BRPI0907756A2 - Janela de aeronave laminada tolerante a dano e suporte de carga - Google Patents
Janela de aeronave laminada tolerante a dano e suporte de cargaInfo
- Publication number
- BRPI0907756A2 BRPI0907756A2 BRPI0907756-1A BRPI0907756A BRPI0907756A2 BR PI0907756 A2 BRPI0907756 A2 BR PI0907756A2 BR PI0907756 A BRPI0907756 A BR PI0907756A BR PI0907756 A2 BRPI0907756 A2 BR PI0907756A2
- Authority
- BR
- Brazil
- Prior art keywords
- damage
- window
- load bearing
- tolerant
- vehicle
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/14—Windows; Doors; Hatch covers or access panels; Surrounding frame structures; Canopies; Windscreens accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers
- B64C1/1476—Canopies; Windscreens or similar transparent elements
- B64C1/1484—Windows
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Laminated Bodies (AREA)
- Rolling Contact Bearings (AREA)
- Memory System Of A Hierarchy Structure (AREA)
- Reinforced Plastic Materials (AREA)
- Securing Of Glass Panes Or The Like (AREA)
- Joining Of Glass To Other Materials (AREA)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US6362508P | 2008-02-05 | 2008-02-05 | |
DE102008007545A DE102008007545A1 (de) | 2008-02-05 | 2008-02-05 | Lasttragendes und schadenstolerantes Laminatflugzeugfenster |
PCT/EP2009/050972 WO2009098159A1 (de) | 2008-02-05 | 2009-01-29 | Lasttragendes und schadenstolerantes laminatflugzeugfenster |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0907756A2 true BRPI0907756A2 (pt) | 2015-07-21 |
Family
ID=40896422
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0907756-1A BRPI0907756A2 (pt) | 2008-02-05 | 2009-01-29 | Janela de aeronave laminada tolerante a dano e suporte de carga |
Country Status (10)
Country | Link |
---|---|
US (1) | US8245975B2 (pt) |
EP (1) | EP2240363B1 (pt) |
JP (1) | JP2011510868A (pt) |
CN (1) | CN101939218B (pt) |
AT (1) | ATE520589T1 (pt) |
BR (1) | BRPI0907756A2 (pt) |
CA (1) | CA2712398A1 (pt) |
DE (1) | DE102008007545A1 (pt) |
RU (1) | RU2483974C2 (pt) |
WO (1) | WO2009098159A1 (pt) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8997416B2 (en) | 2008-07-15 | 2015-04-07 | The Boeing Company | Opaque fiber reinforcement of composites |
DE102009024397B4 (de) * | 2009-06-09 | 2015-10-08 | Airbus Operations Gmbh | Thermisch und/oder mechanisch fügbares Schalenbauteil zur Bildung einer Rumpfzelle eines Flugzeugs |
US9682536B2 (en) * | 2010-12-15 | 2017-06-20 | The Boeing Company | Sandwiched fiber composites for ballistic applications |
US8616500B2 (en) * | 2011-03-04 | 2013-12-31 | The Boeing Company | Diamond shaped window for composite and/or metallic airframe |
US9327458B2 (en) | 2014-09-30 | 2016-05-03 | The Boeing Company | In-situ annealing of polymer fibers |
DE102015110165B4 (de) | 2015-06-24 | 2017-03-02 | Airbus Operations Gmbh | Hautfeldfenstereinheit für ein Luftfahrzeug |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3616122A (en) * | 1969-06-30 | 1971-10-26 | Ppg Industries Inc | Laminated window panels |
GB1406441A (en) * | 1972-03-13 | 1975-09-17 | Triplex Safety Glass Co | Laminated transparent assemblies |
US3919022A (en) * | 1974-02-21 | 1975-11-11 | Ppg Industries Inc | Window panel edge construction |
US5039566A (en) * | 1988-06-27 | 1991-08-13 | Mcdonnell Douglas Corporation | Transparent composite material |
GB2280924B (en) * | 1993-08-10 | 1997-02-26 | Brian See | Structural members |
RU5167U1 (ru) * | 1995-08-08 | 1997-10-16 | Научно-производственное предприятие "Легкая авиация Таганрога" | Самолетное остекление |
GB9817777D0 (en) * | 1998-08-15 | 1998-10-14 | British Aerospace | Composite material construction |
AU6250999A (en) * | 1998-10-06 | 2000-04-26 | Williams International Company, L.L.C. | Aircraft window |
JP4318381B2 (ja) * | 2000-04-27 | 2009-08-19 | 本田技研工業株式会社 | 繊維強化複合材からなる胴体構造体の製造方法、及びそれにより製造される胴体構造体 |
NL1015141C2 (nl) * | 2000-05-09 | 2001-11-13 | Fokker Aerostructures Bv | Verbindingsconstructie in een laminaat uit metalen en kunststof lagen. |
US6818306B2 (en) * | 2002-09-27 | 2004-11-16 | The Boeing Company | Optically clear structural laminate |
US7300693B2 (en) * | 2003-09-04 | 2007-11-27 | The Boeing Company | Resin infused transparent skin panel and method of making same |
DE102005010252A1 (de) * | 2004-08-04 | 2006-03-16 | Schierholt, Johannes, Dipl.-Ing. | Verwendung von Faserverbundwerkstoff-Produktionsverfahren zur Erzeugung von transparenten, frei formbaren, lastaufnehmenden, schadenstoleranten und kratzfesten Strukturen (Fenstern) |
GB2421952B (en) * | 2005-01-07 | 2010-04-21 | Univ Sheffield | Damage Detection System |
DE102006025930B4 (de) * | 2006-06-02 | 2008-09-11 | Airbus Deutschland Gmbh | Rumpfstruktur und Verfahren zur Herstellung einer Rumpfstruktur |
-
2008
- 2008-02-05 DE DE102008007545A patent/DE102008007545A1/de not_active Ceased
-
2009
- 2009-01-29 EP EP09708461A patent/EP2240363B1/de not_active Not-in-force
- 2009-01-29 CN CN2009801046245A patent/CN101939218B/zh not_active Expired - Fee Related
- 2009-01-29 AT AT09708461T patent/ATE520589T1/de active
- 2009-01-29 WO PCT/EP2009/050972 patent/WO2009098159A1/de active Application Filing
- 2009-01-29 CA CA2712398A patent/CA2712398A1/en not_active Abandoned
- 2009-01-29 JP JP2010545437A patent/JP2011510868A/ja active Pending
- 2009-01-29 RU RU2010128457/11A patent/RU2483974C2/ru not_active IP Right Cessation
- 2009-01-29 BR BRPI0907756-1A patent/BRPI0907756A2/pt not_active IP Right Cessation
-
2010
- 2010-07-20 US US12/839,845 patent/US8245975B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20110017871A1 (en) | 2011-01-27 |
CN101939218B (zh) | 2013-11-20 |
RU2483974C2 (ru) | 2013-06-10 |
CA2712398A1 (en) | 2009-08-13 |
EP2240363B1 (de) | 2011-08-17 |
WO2009098159A1 (de) | 2009-08-13 |
EP2240363A1 (de) | 2010-10-20 |
CN101939218A (zh) | 2011-01-05 |
RU2010128457A (ru) | 2012-03-20 |
ATE520589T1 (de) | 2011-09-15 |
JP2011510868A (ja) | 2011-04-07 |
DE102008007545A1 (de) | 2009-08-27 |
US8245975B2 (en) | 2012-08-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0907756A2 (pt) | Janela de aeronave laminada tolerante a dano e suporte de carga | |
BR112013003588A2 (pt) | estruturas compostas possuindo juntas de material composto com metal e método de fabricação das mesmas | |
FR2962175B1 (fr) | Aube a longeron composite integre | |
EP2463083A3 (en) | Green aircraft interior panels and method of fabrication | |
BRPI0923609A2 (pt) | pré-formas integralmente tecida com endurecedores em duas ou mais direções, compósitos reforçados de fibra e métodos de formação de pré-forma integralmente tecida e de compósito reforçado de fibra | |
MX2016016282A (es) | Cristal compuesto, compuesto de un cristal polimerico y un cristal de vidrio. | |
CR20120377A (es) | Sistemas de construcción y paneles compuestos | |
BR112012029510A2 (pt) | método de fabricação de um elemento estrutural, particularmente para uma suspensão de veículo. | |
MX2011010463A (es) | Paneles de espejo solar y su fabricacion. | |
BR112012030065A2 (pt) | elemento de segurança com estruturas de condução de fibra óptica | |
MX2016005141A (es) | Cristal compuesto que consiste de un compuesto de un cristal polimerico y un cristal de vidrio. | |
WO2011159028A3 (ko) | 터치 패널 디스플레이 장치 | |
CO6761347A2 (es) | Luna de vidrio blindado teniendo refuerzo de borde | |
MX355178B (es) | Vidrio laminado resistente a las balas. | |
BR112013009979A2 (pt) | estrutura plástica de camadas múltiplas tendo baixa transmissão de energia | |
WO2011080320A3 (de) | Luft- oder raumfahrzeughülle | |
EA201291389A1 (ru) | Изолирующий стеклопакет | |
MX2014013299A (es) | Capa de deslizamiento y elemento de deslizamiento con una capa de deslizamiento de este tipo. | |
BR112015014255A2 (pt) | materiais compósitos reforçados por fibras e carregados com partículas | |
WO2011131700A3 (de) | Abstandhalter | |
ATE524377T1 (de) | Verstärkte platte | |
WO2011073423A3 (de) | Solarmodule mit verbesserten korrosionseigenschaften | |
RU2771543C2 (ru) | Авиационное ламинированное остекление с высокой стойкостью к разрушению при столкновении с птицами | |
ATE455035T1 (de) | Selbststabilisierte versteifung | |
BRPI0919003A2 (pt) | painel sanduíche composto e elemento para uma aeronave. |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE AS 6A E 7A ANUIDADES. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2344 DE 08-12-2015 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |