect of the present invention, a second handle is connected to the roller support bar and the second handle has a strap. According to another aspect of the present invention, a method of using the adhesive sheet material application device is disclosed, which includes securing a portion of adhesive sheet material to a surface, applying the adhesive sheet material to the surface with the adhesive sheet material application device, and regressing and eradicating bubbles between the adhesive sheet material and surface.

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30-01-2014 дата публикации

Flexurally rigid laminated sheets, parts molded therefrom and method of fabrication

Номер: US20140030491A1
Принадлежит: QUADRANT PLASTIC COMPOSITES JAPAN LTD

Flexurally rigid molded parts are prepared by stacking a needled nonwoven mat of reinforcing fibers, at least one thermoplastic resin sheet and at least one surface sheet formed of a non-woven cloth comprising cloth fibers. The multilayered sheet obtained in this manner is subjected to heat and pressure followed by cooling under pressure, thereby forming a semi-finished product consisting of a consolidated laminated sheet with a porosity not exceeding 5% by volume. Upon reheating, the main body increases in thickness, thereby forming a porous laminated sheet that can be formed to a compact in a hot molding process.

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06-02-2014 дата публикации

Variable reflectance mirror system

Номер: US20140036339A1
Принадлежит: Gentex Corp

Anisotropic film laminates for use in image-preserving reflectors such as rearview automotive mirror assemblies, and related methods of fabrication. A film may comprise an anisotropic layer such as a light-polarizing layer and other functional layers. The film having controlled water content is heated under omnidirectional pressure and vacuum to a temperature substantially equal to or above a lower limit of a glass-transition temperature range of the film so as to be laminated to a substrate. The laminated film is configured as part of a mirror structure so as to increase contrast of light produced by a light source positioned behind the mirror structure and transmitted through the mirror structure towards a viewer. The mirror structure is devoid of any extended distortion and is characterized by SW and LW values less than 3, more preferably less than 2, and most preferably less than 1.

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06-03-2014 дата публикации

Composite laminate for a thermal and acoustic insulation blanket

Номер: US20140065357A1
Принадлежит: EI Du Pont de Nemours and Co

A multilayer laminate for use as a flame barrier in an aircraft comprising (i) a polymeric film layer capable of withstanding a temperature of at least 200 C for at least 10 min, (ii) an adhesive layer having an areal weight of from 2 to 40 gsm capable of activation at a temperature of from 75 to 200 degrees C., (iii) an inorganic refractory layer, and (iv) aramid paper comprising from 50 to 90 weight percent of aramid fibers and from 10 to 50 weight percent of meta-aramid binder wherein the inorganic refractory layer of (iii) comprises platelets in an amount of at least 85% by weight with a dry areal weight of 15 to 50 gsm and a residual moisture content of no greater than 10 percent by weight.

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13-03-2014 дата публикации

Process for producing sandwich elements

Номер: US20140072753A1
Принадлежит: BASF SE

The present invention relates to processes for producing sandwich elements, where the sandwich elements comprise a rigid polyurethane foam as core foam surrounded entirely or to some extent by a plastics resin comprising reinforcing-agent layers, by producing the rigid polyurethane foam on the reinforcing-agent layers and then saturating the reinforcing-agent layers in a liquid resin and hardening the resin. The present invention further relates to sandwich elements that can be produced by a process of the invention, and also to the use of these sandwich elements as wind-turbine blade, aircraft wing, wind-turbine nacelle, boat-hull, or housing for vehicles.

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27-03-2014 дата публикации

Resin article

Номер: US20140087157A1
Принадлежит: LG Chem Ltd

Provided is a resin article having a layer-separated structure. The resin article may include a first resin layer and a second resin layer formed on the first resin layer. Also, the component of the first resin layer is detected on a surface of the second resin layer by infrared spectrometer. The resin article may have improved mechanical and surface characteristics. Further, since coating or plating is not required for manufacturing a resin article, a manufacturing time and/or cost can be reduced, and productivity can be increased.

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27-03-2014 дата публикации

Prepreg tape slitting method and apparatus

Номер: US20140087198A1
Принадлежит: WEB INDUSTRIES Inc

Improved methods and apparatus are provided for the production of prepreg slit tape wherein master rolls of prepreg sheet are formed which are capable of being slit, with liner attached, at high precision.

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10-04-2014 дата публикации

Multi-layer material for application to a vehicle underbody

Номер: US20140097036A1
Принадлежит: US Farathane Corp

A dual layer material adapted to being applied to a vehicle underbody including a panel shaped body formed by a moldable polyethylene terephthalate (PET) layer joined with a polypropylene and glass composite layer in order to provide at least one of improved wear and abrasion resistance on an outer facing surface and acoustic noise attenuation on an inner vehicle facing surface. The dual layer material can also incorporate a bonding agent for adhering the layers together.

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06-01-2022 дата публикации

METHOD FOR PRODUCING A MULTILAYERED HEAT SHIELD

Номер: US20220001439A1
Принадлежит:

In a method for producing a multilayered heat shield, which has a first metal layer and a second metal layer that has an insulating layer arranged between the metal layers, the metal layers are connected at the edge by a flanging. To produce the heat shield, the first metal layer, the insulating layer and the second metal layer are placed into a first pressing tool. This is effected in such a way that an edge portion of the first metal layer protrudes beyond an edge portion of the second metal layer. The insulating layer is set back from the edge portions of the first metal layer and of the second metal layer. 14-. (canceled)5. A method of producing a multilayered heat shield , the method comprising: an edge portion of the first metal layer has a protruding limb that protrudes beyond an edge portion of the second metal layer, and', 'the insulating layer is set back from the edge portions of the first metal layer and the second metal layer;, 'placing a sandwich comprising a first metal layer, a second metal layer, and an insulating layer arranged between the first and second metal layers, into a first pressing tool, wherein'} the edge portion of the first metal layer and the edge portion of the second metal layer are bent over together in a forming direction,', 'the protruding limb of the edge portion of the first metal layer is repositioned counter to the forming direction to form a standing seam, and', 'the standing seam has a folded end and a free end;, 'forming the sandwich in the first pressing tool to form the edge portion of the first metal layer and the edge portion of the second metal layer relative to a plane of the insulating layer, wherein'}transferring the formed sandwich comprising the first metal layer, the second metal layer, and the insulating layer to a second pressing tool, the second pressing tool comprising an upper tool and a lower tool which receives the formed sandwich therebetween; and the upper tool comes into contact with the folded end of ...

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01-01-2015 дата публикации

CRASH-DURABLE ADHESIVE WITH ENHANCED STRESS DURABILITY

Номер: US20150001281A1
Принадлежит:

A heat-curable structural adhesive includes a non-rubber-modified epoxy resin, a reaction product of a carboxyl- or amine-terminated butadiene polymer or copolymer and a bisphenol F-based epoxy resin, a elastomeric toughener containing capped isocyanate groups, one or more epoxy curing agents a moisture scavenger and a heat activatable catalyst comprising a mixture of a solid or liquid tertiary amine compound that has a boiling temperature of at least 130° C. and a novolac resin. The structural adhesive develops excellent bonding properties when cured at moderate temperatures, especially from 120 to 170° C., and in addition performs very well in environmental aging stress testing. The adhesive is particularly good for bonding aluminum to another metal, or bonding aluminum to aluminum. 1. A heat-curable structural adhesive comprisingA) at least one non-rubber-modified epoxy resin;B) a reaction product of a carboxyl- or amine-terminated butadiene polymer or copolymer and a bisphenol F-based epoxy resin;C) at least one elastomeric toughener containing capped isocyanate groups;D) one or more epoxy curing agents;E) from 0.5 to 10 weight percent of a moisture scavenger, based on the total weight of the heat-curable structural adhesive; andF) a heat activatable catalyst comprising a mixture of a solid or liquid tertiary amine compound that has a boiling temperature of at least 130° C. and a novolac resin,and further wherein the elastomeric toughener and the rubber portion of the rubber-modified epoxy resin together constitute from 15 to 25% of the total weight of the heat-curable adhesive.2. The heat-curable structural adhesive of whicha) exhibits an impact shear strength of at least 20 N/mm as measured according to the ISO 11343 wedge impact method on 2 mm-thick aluminum 6111 alloy substrates after curing at 160° C. for 10 minutes,b) exhibits a storage modulus of at least 900 MPa at 50° C. as measured by dynamic mechanical analysis according to ASTM E2254-09; and/orc) ...

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06-01-2022 дата публикации

Two-Component, Water-Based Lamination Adhesive and Use of the Same to Bond Substrates and Foams

Номер: US20220002600A1
Принадлежит: Henkel AG and Co KGaA

A water comprising, two component polyurethane dispersion adhesive comprising an anionic polyester polyurethane resin and a solvent-free liquid aliphatic polyisocyanate cross-linker. The dispersion can be reactivated one or more times for edge bonding a flexible sheet material onto a substrate having a main surface, a peripheral surface and an edge connecting the main surface and the peripheral surface.

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07-01-2021 дата публикации

COMPOSITE MATERIAL AND METHOD FOR CURING COMPOSITE MATERIAL

Номер: US20210001588A1
Принадлежит:

A composite material is capable of suppressing decrease in the strength, which is caused by bending of fibers of a skin material during the time when the composite material is cured. A composite material is provided with a honeycomb core, a first skin material, a second skin material, a thunder-resistant mesh and a resin material; and the resin material is not arranged in a neighborhood portion which is the region corresponding to the region at the front end of the honeycomb core. A first film adhesive is arranged between the first skin material and the honeycomb core; a second film adhesive is arranged between the second skin material and the honeycomb core; and a fourth film adhesive is arranged in the neighborhood portion of the resin material in a weight per square meter, which is lower than those of the first film adhesive and the second film adhesive. 1. A composite material comprising:a honeycomb core;a first skin material disposed on one surface of the honeycomb core to be bonded to the honeycomb core;a second skin material disposed on an opposite surface of the honeycomb core from the one surface to be bonded to the honeycomb core;a lightning protection mesh disposed on an opposite surface of the second skin material from a surface of the second skin material, the surface being bonded to the honeycomb core; anda resin material disposed on an opposite surface of the lightning protection mesh from a second skin material side,wherein the resin material is not disposed in a neighboring portion of the resin material in a region corresponding to a region of a tip of an end portion of the honeycomb core.2. The composite material according to claim 1 ,wherein a first film adhesive bonding the first skin material to the honeycomb core is disposed between the first skin material and the honeycomb core,a second film adhesive bonding the second skin material to the honeycomb core is disposed between the second skin material and the honeycomb core, anda fourth film ...

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07-01-2021 дата публикации

HONEYCOMB CORE SANDWICH PANELS

Номер: US20210001589A1
Принадлежит:

In accordance with one embodiment of the present disclosure, a method for manufacturing a honeycomb core sandwich panel includes placing a thermoset facesheet in contact with a thermoplastic honeycomb core without using a separate adhesive and attaching the thermoset facesheet to the thermoplastic honeycomb core by using a curing profile comprising a temperature that is lower than a gel point temperature of the thermoset facesheet and higher than a softening point temperature of the thermoplastic honeycomb core. 120.-. (canceled)21. A method , comprising:placing a thermoset facesheet in contact with a thermoplastic honeycomb core; andattaching the thermoset facesheet to the thermoplastic honeycomb core by using a curing profile;wherein using the curing profile comprises curing the thermoplastic facesheet and the thermoplastic honeycomb core at a same time and at a same temperature.22. The method of claim 21 , wherein the thermoset facesheet comprises an epoxy resin.23. The method of claim 21 , wherein the thermoplastic honeycomb core comprises polyetherimide (PEI).24. The method of claim 21 , wherein the thermoset facesheet is attached to the thermoplastic honeycomb core without using a separate adhesive disposed between the thermoset facesheet and the thermoplastic honeycomb core.25. The method of claim 21 , wherein the thermoplastic honeycomb core comprises a plurality of cells claim 21 , each cell comprising a curved cell wall in a substantially circular tube shape.26. The method of claim 25 , wherein each cell has a diameter that claim 25 , when measured at a midplane of each cell claim 25 , does not vary more than 10 percent within the same cell.27. The method of claim 25 , wherein the plurality of cells have a longitudinal axis that is perpendicular to a plane of the thermoset facesheet.28. The method of claim 21 , wherein the curing occurs at a pressure less than an ambient pressure for a certain period of time and in a vacuum-capable oven.29. The method of ...

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07-01-2021 дата публикации

MOLDED PART AND METHOD FOR PRODUCING SUCH A MOLDED PART

Номер: US20210001591A1
Принадлежит:

A molded part comprises a decorative layer having on its front side a decorative ply of a wood veneer, wherein: a grain structure of the wood veneer is visible on the front side thereof, the grain structure has light regions and dark regions, a large number of light passages are provided in the decorative layer, and the light passages extend through the decorative layer; a translucent carrier; a light element comprising a light source and light passages arranged to imitate the grain structure of the wood veneer on the front side of the decorative ply, such that the density of the light passages in the decorative layer is dependent on the grain structure on the front side of the wood veneer, whereby, in the dark regions of the grain structure, there is a higher density or lower density of light passages than in the light regions of the grain structure. 110-. (canceled)11. A molded part comprising:a decorative layer having a front side designed as a visible side and a rear side opposite the front side, wherein the decorative layer comprises on its front side a decorative ply formed from wood veneer, wherein a grain structure of the wood veneer is visible on the front side of the decorative ply, wherein the grain structure has light regions and dark regions,wherein a plurality of light passages for transmitting light from the rear side of the decorative layer to the front side of the decorative layer being designed as the visible side, is provided in the decorative layer, wherein the light passages extend through the decorative layer,a transparent or translucent carrier, wherein the carrier is provided on the rear side of the decorative layer,a light element comprising at least one light source, wherein the light element is provided for illuminating the light passages, and the light element is provided on a rear side of the carrier,wherein the light passages are arranged so as to imitate the grain structure of the wood veneer on the front side of the decorative ply ...

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07-01-2021 дата публикации

COMPOSITE STRUCTURE FOR AN AIRBAG COVER, AND SEWN PRODUCT OF THE COMPOSITE STRUCTURE

Номер: US20210001594A1

The present invention provides a composite structure, a method for its manufacture, a sewn product containing the composite structure, and a method for manufacturing the sewn product. The composite structure comprises a foam layer, a textile layer, a cover layer and a lacquer layer in this order, wherein the foam layer has a density of at most 300 kg/mand contains a polyolefin, the cover layer is thermoplastic and comprises at least two compact sublayers of different composition, each sublayer containing at least one thermoplastic selected from polyolefin and polyvinyl chloride. 1. A composite structure comprising a foam layer , a textile layer , a cover layer and a lacquer layer in this order , the foam layer having a density of at most 300 kg/mand containing a polyolefin , the cover layer being thermoplastic and comprising at least two compact sublayers of different composition , each sublayer containing at least one thermoplastic selected from polyolefin and polyvinyl chloride.2. The composite structure according to claim 1 , which is suitable as a tearable coating for an airbag cover without a material weakening.3. The composite structure according to or claim 1 , wherein the polyolefin of the foam layer contains a polypropylene or consists of polypropylene.4. The composite structure according to any of the foregoing claims claim 1 , wherein the textile layer has a thickness of 0.05 to 2 mm.5. The composite structure according to one of the foregoing claims claim 1 , which has a Shore A hardness according to DIN 53505 of 20 to 45.6. The composite structure according to any of the foregoing claims claim 1 , wherein the foam layer has a gel content of 20 to 80%.7. The composite structure according to any of the foregoing claims claim 1 , wherein the thickness of the foam layer is 1 to 5 mm and the thickness of the cover layer is 0.2 to 1 mm.8. The composite structure according to any of the foregoing claims claim 1 , wherein the foam layer consists of sharpened ...

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07-01-2016 дата публикации

SYSTEMS AND METHOD FOR PRODUCING THREE-DIMENSIONAL ARTICLES FROM FLEXIBLE COMPOSITE MATERIALS

Номер: US20160001472A1
Принадлежит:

The present disclosure encompasses three-dimensional articles comprising flexible-composite materials and methods of manufacturing said three-dimensional articles. More particularly, the present system relates to methods for manufacturing seamless three-dimensional-shaped articles usable for such finished products as airbags/inflatable structures, bags, shoes, and similar three-dimensional products. A preferred manufacturing process combines composite molding methods with specific precursor materials to form fiber-reinforced continuous shaped articles that are flexible and collapsible. 1. (canceled)2. A method of producing three-dimensionally shaped , flexible composite parts , said method comprising the steps of:providing a male mold having a three-dimensional shape;shaping a composite layup over the male mold, said composite layup comprising (i) at least one fiber-reinforced scrim layer stretched over the male mold, said fiber-reinforced scrim layer comprising two or more layers of unidirectional fibers placed at different configurations to create a bias direction to which said fiber-reinforced scrim layer is stretched; and (ii) at least one additional fiber-reinforced scrim layer comprising unidirectional fibers oriented to limit stretch of the three-dimensionally shaped, flexible composite part along specific load paths; andcuring said composite layup to form a unitary three-dimensionally shaped flexible composite part having the three-dimensional shape of the male mold.3. The method of claim 2 , further comprising the step of adding one or more surface layers to said composite layup prior to said step of curing.4. The method of claim 2 , wherein said fiber-reinforced scrim layers are unitape layers comprising thinly spread substantially parallel fibers coated by claim 2 , or embedded in claim 2 , a matrix adhesive.5. The method of claim 4 , wherein said fibers comprise ultra-high molecular weight polyethylene (UHMWPE) claim 4 , p-aramids claim 4 , m-aramids ...

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07-01-2021 дата публикации

LOCALIZED PANEL STIFFENER

Номер: US20210001600A1
Принадлежит:

A device () comprising a carrier material () and a matrix material () deposited onto the carrier material in a pattern that leaves a predetermined amount of space () between each deposition of matrix material. 1. A device comprising:a carrier material; anda matrix material deposited onto the carrier material in a pattern that leaves a predetermined amount of space between each deposition of matrix material.2. The device of claim 1 , wherein each deposition of matrix material is about 0.5 mm or more in diameter and about 10 mm or less in diameter.3. The device of claim 1 , wherein the device is capable of bending without breaking.4. The device of claim 1 , wherein the device will bend under its own weight when held at its end.5. The device of claim 1 , wherein the matrix material is an activatable material and the volumetric activation of the matrix material is at least about 100% and less than about 300%.6. The device of claim 1 , wherein the matrix material includes a structural adhesive material.7. The device of claim 1 , wherein the matrix material includes a sealant material.8. The device of claim 1 , wherein each deposition of matrix material is about 1 mm or more in diameter and about 4 mm in diameter or less.9. The device of claim 1 , wherein the carrier is free of any sharp corners and includes only rounded corners.10. The device of claim 1 , wherein the predetermined amount of space between each deposition of matrix material is at least about 0.5 mm claim 1 , at least about 1 mm claim 1 , at least about 2 mm or even at least about 5 mm.11. The device of claim 1 , including an elastic material deposited onto the carrier material in a pattern that leaves a predetermined amount of space between each deposition of elastic material.12. The device of claim 11 , wherein the matrix material and the elastic material are deposited in an alternating pattern onto the carrier.13. The device of claim 1 , wherein the matrix material is deposited onto only one surface of ...

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07-01-2021 дата публикации

THERMALLY LAYERED FIRE TREATED VENEER PANEL

Номер: US20210001606A1
Принадлежит: GOODRICH CORPORATION

A veneer panel may include a face veneer, a first inner layer bonded to the face veneer, a second inner layer bonded to the first inner layer, and a thermally conductive backing layer bonded to the second inner layer. The first inner layer and the second inner layer are treated with a flame retardant. The first inner layer is disposed between the face veneer and the second inner layer, and the second inner layer is disposed between the first inner layer and the thermally conductive backing layer. 1. A veneer panel , comprising:a face veneer;a first inner layer;a first adhesive material disposed between the face veneer and the first inner layer, wherein the first adhesive material bonds the first inner layer to a back surface of the face veneer;a second inner layer bonded to the first inner layer, the first inner layer and the second inner layer are treated with a flame retardant; anda thermally conductive backing layer; anda second adhesive material disposed between the thermally conductive backing layer and the second inner layer, wherein the second adhesive material bonds the second inner layer to the thermally conductive backing layer,wherein the first inner layer is disposed between the face veneer and the second inner layer, and the second inner layer is disposed between the first inner layer and the thermally conductive backing layer, and the first adhesive material comprises a phenolic adhesive and the second adhesive material comprises an acrylic adhesive,wherein the first inner layer comprises a wood.24-. (canceled)5. The veneer panel of claim 1 , wherein the thermally conductive backing layer comprises an annealed aluminum.6. The veneer panel of claim 5 , wherein a thickness of the first adhesive material is 0.002 inches and 0.007 inches.7. The veneer panel of claim 6 , wherein a thickness of the second adhesive material is between 0.001 inches and 0.01 inches.8. The veneer panel of claim 7 , further comprising a third adhesive material disposed between ...

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05-01-2017 дата публикации

POLYURETHANE BASED RIGID FLOORING LAMINATE

Номер: US20170001414A1
Принадлежит:

The laminate according to the invention is a multiple layer structure and contains predominantly urethane-based polymeric materials in the cap and base layers thereof, with no significant amount of PVC. As such, under combustion conditions, the laminate releases substantially no harmful halogen-based bases, such as HCl or other toxic gases, and exhibits toxicity and smoke generation parameters well below acceptable industry standards. 1. A laminate structure comprising:a backing layer comprising, by weight, from about 20% to about 80% fiber reinforcement and from about 80% to about 20% thermoset or thermoplastic polymer selected from acrylic, polyvinylester, polyester, phenolic, epoxy, polysulfone, polyethersulfone and mixtures thereof;a base layer comprising polyurethane-based material combined with a copolymer of polyamide, polyether, polyester, polyether, polyimide, polyphenylene oxide, acrylic and polystyrene; andan adhesive layer disposed on a first surface of the base layer between the backing layer and the base layer; anda cap layer comprising polyurethane.21. The laminate of claim. , wherein the copolymer is a terpolymer comprising polyamide , polyester and polyether or any combination thereof.3. The laminate of claim 2 , wherein the base layer includes the polyurethane/terpolymer as a sub layer in combination with at least one other sub layer selected from a primer sub layer claim 2 , a fiber sub layer and a sealing sub layer.4. The laminate of claim 3 , wherein the fiber sub layer comprises at least one of glass claim 3 , aramid claim 3 , carbon claim 3 , PVA claim 3 , hemp claim 3 , jute claim 3 , organic fiber claim 3 , synthetic fiber disposed in a thermoset or thermoplastic resin5. The laminate of claim 1 , wherein the adhesive layer comprises thermoplastic polyurethane.6. The laminate of claim 1 , wherein the adhesive layer comprises by weight claim 1 , from about 50% to about 70% polymer and from about 30% to about 50% flame retardant additive.7. The ...

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05-01-2017 дата публикации

INTERLAYER FOR LAMINATED GLASS, INTERLAYER FOR LUMINESCENT LAMINATED GLASS, AND LAMINATED GLASS

Номер: US20170001417A1
Автор: Izu Yasuyuki, Oota Yuusuke
Принадлежит: Sekisui Chemical Co., Ltd.

The first aspect of the present invention aims to provide an interlayer film for laminated glass, an interlayer film for luminescent laminated glass, and a laminated glass including the interlayer film for laminated glass which are significantly suppressed while containing an aromatic compound such as a salicylic acid compound or a benzophenone compound. The second aspect of the present invention aims to provide an interlayer film for laminated glass which enables display of high luminance images under irradiation with light and inhibits reduction in the luminance of images even after use for a long period of time, and a laminated glass including the interlayer film for laminated glass. The first aspect of the present invention relates to an interlayer film for laminated glass containing: a thermoplastic resin; an aromatic compound that has a structure capable of coordinating with a metal; and an antioxidant, the antioxidant being at least one antioxidant selected from the group consisting of a phenolic compound, a phosphoric acid compound, and a sulfur compound. The second aspect of the present invention relates to an interlayer film for laminated glass including a luminescent layer that contains a thermoplastic resin, a luminescent material having a terephthalic acid ester structure, and a benzotriazole ultraviolet absorber, the luminescent layer containing the benzotriazole ultraviolet absorber in an amount of 0.05 to 10 parts by weight based on 1 part by weight of the luminescent material having a terephthalic acid ester structure. 1. An interlayer film for laminated glass comprising:a thermoplastic resin;an aromatic compound that has a structure capable of coordinating with a metal; andan antioxidant,the antioxidant being at least one antioxidant selected from the group consisting of a phenolic compound, a phosphoric acid compound, and a sulfur compound.2. The interlayer film for laminated glass according to claim 1 ,which contains the aromatic compound that ...

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05-01-2017 дата публикации

FIBER REINFORCED PLASTIC MEMBER FOR VEHICLE AND METHOD OF PRODUCING THE SAME

Номер: US20170001418A1
Принадлежит:

The fiber-reinforced plastic member includes a continuous variation layer which includes a synthetic resin constituting a base and a plurality of reinforcement fibers embedded in the synthetic resin, and a reinforcing layer which is attached to the continuous variation layer to constitute the fiber-reinforced plastic member for a vehicle and is composed of a synthetic resin constituting the base and a plurality of reinforcement fibers. 1. A fiber-reinforced plastic member for a vehicle comprising:a continuous variation layer which comprises a synthetic resin constituting a base and a plurality of reinforcement fibers embedded in the synthetic resin, the plurality of reinforcement fibers being arranged so as to be inclined with respect to a longitudinal direction of the fiber-reinforced plastic member for a vehicle and angles of the reinforcement fibers with respect to the longitudinal direction of the fiber-reinforced plastic member progressively varying along the longitudinal direction; anda reinforcing layer which is attached to the continuous variation layer to constitute the fiber-reinforced plastic member for a vehicle and comprises a synthetic resin constituting the base and a plurality of reinforcement fibers, the plurality of reinforcement fibers being embedded in the synthetic resin and intersecting each other in a reticular pattern.2. The fiber-reinforced plastic member for a vehicle according to claim 1 , wherein the reinforcement fibers of the reinforcing layer comprises a first group of fibers and a second group of fibers claim 1 ,wherein the first group of fibers are arranged to intersect reinforcement fibers of the continuous variation layer disposed at one side of the continuous variation layer, and the second group of fibers are arranged to intersect reinforcement fibers of the continuous variation layer disposed at another side of the continuous variation layer, andwherein the first and second groups of fibers are arranged to intersect each other ...

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07-01-2016 дата публикации

Cold lamination with radiation

Номер: US20160001535A1
Принадлежит: Lisa Draexlmaier GmbH

A process for laminating a material layer to a support including: providing the support, applying the material layer to the support, a heat-activatable adhesive being applied to s side of the material layer facing the dimensionally stable support and/or to the side of the dimensionally stable support facing the material layer, pressing the flexible material layer and the dimensionally stable support together by means of a lower dimensionally stable mold half and an upper dimensionally stable mold half, irradiating the mold halves, the support and the material layer with electromagnetic radiation, in particular with microwave radiation, high-frequency radiation or induction radiation, whereby the adhesive is activated directly or indirectly.

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07-01-2021 дата публикации

Windshield

Номер: US20210001695A1
Принадлежит: Nippon Sheet Glass Co Ltd

A laminated glass according to the present invention is a windshield for an automobile to which an information acquisition device for acquiring information from the outside of a vehicle by emitting and/or receiving light can be installed, the windshield including an outer glass plate that includes a first side and a second side that is opposite to the first side, an inner glass plate that is arranged opposite to the outer glass plate and has substantially the same shape as the outer glass plate, and an intermediate film that is arranged between the outer glass plate and the inner glass plate. The windshield includes an information acquisition region that is to be located opposite to the information acquisition device and through which the light passes.

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07-01-2021 дата публикации

VEHICLE WINDOW UNIT

Номер: US20210001696A1
Принадлежит:

A vehicle window unit that includes side curved regions that are arranged, in the installed state, near a, in particular standing, pillar of the vehicle body, wherein the curved regions are at least partially coloured in a transmittance reducing manner. The degree of colouration correlates with the degree of curvature. 1. A vehicle window unit that includes side curved regions that are arranged , in an installed state , near a pillar of the vehicle body ,wherein the curved regions are at least partially coloured in a transmittance reducing manner,wherein the degree of colouration changes as a function of location, and wherein the degree of colouration correlates with the degree of curvature.2. The vehicle window unit according to claim 1 , wherein the curvature in the side curved regions is more pronounced than an averaged curvature of the pane.3. The vehicle window unit according to claim 1 , wherein a radius of curvature in the side curved regions is less than 300 mm.4. The vehicle window unit according to claim 1 , wherein in the side curved regions a gradient of radii of curvature of at least 10 occurs.5. The vehicle window unit according to claim 1 , implemented as a front window unit of a passenger means of transportation claim 1 , wherein the coloured curved regions are those that are positioned claim 1 , in the installed state claim 1 , near an A-pillar of the vehicle body.6. The vehicle window unit according to claim 1 , implemented as a rear window unit of a passenger means of transportation claim 1 , wherein the coloured curved regions are positioned claim 1 , in the installed state claim 1 , near a C-pillar of the vehicle body.7. The vehicle window unit according to claim 1 , implemented as a glass roof unit of a passenger means of transportation claim 1 , wherein a coloured curved region is provided at least at or near a narrow side edge of the glass roof unit claim 1 , which is positioned claim 1 , in the installed state claim 1 , at a border strut of ...

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04-01-2018 дата публикации

Joining structure

Номер: US20180001525A1
Принадлежит: Kobe Steel Ltd

A joining structure includes a first member, a second member of a material different from that of the first member, and a separation mechanism provided between the first member and the second member and that separates the first member and the second member from each other, wherein a resin is filled into the space between the edge of at least one member among the first member and the second member, and the other member.

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04-01-2018 дата публикации

DIE SLIDE ROTATIONAL HOLLOW MOLDING ASSEMBLY FOR CREATING AN ARTICLE WITH A HOLLOW INTERIOR

Номер: US20180001526A1
Автор: Bland Wayne
Принадлежит:

A mold assembly for forming a component exhibiting a sealed interior, including providing first and second mold halves, forming first and second half shells of material within cavities defined within each of the mold halves, and upon mating the mold halves together in a first closed mold configuration. The mold halves are reopened, with at least one of the shells being subsequently reoriented such that the first and second half shells are arrayed in opposing fashion with perimeter extending edges of each half shell arranged in contact with one another. Additional steps include reclosing the mold halves and subsequently forming a second perimeter extending material in contact with the contacting perimeter extending edges in order to bond the half shells together, upon which the mold halves are reopened and a completed component removed. 1. A mold assembly for forming a component exhibiting a sealed interior , said mold assembly comprising:a stationary supported mold half;a rotary platen supported mold half, each of said mold halves being movable in directions towards and away from one another in order to define each of engaged/closed and opened/separated positions;each of said mold halves exhibiting a plurality of shell forming locations defined in opposing configured surfaces thereof for forming a first half shell of material in said stationary supported mold half and a second half shell of material in said rotary platen supported mold half and, upon mating said mold halves together in a first closed mold configuration; andupon separating the mold halves and subsequently rotating the rotary platen supported mold half 180° in order to reposition the second half shell relative to a further shell forming location associated with the first mold half, the first and second half shells are arrayed in opposing fashion with a perimeter extending and formed edge of each half shell arranged in contact with one another;said mold halves being subsequently reclosed prior to a ...

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04-01-2018 дата публикации

COMPOSITE WING STRUCTURE AND METHODS OF MANUFACTURE

Номер: US20180001579A1
Принадлежит: Bell Helicopter Textron Inc.

In one aspect, there is a method of making a pre-cured laminate having a total number of plies in a mold, the mold having a periphery defined by a forward edge, an aft edge, and outboard ends. The method includes selecting a first plurality of resin impregnated plies that continuously extend beyond the periphery of the mold, the first plurality of resin impregnated plies includes at least 50 percent of the total number of plies; laying the plies in a mold; compacting the plies in a mold; and pre-curing the plies to form a pre-cured laminate, which can extend beyond the periphery of the mold. In an embodiment, a pre-cured laminate includes a first plurality of resin impregnated plies that continuously extend beyond the periphery of the mold, the first plurality of resin impregnated plies includes at least 50 percent of the total number of plies. 2. The method of claim 1 , wherein the first plurality of resin impregnated plies comprises from about 50 percent to about 90 percent of the total number of plies.3. The method of claim 1 , further comprising:selecting a second plurality of resin impregnated plies that do not extend beyond the forward edge and continuously extend beyond the aft edge; andlaying the second plurality of resin impregnated plies in the mold to form a portion of the total number of plies.4. The method of claim 3 , wherein the second plurality of resin impregnated plies comprises from about 15 percent to about 25 percent of the total number of plies.5. The method of claim 3 , further comprising:selecting a third plurality of resin impregnated plies that do not extend beyond the aft edge and continuously extend beyond the forward edge; andlaying the third plurality of resin impregnated plies in the mold to form a portion of the total number of plies.6. The method of claim 5 , wherein the third plurality of resin impregnated plies comprises from about 15 percent to about 25 percent of the total number of plies.7. The method of claim 5 , wherein a ...

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04-01-2018 дата публикации

COMPOSITE WING STRUCTURE AND METHODS OF MANUFACTURE

Номер: US20180001590A1
Принадлежит: Bell Helicopter Textron Inc.

In one aspect, there is a method of making a composite skin for a tiltrotor aircraft including providing a first skin in a mold, the first skin having a periphery defined by a forward edge, an aft edge, and outboard ends; providing a plurality of honeycomb panels having an array of large cells onto the first skin, each cell having a width of at least 1 cm; assembling the plurality of honeycomb panels along the longitudinal axis of the first skin to form a honeycomb core having an outer perimeter within the periphery of the first skin; positioning a second skin onto the honeycomb core, the second skin having an outer perimeter within the periphery of the first skin; and curing an adhesive to create a bond between the first skin, the honeycomb core, and the second skin to form a composite skin. 1. A method of making a composite skin for a tiltrotor aircraft , comprising:providing a first skin in a mold, the first skin having a periphery defined by a forward edge, an aft edge, and outboard ends;providing a plurality of honeycomb panels having an array of large cells onto the first skin, each cell having a width of at least 1 cm;assembling the plurality of honeycomb panels along the longitudinal axis of the first skin to form a honeycomb core having an outer perimeter within the periphery of the first skin;positioning a second skin onto the honeycomb core, the second skin having an outer perimeter within the periphery of the first skin; andcuring an adhesive to create a bond between the first skin, the honeycomb core, and the second skin to form a composite skin.2. The method of claim 1 , wherein the outer perimeter of the honeycomb core and the second skin on the forward and aft edges is from about 1 cm to about 16 cm from the forward and aft edges of the first skin.3. The method of claim 1 , wherein the outer perimeter of the honeycomb core and the second skin on the outboard edges is from about 7 cm to about 91 cm from the outboard edges of the first skin.4. The ...

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04-01-2018 дата публикации

Method for producing a sandwich panel comprising a reinforced foam core

Номер: US20180001593A1
Принадлежит: Airbus Defence and Space GmbH

A method for producing a sandwich panel with a reinforced foam core includes inserting rod-shaped, thermoplastic reinforcing elements into a thermoplastic foam material such that the reinforcing elements extend through the foam material. End regions of the reinforcing elements project out of the foam material. The foam material is thermoformed to form a reinforced foam core, wherein the end regions of the reinforcing elements are integrally formed by applying temperature and pressure to the cover surfaces of the foam material and are bonded to the foam material in a fused connection. A thermoplastic cover layer is laminated on either side by applying temperature and pressure to the reinforced foam core on the cover surfaces of the foam material in order to form the sandwich panel, wherein the cover layers are bonded to the reinforced foam core in a fused connection.

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04-01-2018 дата публикации

INTERMEDIATE FILM FOR LAMINATED GLASS, AND LAMINATED GLASS

Номер: US20180001598A1
Принадлежит:

There is provided an interlayer film for laminated glass with which the flexural rigidity of laminated glass can be enhanced over a wide temperature range and the sound insulating properties of laminated glass can be enhanced over a wide temperature range. The interlayer film for laminated glass according to the present invention has a shear storage equivalent elastic modulus of 10 MPa or more and 500 MPa or less in a temperature region of 80% or more of the temperature region of 0° C. or more and 60° C. or less, a value obtained by dividing a shear storage equivalent elastic modulus at 10° C. by a shear storage equivalent elastic modulus at 50° C. of 1 or more and 10 or less, a glass transition temperature falling within the range of −25° C. or more and 0° C. or less, and a largest value of tan δ in a temperature region of −50° C. or more and 0° C. or less of 0.1 or more and 1 or less. 1. An interlayer film for laminated glass having: a shear storage equivalent elastic modulus of 10 MPa or more and 500 MPa or less in a temperature region of 80% or more of the temperature region of 0° C. or more and 60° C. or less;a value obtained by dividing a shear storage equivalent elastic modulus at 10° C. by a shear storage equivalent elastic modulus at 50° C. of 1 or more and 10 or less;a glass transition temperature falling within the range of −25° C. or more and 0° C. or less; anda largest value of tan δ in a temperature region of −50° C. or more and 0° C. or less of 0.1 or more and 1 or less.2. The interlayer film for laminated glass according to claim 1 , having a glass transition temperature falling within the range of −20° C. or more.3. The interlayer film for laminated glass according to claim 1 , comprising a resin with a weight average molecular weight of 100000 or more and 1300000 or less.4. The interlayer film for laminated glass according to claim 1 , having a value of tan δ of 0.1 or more in a temperature region of 10% or more of the temperature region of −50° C. ...

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04-01-2018 дата публикации

INTERMEDIATE FILM FOR LAMINATED GLASS, AND LAMINATED GLASS

Номер: US20180001599A1
Принадлежит:

There is provided an interlayer film for laminated glass with which the flexural rigidity, sound insulating properties and long-term adhesive stability of laminated glass can be enhanced. The interlayer film for laminated glass according to the present invention has a shear storage equivalent elastic modulus of 10 MPa or more and 500 MPa or less in a temperature region of 80% or more of the temperature region of 0° C. or more and 30° C. or less, a value obtained by dividing a shear storage equivalent elastic modulus at 10° C. by a shear storage equivalent elastic modulus at 30° C. of 1 or more and 10 or less, a glass transition temperature falling within the range of −25° C. or more and 0° C. or less, and a largest value of tan δ in a temperature region of −50° C. or more and 0° C. or less of 0.1 or more and 1 or less. 1. An interlayer film for laminated glass having: a shear storage equivalent elastic modulus of 10 MPa or more and 500 MPa or less in a temperature region of 80% or more of the temperature region of 0° C. or more and 30° C. or less;a value obtained by dividing a shear storage equivalent elastic modulus at 10° C. by a shear storage equivalent elastic modulus at 30° C. of 1 or more and 10 or less;a glass transition temperature falling within the range of −25° C. or more and 0° C. or less; anda largest value of tan δ in a temperature region of −50° C. or more and 0° C. or less of 0.1 or more and 1 or less.2. The interlayer film for laminated glass according to claim 1 , having a glass transition temperature falling within the range of −20° C. or more.3. The interlayer film for laminated glass according to claim 1 , comprising a resin with a weight average molecular weight of 100000 or more and 1300000 or less.4. The interlayer film for laminated glass according to claim 1 , having a value of tan δ of 0.1 or more in a temperature region of 10% or more of the temperature region of −50° C. or more and 0° C. or less.5. The interlayer film for laminated glass ...

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04-01-2018 дата публикации

Interlayer for laminated glass and laminated glass

Номер: US20180001600A1
Принадлежит: Sekisui Chemical Co Ltd

There is provided an interlayer film for laminated glass with which the flexural rigidity of laminated glass can be enhanced and the sound insulating properties of laminated glass can be enhanced. The interlayer film for laminated glass according to the present invention includes a thermoplastic resin, and has a smallest value of the shear storage elastic modulus in a temperature region of 10° C. or more and 40° C. or less measured at a frequency of 0.5 Hz of 3 MPa or more, a ratio of a shear storage elastic modulus at 20° C. measured at a frequency of 0.5 Hz to a shear storage elastic modulus at −30° C. measured at a frequency of 0.5 Hz of 0.01 or more and 0.8 or less, a glass transition temperature falling within the range of −20° C. or more and 0° C. or less, and a largest value of tan δ in a temperature region of −20° C. or more and 0° C. or less of 0.1 or more.

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04-01-2018 дата публикации

Coating of parts or objects and method for obtaining it

Номер: US20180001602A1
Автор: Ferro Emiliano
Принадлежит:

A coating of structures or elements or parts made of plastic material obtained by molding includes a finish layer; a reinforcement layer coupled to the finish layer, from the opposite side to the exposed face, to form a sandwich; and a heat-sealable film coupled in its solid form to the reinforcing layer, wherein this sandwich is suited to be coupled to a support part in a plastic material obtained by molding, and wherein this coupling occurs during the molding of the support part by way of the heat-sealable film suited to be activated at the molding temperature. 1111. A coating () of structures , elements , or parts () made of a plastic material obtained by molding , comprising:{'b': 2', '6', '21, 'at least one finish layer () adapted to be secured to a support part () made of a plastic material and produced by molding, said at least one finish layer having at least one exposed face () intended to remain visible;'}{'b': 3', '2', '22', '21', '5, 'at least one reinforcement layer () directly or indirectly coupled to said at least one finish layer (), at least at an opposite side () of said exposed face (), to form a sandwich (); and'}{'b': 4', '3, 'at least one heat-sealable film () directly or indirectly coupled in solid form at least to said at least one reinforcement layer (),'}{'b': 5', '6, 'wherein said sandwich () is adapted to be coupled to said at least one support part () made of said plastic material, and'}{'b': 6', '4, 'wherein said coupling takes place during the molding of said at least one support part (), by way of said at heat-sealable film () activated at a molding temperature.'}212. The coating () according to claim 1 , wherein said at least one finish layer () is a sheet of burl wood or a wood veneer.312. The coating () according to claim 1 , wherein said at least one finish layer () is made of leather claim 1 , imitation leather claim 1 , stone or derivatives thereof claim 1 , or natural or synthetic fabrics.41324. The coating () according to ...

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02-01-2020 дата публикации

THERMOPLASTIC AEROSTRUCTURE WITH LOCALIZED PLY ISOLATION AND METHOD FOR FORMING AEROSTRUCTURE

Номер: US20200001569A1
Принадлежит:

A composite wingbox structure formed of reinforced thermoplastic. The composite includes carbon fiber reinforcement and a plurality of insulation elements to localize the heat formed during the process of manufacturing the structure. The process of manufacturing the wingbox includes the steps of interleaving a series of insulations elements within a plurality of laminae and consolidating the insulation elements and laminae to form a laminate. The laminate is then aligned with a support structure such that the insulation elements overlie the supports structure. The laminate is then fused to the support structure using a non-contact heating process, such as inductive welding. 1. A method for forming a composite wingbox , comprising the steps of:providing a plurality of spars;connecting a plurality of ribs with the plurality of spars; a plurality of structural layers, each formed of carbon fiber reinforced thermoplastic laminae;', 'a plurality of insulating layers each formed of a plurality of spaced apart electrically insulating elements, wherein each insulating element has a length and a width and the length is substantially longer than the width, wherein the insulating layers are aligned with one another and are disposed between the structural layers, wherein the insulating layers are configured so that the insulating elements overlie the spars and ribs when the composite skin overlies the spars and ribs;', 'a weld layer formed of carbon fiber reinforced thermoplastic lamina;, 'forming a composite skin, comprisingpositioning the composite skin over the ribs and spars so that the layers of the composite skin overlie the ribs and spars;welding the composite skin to the ribs and spars, wherein the step of welding comprises the step of conveying an induction welding head over the composite laminate adjacent the ribs and spars so the induction welding head imposes an electromagnetic field through the composite laminate so that weld layer is heated above the melting ...

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02-01-2020 дата публикации

LIGHT WEIGHT COMPOSITE MATERIAL SYSTEMS, POLYMERIC MATERIALS, AND METHODS

Номер: US20200001574A1
Принадлежит:

The present invention relates to filled polymeric materials including a polymer and a filler distributed within the polymer, and to light weight composites which comprise at least a pair of metallic layers and a polymeric layer interposed between the pair of metallic layers, the polymeric layer containing the filled polymeric material. The composite materials of the present invention may be formed using conventional stamping equipment at ambient temperatures. Composite materials of the present invention may also be capable of being welded to other metal materials. The composite materials may be employed in an automotive part. Preferred composite materials include one or any combination of the following features: metallic fibers, ribbon fibers; or a polyolefin. 1. A method of producing a light weight composite material comprising steps of:extruding a sheet of a filled polymeric material; andinterposing the sheet between a first metallic layer and a second metallic layer; i. one or more polymers including a polyolefin polymer having a crystallinity of about 20 wt. % to about 80 wt. % as measured using differential scanning calorimetry and a melting point greater than about 100° C., as measured according to ASTM D3418-08; and', 'ii. a metallic filler;', 'wherein the light weight composite material is weldable and stampable., 'wherein the filled polymeric material comprises2. The method of claim 1 , wherein the sheet has a thickness;the metallic filler includes greater than 5 volume percent and less than 25 volume percent based on the total volume of the filled polymeric material of a mass of metallic fibers distributed within the polymer the mass spanning a thickness of the extruded sheet and including ribbon fibers having a weight average length greater than about 200 μm and less than about 25 mm; andthe weight ratio of the one or more polymers to the metallic fibers is greater than about 2.2:1.3. The method of claim 2 , wherein the fraction of the metallic fibers ...

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02-01-2020 дата публикации

ASYMMETRIC GLASS LAMINATES

Номер: US20200001576A1
Принадлежит:

Principles and embodiments of the present disclosure relate to unique asymmetric laminates and methods that produce the laminates where the laminate includes an first glass substrate having a first thickness (t), an second glass substrate having a second thickness (t), an interlayer disposed between the second glass substrate and the first glass substrate, wherein the first thickness and the second thickness has a combined third thickness (t), and wherein t/tor t/tis in a range from about 0.7 to about 0.99. 1. A laminate comprising:{'sub': 'o', 'a first glass substrate comprising a first thickness (t) and a first outer surface and a second inner surface;'}{'sub': 'i', 'a second glass substrate comprising a second thickness (t) that is less than to, a third outer surface, and a fourth inner surface;'}an interlayer disposed between the second inner surface and the third outer surface;{'sub': t', 'i, 'wherein a third thickness (t) is equal to the sum of to and t;'}{'sub': o', 't, 'wherein t/tis in a range of from 0.7 to 0.999; and'}{'sub': rr', 'rr', 't', 't', 't, 'sup': '2', 'wherein, when the first outer surface is impacted at normal incidence with a 1 gram ball bearing traveling at a speed of 45 mph, the fourth inner surface experiences a flexural stress (σ) of no more than σ=10.344t−109.33t+347.75 as measured by strain gauge for tin a range of from 2 mm to 7 mm.'}2. The laminate of claim 1 , wherein the second glass substrate comprises a soda-lime silicate glass composition claim 1 , an aluminosilicate glass composition claim 1 , or an alkali aluminosilicate glass composition.3. The laminate of claim 1 , wherein the second glass substrate comprises a second glass comprising a surface compressive stress (CS) of no more than 300 MPa4. The laminate of claim 1 , wherein the second glass substrate comprises a strengthened glass substrate.5. The laminate of claim 4 , wherein the second glass substrate comprises at least one of a surface CS in a range from about 50 MPa to ...

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05-01-2017 дата публикации

KNEE PROTECTION STRUCTURE FOR VEHICLE

Номер: US20170001589A1
Принадлежит:

A knee protection structure for a vehicle may include a bracket disposed on a vehicle body structure, and a lower crash pad panel disposed to be supported by the bracket so that a knee of a passenger hits the lower crash pad panel in the event of a collision, in which the lower crash pad panel may include a uni-directional continuous-fiber composite material, continuous fibers may be arranged in a given direction, inserted into at least a predetermined region of the entire region thereof, and a multi-directional continuous-fiber composite material, in which continuous fibers may be arranged in multiple directions, inserted into the remaining region. 1. A knee protection structure for a vehicle , comprising:a bracket disposed on a vehicle body structure; anda lower crash pad panel disposed to be supported by the bracket so that a knee of a passenger hits the lower crash pad panel in the event of a collision,wherein the lower crash pad panel includes a uni-directional continuous-fiber composite material, in which continuous fibers are arranged in a given direction, inserted into at least a predetermined region of the entire region thereof, and a multi-directional continuous-fiber composite material, in which continuous fibers are arranged in multiple directions, inserted into the remaining region.2. The knee protection structure of claim 1 , wherein the uni-directional continuous-fiber composite material is inserted into both side portions in a left-and-right direction of an entire region of the lower crash pad panel claim 1 , and the multi-directional continuous-fiber composite material claim 1 , in which the continuous fibers are arranged in multiple directions claim 1 , is inserted into a central portion in the left-and-right direction of the lower crash pad panel.3. The knee protection structure of claim 2 , wherein the continuous-fiber composite material inserted into the side portions has a smaller thickness than a thickness of the continuous-fiber composite ...

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04-01-2018 дата публикации

BATTERY PACK, BATTERY CHARGING STATION, AND CHARGING METHOD

Номер: US20180001735A1
Автор: Chuang Chi-Sheng

Various techniques described herein relate to battery packs of electric vehicles, batteries, and battery charging systems. Batteries may comprise a plurality of battery modules, wherein each battery module may be provided with one or more battery cells, and the plurality of battery modules may be connected in series when providing electric power output. Battery charging systems described herein may comprise a charging circuit that connects a plurality of battery modules in series, and may be used for charging the plurality of battery modules in the battery in series. Additional charging circuits may be connected respectively to the plurality of battery modules, and the additional charging circuits may be used for charging at least one battery module in the plurality of battery modules. 1. A battery pack for an electric vehicle , comprising:a battery comprising a plurality of battery modules connected in series, the battery modules including a first battery module and a second battery module; a first charging circuit configured to charge the plurality of battery modules in series to a first preset voltage;', 'a plurality of second charging circuits each corresponding one or more of the plurality of battery modules, each of the second charging circuits being configured to charge a corresponding battery module to a second preset voltage individually, the plurality of second charging circuits including a second charging circuit connected to the first battery module and the second battery module; and, 'a battery charging system, comprising charging the plurality of the battery modules to the first preset voltage through the first charging circuit;', 'detecting whether the plurality of battery modules have been charged to the first preset voltage through the first charging circuit; and', 'when it is detected that the plurality of battery modules have been charged to the first preset voltage through the first charging circuit, switching off the first charging circuit and, ...

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05-01-2017 дата публикации

Method for the production of an exterior trim panel for a movable body part and a corresponding exterior trim panel with reinforcement by back injecting fibre-reinforced material

Номер: US20170001670A1
Принадлежит: THYSSENKRUPP STEEL EUROPE AG

A method for producing a large outer paneling part for a movable body part of a motor vehicle such as a door, a front hood, or a tailgate may involve using a forming die to form a large metallic panel part into formed panel part having a three-dimensional shape. A reinforcement made of plastic may be applied to at least a portion of an inside of the formed panel part by back injection molding. In some cases, the metallic panel has a sheet metal thickness of less than 0.6 mm, and in some cases less than 0.5 mm. The formed panel part provided with the at least one plastic reinforcement may be connected to an inner structure produced from metal sheet and/or plastic by folding and/or adhesive bonding the plastic reinforcement.

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03-01-2019 дата публикации

METHOD FOR ADJUSTING THE ELASTICITY OF A MATERIAL AND WORKPIECE PRODUCED BY THIS METHOD

Номер: US20190001607A1
Автор: BOESE Till-Falco
Принадлежит: KARLSRUHER INSTITUT FUER TECHNOLOGIE

The present invention relates to a method for adjusting the elasticity of a work material, to a workpiece produced by this method, and to the use thereof. 114.-. (canceled)15. A method for adjusting the elasticity of a work material , wherein the work material comprises two or more materials which are arranged in layers and wherein the layers have different moduli and are arranged so that—starting from a neutral fiber—the layers have decreasing moduli.16. The method of claim 15 , wherein different materials are used as the two or more materials.17. The method of claim 15 , wherein the different moduli comprise different E moduli and/or different G moduli.18. The method of claim 15 , wherein the different moduli comprise different E moduli.19. The method of claim 15 , wherein the different moduli comprise different G moduli.20. The method of claim 15 , wherein the two or more materials comprise materials selected from one or more of natural fibers claim 15 , organic fibers claim 15 , inorganic fibers claim 15 , and metal fibers.21. A work material claim 15 , wherein the work material comprises two or more materials which arranged in layers having different moduli and being arranged so that—starting from a neutral fiber—the layers have decreasing moduli.22. The work material of claim 21 , wherein the different moduli comprise different E moduli and/or different G moduli.23. The work material of claim 21 , wherein the different moduli comprise different E moduli.24. The work material of claim 21 , wherein the different moduli comprise different G moduli.25. The work material of claim 21 , wherein the two or more materials comprise materials selected from one or more of natural fibers claim 21 , organic fibers claim 21 , inorganic fibers claim 21 , and metal fibers.26. The work material of claim 21 , wherein a high tensile fiber is arranged in a middle of the work material.27. The work material of claim 26 , wherein the high tensile fiber is or comprises carbon.28. The ...

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03-01-2019 дата публикации

STRUCTURAL BODY AND CORE

Номер: US20190001613A1
Принадлежит: KABUSHIKI KAISHA TOSHIBA

According to one embodiment, there is provided a structural body including a core composed of fiber and a support, which is a component of the core and is in contact with the core. 110-. (canceled)11. A structural body comprising a stack that includes plural porous layers with a porosity of 45% to 95% including a resin with a density of 0.5 g/cmto 3 g/cmand a fiber with an average diameter of 30 nm or more and less than 5 μm.12. The structural body according to claim 11 , wherein the density is from 1 g/cmto 2 g/cm.13. The structural body according to claim 11 , wherein the porosity of the stack is from 45% to 95%.14. The structural body according to claim 11 , wherein a heat conductivity of the fiber is from 0.01 W/m·K to 5 W/m·K.15. The structural body according to claim 11 , wherein the resin is an epoxy resin.16. (canceled)17. The structural body according to claim 11 , wherein the fiber includes the resin.18. The structural body according to claim 17 , wherein a heat conductivity of the fiber is from 0.01 W/m·K to 5 W/m·K.19. The structural body according to claim 11 , wherein the fiber includes an electrolyte.20. The structural body according to claim 19 , wherein the electrolyte includes LiBr.21. The structural body according to claim 19 , wherein an amount of the electrolyte in the fiber is within a range of 0.01 wt % to 10 wt %.22. The structural body according to claim 20 , wherein an amount of the electrolyte in the fiber is within a range of 0.01 wt % to 10 wt %. This is a Divisional Application of U.S. patent application Ser. No. 15/384,673, filed on Dec. 20, 2016, which is a Continuation Application of PCT Application No. PCT/JP2016/058590, filed Mar. 17, 2016, and is based upon and claims the benefit of priority from Japanese Patent Application No. 2015-053452, filed Mar. 17, 2015, the entire contents of all of which are incorporated herein by reference.Embodiments of the present invention relate to a structural body including a core made of fiber and ...

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03-01-2019 дата публикации

Image containing laminate

Номер: US20190001622A1
Принадлежит: Hewlett Packard Development Co LP

One example provides a method. The method includes printing an image on a surface of laminate, the laminate including: a backing layer; and a transparency disposed over the backing layer. The transparency may have a first side having the image printed thereon and a second side disposed over a first side of the backing layer, the second side opposite the first side. The method may include detaching the second side of the transparency from the first side of the backing layer and reattaching the first side of the transparency to the first side of the backing layer to form a laminated image. The method may include disposing the laminated image over a substrate surface having a curvature.

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03-01-2019 дата публикации

LAMINATED VEHICLE WINDSHIELD WITH INTERNAL LUMINOUS SIGN(S)

Номер: US20190001629A1
Автор: LALUET Jean-Yves
Принадлежит: SAINT-GOBAIN GLASS FRANCE

A laminated vehicle windshield containing internal luminous information includes a first glazing, a lamination interlayer, and a second glazing with a face bearing a first curved organic-light-emitting-diode device that is configured to illuminate the first sign. 1. A laminated vehicle windshield including one or more internal luminous signs , comprising:a first curved glazing with a first main face, which first main face is intended to be on an exterior side of the vehicle, and an opposite second main face;a second curved glazing with a third main face and an opposite fourth main face, which fourth main face is intended to be on an interior side of the vehicle, at least one of the first and second curved glazings being made of mineral glass.said first and second curved glazings being connected together via the second and third main faces by a lamination interlayer made of a thermoformable polymeric material, said lamination interlayer including a first bonding main face toward a side of the second main face and a second bonding main face toward a side of the third main face;a first peripheral layer forming an interior masking layer made of opaque material, which is between the second bonding face and the third main face or which is on the fourth main face;and/or a second peripheral layer forming an exterior masking layer made of opaque material, between the first bonding face and the second main face; anda first light source configured to emit a first emission in the visible spectrum for a first sign made up of one or more symbols and/or one or more letters;wherein the first light source includes a first curved organic-light-emitting-diode (OLED) device, said first curved OLED device being associated with the fourth main face and on a periphery of the fourth main face side, and wherein the first curved OLED device is configured to emit a first emission in the visible spectrum to illuminate the first sign, which is further from the fourth main face than the first ...

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03-01-2019 дата публикации

Method for manufacturing 3d polymer dispersed liquid crystal composite layer structure

Номер: US20190001632A1
Принадлежит: Nanobit Tech Co ltd

The invention provides a method for manufacturing a 3D polymer dispersed liquid crystal (PDLC) composite layer structure. A 3D PDLC composite layer is first provided and has an upper transparent resin substrate, a lower transparent resin substrate, a PDLC layer, an upper protective layer and a lower protective layer. The 3D PDLC composite layer is hot-press molded to form a 3D PDLC composite layer structure with a recess portion, where internal light transmission ratio before hot pressing and after hot pressing are in a range of 0.1%-10%. The upper protective layer and the lower protective layer are removed from the resulting structure.

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03-01-2019 дата публикации

Reinforced polymer laminate

Номер: US20190001650A1
Принадлежит: SABIC Global Technologies BV

A polymer laminate and a method for manufacturing a polymer laminate are disclosed. The polymer laminate includes a first layer having a first surface and a second surface. The first layer includes a first non-porous polymer material. The polymer laminate also includes a second layer on the first surface of the first layer. The second layer includes a first porous polymer material defining a first plurality of pores, and the first non-porous polymer material located within the first plurality of pores.

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