CN101511674B - 用于飞行器的舱门框 - Google Patents
用于飞行器的舱门框 Download PDFInfo
- Publication number
- CN101511674B CN101511674B CN2007800325675A CN200780032567A CN101511674B CN 101511674 B CN101511674 B CN 101511674B CN 2007800325675 A CN2007800325675 A CN 2007800325675A CN 200780032567 A CN200780032567 A CN 200780032567A CN 101511674 B CN101511674 B CN 101511674B
- Authority
- CN
- China
- Prior art keywords
- reinforcing member
- door frame
- hatch door
- collapsible
- aircraft
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 239000002131 composite material Substances 0.000 claims abstract description 26
- 230000003014 reinforcing effect Effects 0.000 claims description 68
- 229920000049 Carbon (fiber) Polymers 0.000 claims description 3
- 239000004917 carbon fiber Substances 0.000 claims description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 claims description 3
- 239000003351 stiffener Substances 0.000 abstract description 3
- 230000003601 intercostal effect Effects 0.000 description 11
- 238000004519 manufacturing process Methods 0.000 description 8
- 238000000034 method Methods 0.000 description 6
- 238000009745 resin transfer moulding Methods 0.000 description 5
- 238000010521 absorption reaction Methods 0.000 description 4
- 230000000694 effects Effects 0.000 description 4
- 239000004744 fabric Substances 0.000 description 4
- 239000000463 material Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 239000004411 aluminium Substances 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000005516 engineering process Methods 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 230000015572 biosynthetic process Effects 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000002655 kraft paper Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 229920005989 resin Polymers 0.000 description 2
- 239000011347 resin Substances 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 229920000271 Kevlar® Polymers 0.000 description 1
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000004761 kevlar Substances 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 150000002739 metals Chemical group 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 238000006116 polymerization reaction Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
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
- B64C1/1407—Doors; surrounding frames
- B64C1/1461—Structures of doors or surrounding frames
-
- 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
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/061—Frames
- B64C1/062—Frames specially adapted to absorb crash loads
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Body Structure For Vehicles (AREA)
- Securing Of Glass Panes Or The Like (AREA)
- Wing Frames And Configurations (AREA)
- Buildings Adapted To Withstand Abnormal External Influences (AREA)
- Seal Device For Vehicle (AREA)
- Lock And Its Accessories (AREA)
Abstract
Description
Claims (10)
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0653233 | 2006-08-01 | ||
FR0653233A FR2904602B1 (fr) | 2006-08-01 | 2006-08-01 | Encadrement de porte pour aeronef |
PCT/FR2007/051735 WO2008015360A1 (fr) | 2006-08-01 | 2007-07-26 | Encadrement de porte pour aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
CN101511674A CN101511674A (zh) | 2009-08-19 |
CN101511674B true CN101511674B (zh) | 2012-06-13 |
Family
ID=37772998
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2007800325675A Expired - Fee Related CN101511674B (zh) | 2006-08-01 | 2007-07-26 | 用于飞行器的舱门框 |
Country Status (11)
Country | Link |
---|---|
US (1) | US8146863B2 (zh) |
EP (1) | EP2046636B1 (zh) |
JP (1) | JP5006931B2 (zh) |
CN (1) | CN101511674B (zh) |
AT (1) | ATE474768T1 (zh) |
BR (1) | BRPI0714579A2 (zh) |
CA (1) | CA2658317C (zh) |
DE (1) | DE602007007953D1 (zh) |
FR (1) | FR2904602B1 (zh) |
RU (1) | RU2424945C2 (zh) |
WO (1) | WO2008015360A1 (zh) |
Families Citing this family (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2923800B1 (fr) * | 2007-11-16 | 2010-05-21 | Airbus France | Dispositif de liaison entre une piece de structure interne d'un aeronef et le fuselage de celui-ci |
DE102008012282A1 (de) * | 2008-03-03 | 2009-09-17 | Airbus Deutschland Gmbh | Rumpfstruktur für Flugzeug |
FR2934562B1 (fr) | 2008-07-31 | 2011-04-22 | Airbus France | Panneau de protection et module de train d'atterissage le comportant. |
US8109551B2 (en) * | 2009-02-04 | 2012-02-07 | New Flyer Industries Canada Ulc | Bus cabin structure |
FR2947241B1 (fr) | 2009-06-29 | 2012-12-07 | Airbus France | Encadrement d'une ouverture menagee dans un fuselage d'aeronef |
DE102009057010B4 (de) | 2009-12-04 | 2018-05-03 | Airbus Defence and Space GmbH | Türpanelanordnung für eine Flugzeugrumpfstruktur und Verfahren zur Herstellung der Rumpfstruktur |
DE102009057012B8 (de) * | 2009-12-04 | 2014-11-27 | Airbus Defence and Space GmbH | Türumgebungsanordnung |
DE102010003497B4 (de) * | 2010-03-31 | 2018-04-05 | Benteler Sgl Gmbh & Co. Kg | Verfahren zur Herstellung eines Aufprallschutzelementes |
ES2400768B1 (es) * | 2010-06-30 | 2014-02-12 | Airbus Operations, S.L. | Estructura interna de aeronave en material compuesto. |
DE102011004844A1 (de) * | 2011-02-28 | 2012-08-30 | Airbus Operations Gmbh | Türrahmenverbund, Rumpfabschnitt sowie Luft- oder Raumfahrzeug |
CN103161392A (zh) * | 2013-03-07 | 2013-06-19 | 苏州市江诚人防设备有限公司 | 超轻防护门 |
DE102014202751B4 (de) | 2014-02-14 | 2020-03-19 | Airbus Operations Gmbh | Innenverkleidungsanordnung für eine Passagierkabine eines Fahrzeugs |
DE102014202783B4 (de) * | 2014-02-14 | 2022-02-24 | Airbus Operations Gmbh | Flugzeugkabinenanordnung |
EP3536602B1 (en) * | 2014-10-16 | 2021-09-15 | Airbus Operations GmbH | Spoiler for an aircraft and associated method |
EP3165447B1 (en) * | 2015-11-09 | 2019-07-17 | Airbus Operations GmbH | Aircraft fuselage structure |
US10144497B2 (en) | 2016-04-18 | 2018-12-04 | The Boeing Company | Hat section door frame with integral gussets |
US10179438B2 (en) | 2016-09-23 | 2019-01-15 | Bell Helicopter Textron Inc. | Method and assembly for manufacturing door skin and wall with doorway |
RU2646175C1 (ru) * | 2016-12-20 | 2018-03-01 | федеральное государственное автономное образовательное учреждение высшего образования "Самарский национальный исследовательский университет имени академика С.П. Королева" | Отсек фюзеляжа летательного аппарата с вырезом под люк |
DE102017126052A1 (de) | 2017-11-08 | 2019-05-09 | Airbus Operations Gmbh | Versteifungsanordnung für eine Öffnung in einer Flugzeugstruktur |
DE102017221048A1 (de) * | 2017-11-24 | 2019-05-29 | Airbus Operations Gmbh | Verfahren zur herstellung eines rahmenbauteils für eine türrahmenstruktur eines luftfahrzeugs, rahmenbauteil sowie türrahmenstruktur |
RU182607U1 (ru) * | 2018-03-30 | 2018-08-23 | Акционерное общество "Корпорация "Стратегические пункты управления" АО "Корпорация "СПУ - ЦКБ ТМ" | Дверное обрамление |
RU187755U1 (ru) * | 2019-01-28 | 2019-03-18 | Акционерное общество "Корпорация "Стратегические пункты управления" АО "Корпорация "СПУ - ЦКБ ТМ" | Дверное обрамление |
FR3093500B1 (fr) * | 2019-03-06 | 2021-07-02 | Latecoere | Porte de cabine pressurisée d’aéronef à armature intérieure de reprise d’efforts |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1607272A (en) * | 1926-11-16 | Statfs patfnt cifficf | ||
EP0346210A1 (fr) * | 1988-06-08 | 1989-12-13 | AEROSPATIALE Société Nationale Industrielle | Cadre en matériau composite notamment pour fuselage d'aéronef, et son procédé de fabrication |
US6488235B1 (en) * | 2001-03-12 | 2002-12-03 | Northrop Grumman Corporation | Flexible structural frame |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US257671A (en) * | 1882-05-09 | Map and chart exhibitor | ||
US2349907A (en) * | 1941-07-09 | 1944-05-30 | Cons Vultee Aircraft Corp | Metal door |
US3638992A (en) * | 1969-12-02 | 1972-02-01 | Lloyd T Forshee | Auto and aircraft safety liners |
US3791073A (en) * | 1972-04-28 | 1974-02-12 | Boeing Co | Aircraft door with moving hinge line |
US5171510A (en) | 1988-06-08 | 1992-12-15 | Aerospatiale Societe Nationale Industrielle | Method of producing a frame made of a composite material, especially for the fuselage of an aircraft |
US6059230A (en) * | 1998-05-08 | 2000-05-09 | Northrop Grumman Corporation | Expandable aircraft door |
US6110567A (en) * | 1999-01-27 | 2000-08-29 | Scaled Composites, Inc. | Composite structural panel having a face sheet reinforced with a channel stiffener grid |
DE10035349C1 (de) * | 2000-07-20 | 2001-09-27 | Eurocopter Deutschland | Flugzeugtür |
GB0023979D0 (en) * | 2000-09-30 | 2000-11-15 | Eastman Kodak Co | Black and white graphic arts film |
AU2003243411A1 (en) * | 2002-06-06 | 2003-12-22 | Remmele Engineering, Inc. | Aircraft door system and method of making and installing the same |
EP1607272B1 (de) * | 2004-06-16 | 2008-08-13 | Jacob Composite GmbH | Bauteil zur Energieaufnahme bei einem Aufprall |
-
2006
- 2006-08-01 FR FR0653233A patent/FR2904602B1/fr not_active Expired - Fee Related
-
2007
- 2007-07-26 US US12/376,085 patent/US8146863B2/en not_active Expired - Fee Related
- 2007-07-26 CA CA2658317A patent/CA2658317C/fr not_active Expired - Fee Related
- 2007-07-26 BR BRPI0714579-9A patent/BRPI0714579A2/pt not_active IP Right Cessation
- 2007-07-26 EP EP07823651A patent/EP2046636B1/fr not_active Not-in-force
- 2007-07-26 RU RU2009107165/11A patent/RU2424945C2/ru not_active IP Right Cessation
- 2007-07-26 DE DE602007007953T patent/DE602007007953D1/de active Active
- 2007-07-26 AT AT07823651T patent/ATE474768T1/de not_active IP Right Cessation
- 2007-07-26 JP JP2009522314A patent/JP5006931B2/ja not_active Expired - Fee Related
- 2007-07-26 WO PCT/FR2007/051735 patent/WO2008015360A1/fr active Application Filing
- 2007-07-26 CN CN2007800325675A patent/CN101511674B/zh not_active Expired - Fee Related
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1607272A (en) * | 1926-11-16 | Statfs patfnt cifficf | ||
EP0346210A1 (fr) * | 1988-06-08 | 1989-12-13 | AEROSPATIALE Société Nationale Industrielle | Cadre en matériau composite notamment pour fuselage d'aéronef, et son procédé de fabrication |
US6488235B1 (en) * | 2001-03-12 | 2002-12-03 | Northrop Grumman Corporation | Flexible structural frame |
Also Published As
Publication number | Publication date |
---|---|
EP2046636B1 (fr) | 2010-07-21 |
RU2424945C2 (ru) | 2011-07-27 |
BRPI0714579A2 (pt) | 2013-05-14 |
CN101511674A (zh) | 2009-08-19 |
JP5006931B2 (ja) | 2012-08-22 |
RU2009107165A (ru) | 2010-09-10 |
FR2904602A1 (fr) | 2008-02-08 |
CA2658317A1 (fr) | 2008-02-07 |
DE602007007953D1 (de) | 2010-09-02 |
US8146863B2 (en) | 2012-04-03 |
US20090308977A1 (en) | 2009-12-17 |
FR2904602B1 (fr) | 2009-04-10 |
WO2008015360A1 (fr) | 2008-02-07 |
ATE474768T1 (de) | 2010-08-15 |
JP2009545482A (ja) | 2009-12-24 |
CA2658317C (fr) | 2013-12-17 |
EP2046636A1 (fr) | 2009-04-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C53 | Correction of patent of invention or patent application | ||
CB02 | Change of applicant information |
Address after: France Toulouse Applicant after: Airbus Operations S.A.S. Address before: France Toulouse Applicant before: Airbus France Address after: France Toulouse Applicant after: Airbus France Address before: France Toulouse Applicant before: Airbus France |
|
COR | Change of bibliographic data |
Free format text: CORRECT: APPLICANT; FROM: AIRBUS FRANCE TO: AIRBUS OPERATIONS GMBH |
|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20120613 Termination date: 20180726 |
|
CF01 | Termination of patent right due to non-payment of annual fee |