ATE543730T1 - Vorrichtung zum umgurten einer flugzeuggondel - Google Patents
Vorrichtung zum umgurten einer flugzeuggondelInfo
- Publication number
- ATE543730T1 ATE543730T1 AT09737057T AT09737057T ATE543730T1 AT E543730 T1 ATE543730 T1 AT E543730T1 AT 09737057 T AT09737057 T AT 09737057T AT 09737057 T AT09737057 T AT 09737057T AT E543730 T1 ATE543730 T1 AT E543730T1
- Authority
- AT
- Austria
- Prior art keywords
- cap
- flexible element
- door
- integral
- straping
- Prior art date
Links
- 238000004873 anchoring Methods 0.000 abstract 3
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/06—Attaching of nacelles, fairings or cowlings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Wind Motors (AREA)
- Structure Of Belt Conveyors (AREA)
- Shaping Of Tube Ends By Bending Or Straightening (AREA)
- Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0854892A FR2933956B1 (fr) | 2008-07-18 | 2008-07-18 | Dispositif pour ceinturer une nacelle d'aeronef |
PCT/FR2009/051401 WO2010007311A1 (fr) | 2008-07-18 | 2009-07-15 | Dispositif pour ceinturer une nacelle d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE543730T1 true ATE543730T1 (de) | 2012-02-15 |
Family
ID=40451242
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT09737057T ATE543730T1 (de) | 2008-07-18 | 2009-07-15 | Vorrichtung zum umgurten einer flugzeuggondel |
Country Status (10)
Country | Link |
---|---|
US (1) | US8757546B2 (de) |
EP (1) | EP2310269B1 (de) |
JP (1) | JP5532448B2 (de) |
CN (1) | CN102131702B (de) |
AT (1) | ATE543730T1 (de) |
BR (1) | BRPI0911008A2 (de) |
CA (1) | CA2731131C (de) |
FR (1) | FR2933956B1 (de) |
RU (1) | RU2496686C2 (de) |
WO (1) | WO2010007311A1 (de) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966433B1 (fr) * | 2010-10-26 | 2012-12-07 | Airbus Operations Sas | Capot d'aeronef incorporant des moyens pour limiter les phenomenes d'ecope de type pneumatique |
FR3000721B1 (fr) * | 2013-01-09 | 2016-10-14 | Airbus Operations Sas | Ensemble propulsif d'aeronef comprenant un carenage aerodynamique arriere de mat d'accrochage a parois laterales profilees pour l'injection d'air frais le long d'un plancher de protection thermique |
WO2014151275A1 (en) | 2013-03-15 | 2014-09-25 | United Technologies Corporation | Nacelle mounted latching system |
US10508566B2 (en) * | 2015-03-29 | 2019-12-17 | Rohr, Inc. | Inner fixed structure leading edge latch |
US10618645B2 (en) | 2015-08-25 | 2020-04-14 | Aerovironment, Inc. | Ganged servo flight control system for an unmanned aerial vehicle |
US11046446B2 (en) | 2017-03-02 | 2021-06-29 | Bell Helicopter Textron Inc. | Tiltrotor aircraft rotating proprotor assembly |
US10994853B2 (en) | 2017-03-02 | 2021-05-04 | Bell Helicopter Textron Inc. | Tiltrotor aircraft rotating proprotor assembly |
FR3063714B1 (fr) * | 2017-03-07 | 2019-03-29 | Airbus Operations | Nacelle d'aeronef comportant un capot monte rotatif autour de l'axe longitudinal de la nacelle |
US10875627B2 (en) | 2018-05-01 | 2020-12-29 | Bell Helicopter Textron Inc. | Movable cover for a proprotor nacelle |
FR3121429A1 (fr) * | 2021-04-02 | 2022-10-07 | Airbus Operations | Nacelle d’aéronef comportant un système de joint avec ressort pour une casquette de ladite nacelle |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3119581A (en) * | 1960-06-18 | 1964-01-28 | Dunlop Rubber Co | Securing means for inflatable inlet device |
JPS5311760B2 (de) * | 1972-03-18 | 1978-04-24 | ||
US4549708A (en) * | 1982-08-31 | 1985-10-29 | United Technologies Corporation | Cowling latch system |
JP2510444Y2 (ja) * | 1989-08-15 | 1996-09-11 | 住友重機械工業株式会社 | 分離装置 |
US5088775A (en) * | 1990-07-27 | 1992-02-18 | General Electric Company | Seal ring with flanged end portions |
US5350136A (en) * | 1993-05-14 | 1994-09-27 | United Technologies Corporation | Nacelle arrangement |
US6629712B2 (en) * | 2001-03-30 | 2003-10-07 | Hartwell Corporation | Extendable latch |
RU2210523C1 (ru) * | 2001-12-14 | 2003-08-20 | Открытое акционерное общество "Авиационный комплекс им. С.В. Ильюшина" | Гондола силовой установки летательного аппарата |
FR2861364B1 (fr) * | 2003-10-22 | 2006-02-03 | Airbus France | Dispositif de montage d'un carenage dispose entre une entree d'air d'un moteur d'aeronef et un mat. |
-
2008
- 2008-07-18 FR FR0854892A patent/FR2933956B1/fr not_active Expired - Fee Related
-
2009
- 2009-07-15 JP JP2011517974A patent/JP5532448B2/ja not_active Expired - Fee Related
- 2009-07-15 BR BRPI0911008A patent/BRPI0911008A2/pt not_active IP Right Cessation
- 2009-07-15 CN CN200980128903.5A patent/CN102131702B/zh not_active Expired - Fee Related
- 2009-07-15 US US13/054,290 patent/US8757546B2/en not_active Expired - Fee Related
- 2009-07-15 WO PCT/FR2009/051401 patent/WO2010007311A1/fr active Application Filing
- 2009-07-15 CA CA2731131A patent/CA2731131C/fr not_active Expired - Fee Related
- 2009-07-15 EP EP09737057A patent/EP2310269B1/de not_active Not-in-force
- 2009-07-15 RU RU2011106025/11A patent/RU2496686C2/ru not_active IP Right Cessation
- 2009-07-15 AT AT09737057T patent/ATE543730T1/de active
Also Published As
Publication number | Publication date |
---|---|
US8757546B2 (en) | 2014-06-24 |
RU2496686C2 (ru) | 2013-10-27 |
FR2933956A1 (fr) | 2010-01-22 |
CN102131702B (zh) | 2014-03-19 |
FR2933956B1 (fr) | 2010-07-30 |
CA2731131A1 (fr) | 2010-01-21 |
US20110114796A1 (en) | 2011-05-19 |
EP2310269A1 (de) | 2011-04-20 |
JP2011528298A (ja) | 2011-11-17 |
WO2010007311A1 (fr) | 2010-01-21 |
CN102131702A (zh) | 2011-07-20 |
RU2011106025A (ru) | 2012-08-27 |
CA2731131C (fr) | 2016-09-13 |
EP2310269B1 (de) | 2012-02-01 |
BRPI0911008A2 (pt) | 2015-10-06 |
JP5532448B2 (ja) | 2014-06-25 |
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