ATE490917T1 - Hintere, untere aerodynamische verkleidung für die befestigungsvorrichtung eines flugzeugmotors - Google Patents
Hintere, untere aerodynamische verkleidung für die befestigungsvorrichtung eines flugzeugmotorsInfo
- Publication number
- ATE490917T1 ATE490917T1 AT08717729T AT08717729T ATE490917T1 AT E490917 T1 ATE490917 T1 AT E490917T1 AT 08717729 T AT08717729 T AT 08717729T AT 08717729 T AT08717729 T AT 08717729T AT E490917 T1 ATE490917 T1 AT E490917T1
- Authority
- AT
- Austria
- Prior art keywords
- fairing
- rear lower
- aircraft engine
- floor
- lower aerodynamic
- Prior art date
Links
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
- B64D29/02—Power-plant nacelles, fairings, or cowlings associated with wings
-
- 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
- Body Structure For Vehicles (AREA)
- Motorcycle And Bicycle Frame (AREA)
- Clamps And Clips (AREA)
- Installation Of Indoor Wiring (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0753890A FR2913665B1 (fr) | 2007-03-16 | 2007-03-16 | Carenage aerodynamique arriere inferieur pour dispositif d'accrochage d'un moteur d'aeronef |
PCT/EP2008/052985 WO2008113737A1 (fr) | 2007-03-16 | 2008-03-13 | Carenage aerodynamique arriere inferieur pour dispositif d' accrochage d' un moteur d' aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE490917T1 true ATE490917T1 (de) | 2010-12-15 |
Family
ID=38446866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT08717729T ATE490917T1 (de) | 2007-03-16 | 2008-03-13 | Hintere, untere aerodynamische verkleidung für die befestigungsvorrichtung eines flugzeugmotors |
Country Status (6)
Country | Link |
---|---|
US (1) | US8118252B2 (de) |
EP (1) | EP2146898B1 (de) |
AT (1) | ATE490917T1 (de) |
DE (1) | DE602008003915D1 (de) |
FR (1) | FR2913665B1 (de) |
WO (1) | WO2008113737A1 (de) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2921342B1 (fr) * | 2007-09-20 | 2010-03-12 | Airbus France | Carenage aerodynamique arriere inferieur pour dispositif d'accrochage d'un moteur d'aeronef |
ES2386136B1 (es) * | 2009-03-30 | 2013-07-25 | Airbus Operations, S.L. | Estructura para el acoplamiento de la carena de una aeronave |
FR2950323B1 (fr) * | 2009-09-22 | 2011-11-04 | Airbus Operations Sas | Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe |
FR2950322B1 (fr) * | 2009-09-22 | 2012-05-25 | Airbus Operations Sas | Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe |
FR2960522B1 (fr) * | 2010-05-27 | 2012-06-29 | Airbus Operations Sas | Procede de fabrication par formage superplastique et par eclissage d'une nervure pour carenage aerodynamique de mat d'accrochage de moteur d'aeronef |
FR2960523B1 (fr) * | 2010-05-27 | 2012-06-29 | Airbus Operations Sas | Procede de fabrication par formage superplastique et par eclissage d'une nervure pour carenage aerodynamique de mat d'accrochage de moteur d'aeronef |
FR2964947B1 (fr) * | 2010-09-22 | 2012-10-12 | Airbus Operations Sas | Carenage aerodynamique arriere pour mat d'accrochage de moteur d'aeronef |
FR2977237B1 (fr) | 2011-06-28 | 2014-11-21 | Airbus Operations Sas | Carenage aerodynamique arriere d'un mat de liaison d'un moteur d'aeronef |
FR2981636B1 (fr) * | 2011-10-19 | 2013-12-27 | Airbus Operations Sas | Carenage aerodynamique arriere pour dispositif d'accrochage d'un moteur d'aeronef, comprenant un bouclier thermique capable de se dilater librement |
FR2982845B1 (fr) * | 2011-11-22 | 2013-12-20 | Airbus Operations Sas | Carenage aerodynamique arriere de mat de moteur d'aeronef |
FR2988688B1 (fr) * | 2012-03-27 | 2014-05-09 | Airbus Operations Sas | Carenage aerodynamique arriere a tenue en temperature amelioree pour mat d'accrochage d'ensemble propulsif d'aeronef |
US9783285B2 (en) | 2012-04-09 | 2017-10-10 | The Boeing Company | Thermal insulation support |
WO2014135948A2 (en) * | 2013-03-06 | 2014-09-12 | Bombardier Inc. | Aft pylon fairing for aircraft |
FR3013678B1 (fr) * | 2013-11-25 | 2015-11-20 | Airbus Operations Sas | Carenage aerodynamique |
FR3013679B1 (fr) * | 2013-11-25 | 2015-11-27 | Airbus Operations Sas | Carenage aerodynamique divise en sous-parties |
JP6371068B2 (ja) * | 2014-02-18 | 2018-08-08 | 三菱航空機株式会社 | 電線構造、および電線の電磁シールド方法 |
WO2015128688A1 (en) | 2014-02-28 | 2015-09-03 | Timothy Bishop | Time display, method of presenting time information and timekeeping devices |
FR3021029B1 (fr) | 2014-05-16 | 2016-05-06 | Airbus Operations Sas | Carenage aerodynamique |
EP3048271B1 (de) * | 2014-12-10 | 2020-05-27 | Rolls-Royce Corporation | Versteifungsrippe |
EP3464864B1 (de) * | 2016-05-30 | 2022-07-27 | Airbus Canada Limited Partnership | Flugzeugmotoranordnung |
US10427776B2 (en) | 2016-07-27 | 2019-10-01 | The Boeing Company | Sliding joint kits, systems containing the same, and related methods |
US10260540B2 (en) * | 2016-09-01 | 2019-04-16 | The Boeing Company | Heat shield flange sliding joint |
US10843787B2 (en) * | 2018-03-29 | 2020-11-24 | The Boeing Company | Heat shield assembly and mounting thereof on aircraft |
US11827373B2 (en) * | 2019-09-27 | 2023-11-28 | The Boeing Company | Aircraft engine exhaust systems enabling reduced length aft strut fairings |
US11781482B2 (en) * | 2021-09-03 | 2023-10-10 | The Boeing Company | Heat shield assembly for use with an aircraft engine |
CN114516404B (zh) * | 2022-02-14 | 2024-04-09 | 中国商用飞机有限责任公司 | 吊挂整流罩 |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4238092A (en) * | 1978-08-17 | 1980-12-09 | Rohr Industries, Inc. | Accessory for a turbine engine |
US4466587A (en) * | 1981-12-21 | 1984-08-21 | General Electric Company | Nacelle installation |
US4712750A (en) * | 1986-05-02 | 1987-12-15 | The Boeing Company | Temperature control device for jet engine nacelle associated structure |
US5524846A (en) * | 1993-12-21 | 1996-06-11 | The Boeing Company | Fire protection system for airplanes |
US5906097A (en) * | 1997-03-28 | 1999-05-25 | The Boeing Company | Engine flow control device |
US6983912B2 (en) * | 2002-04-30 | 2006-01-10 | The Boeing Company | Hybrid exhaust heat shield for pylon mounted gas turbine engines |
-
2007
- 2007-03-16 FR FR0753890A patent/FR2913665B1/fr not_active Expired - Fee Related
-
2008
- 2008-03-13 AT AT08717729T patent/ATE490917T1/de not_active IP Right Cessation
- 2008-03-13 US US12/528,646 patent/US8118252B2/en not_active Expired - Fee Related
- 2008-03-13 DE DE602008003915T patent/DE602008003915D1/de active Active
- 2008-03-13 WO PCT/EP2008/052985 patent/WO2008113737A1/fr active Application Filing
- 2008-03-13 EP EP08717729A patent/EP2146898B1/de not_active Not-in-force
Also Published As
Publication number | Publication date |
---|---|
FR2913665B1 (fr) | 2009-06-05 |
US20100051743A1 (en) | 2010-03-04 |
EP2146898B1 (de) | 2010-12-08 |
EP2146898A1 (de) | 2010-01-27 |
US8118252B2 (en) | 2012-02-21 |
WO2008113737A1 (fr) | 2008-09-25 |
DE602008003915D1 (de) | 2011-01-20 |
FR2913665A1 (fr) | 2008-09-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |