ATE481320T1 - Motoranordnung für ein luftfahrzeug mit an zwei getrennten elementen angebrachter aerodynamischer kupplungsverteilung - Google Patents
Motoranordnung für ein luftfahrzeug mit an zwei getrennten elementen angebrachter aerodynamischer kupplungsverteilungInfo
- Publication number
- ATE481320T1 ATE481320T1 AT07787297T AT07787297T ATE481320T1 AT E481320 T1 ATE481320 T1 AT E481320T1 AT 07787297 T AT07787297 T AT 07787297T AT 07787297 T AT07787297 T AT 07787297T AT E481320 T1 ATE481320 T1 AT E481320T1
- Authority
- AT
- Austria
- Prior art keywords
- engine
- aircraft
- aerodynamic
- separate elements
- engine arrangement
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C7/00—Structures or fairings not otherwise provided for
- B64C7/02—Nacelles
-
- 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
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/40—Arrangements for mounting power plants in aircraft
- B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
-
- 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
- B64D29/08—Inspection panels for power plants
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Mechanical Operated Clutches (AREA)
- Connection Of Plates (AREA)
- Arrangement And Driving Of Transmission Devices (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0652912A FR2903666B1 (fr) | 2006-07-11 | 2006-07-11 | Ensemble moteur pour aeronef comprenant un capotage aerodynamique de jonction monte sur deux elements distincts |
PCT/EP2007/057022 WO2008006826A1 (fr) | 2006-07-11 | 2007-07-10 | Ensemble moteur pour aeronef comprenant un capotage aerodynamique de jonction monte sur deux elements distincts |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE481320T1 true ATE481320T1 (de) | 2010-10-15 |
Family
ID=37890405
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07787297T ATE481320T1 (de) | 2006-07-11 | 2007-07-10 | Motoranordnung für ein luftfahrzeug mit an zwei getrennten elementen angebrachter aerodynamischer kupplungsverteilung |
Country Status (11)
Country | Link |
---|---|
US (1) | US8162254B2 (de) |
EP (1) | EP2038176B1 (de) |
JP (1) | JP2009542518A (de) |
CN (1) | CN101484359B (de) |
AT (1) | ATE481320T1 (de) |
BR (1) | BRPI0714033A2 (de) |
CA (1) | CA2657402C (de) |
DE (1) | DE602007009232D1 (de) |
FR (1) | FR2903666B1 (de) |
RU (1) | RU2433070C2 (de) |
WO (1) | WO2008006826A1 (de) |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2920409B1 (fr) * | 2007-08-27 | 2009-12-18 | Airbus France | Berceau de support de capot de soufflante monte sur le mat d'accrochage et sur l'entree d'air de la nacelle |
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 |
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 |
FR2959487B1 (fr) * | 2010-04-29 | 2012-04-13 | Aircelle Sa | Nacelle pour moteur d'aeronef |
US8727269B2 (en) * | 2011-06-06 | 2014-05-20 | General Electric Company | System and method for mounting an aircraft engine |
FR2978730B1 (fr) * | 2011-08-03 | 2013-09-27 | Airbus Operations Sas | Berceau d'articulation de capots de soufflante supportes par ces capots en position fermee |
FR2979613B1 (fr) * | 2011-09-01 | 2014-06-13 | Snecma | Ensemble forme par un turbomoteur et son systeme d'attache a une structure d'aeronef |
US9051057B2 (en) * | 2011-12-28 | 2015-06-09 | Embraer S.A. | Aircraft air inlet diverter assemblies with improved aerodynamic characteristics |
CN103523235B (zh) * | 2012-07-06 | 2015-12-02 | 哈尔滨飞机工业集团有限责任公司 | 飞机发动机舱进气道整流罩 |
US8979020B2 (en) * | 2013-06-07 | 2015-03-17 | Pratt & Whitney Canada Corp. | Mounting system for mounting engine nacelle components and associated method |
US10144524B2 (en) * | 2013-06-14 | 2018-12-04 | Rohr, Inc. | Assembly for mounting a turbine engine to a pylon |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
CN103612769B (zh) * | 2013-10-24 | 2016-09-21 | 中国商用飞机有限责任公司 | 翼吊布局飞机中吊挂的整流罩结构 |
US20150321766A1 (en) * | 2014-05-06 | 2015-11-12 | The Boeing Company | Nacelle-To-Pylon Fairing |
US10000293B2 (en) | 2015-01-23 | 2018-06-19 | General Electric Company | Gas-electric propulsion system for an aircraft |
US9884687B2 (en) | 2015-09-21 | 2018-02-06 | General Electric Company | Non-axis symmetric aft engine |
US9637217B2 (en) | 2015-09-21 | 2017-05-02 | General Electric Company | Aircraft having an aft engine |
US9821917B2 (en) | 2015-09-21 | 2017-11-21 | General Electric Company | Aft engine for an aircraft |
US9815560B2 (en) * | 2015-09-21 | 2017-11-14 | General Electric Company | AFT engine nacelle shape for an aircraft |
US9957055B2 (en) | 2015-09-21 | 2018-05-01 | General Electric Company | Aft engine for an aircraft |
US10017270B2 (en) | 2015-10-09 | 2018-07-10 | General Electric Company | Aft engine for an aircraft |
US9764848B1 (en) | 2016-03-07 | 2017-09-19 | General Electric Company | Propulsion system for an aircraft |
US10392119B2 (en) | 2016-04-11 | 2019-08-27 | General Electric Company | Electric propulsion engine for an aircraft |
US10392120B2 (en) | 2016-04-19 | 2019-08-27 | General Electric Company | Propulsion engine for an aircraft |
US10252810B2 (en) | 2016-04-19 | 2019-04-09 | General Electric Company | Propulsion engine for an aircraft |
US10252790B2 (en) * | 2016-08-11 | 2019-04-09 | General Electric Company | Inlet assembly for an aircraft aft fan |
US10259565B2 (en) * | 2016-08-11 | 2019-04-16 | General Electric Company | Inlet assembly for an aircraft aft fan |
US11105340B2 (en) | 2016-08-19 | 2021-08-31 | General Electric Company | Thermal management system for an electric propulsion engine |
US10800539B2 (en) * | 2016-08-19 | 2020-10-13 | General Electric Company | Propulsion engine for an aircraft |
US10676205B2 (en) | 2016-08-19 | 2020-06-09 | General Electric Company | Propulsion engine for an aircraft |
US10071811B2 (en) | 2016-08-22 | 2018-09-11 | General Electric Company | Embedded electric machine |
US10093428B2 (en) | 2016-08-22 | 2018-10-09 | General Electric Company | Electric propulsion system |
US10487839B2 (en) | 2016-08-22 | 2019-11-26 | General Electric Company | Embedded electric machine |
US10308366B2 (en) | 2016-08-22 | 2019-06-04 | General Electric Company | Embedded electric machine |
FR3058704B1 (fr) * | 2016-11-14 | 2018-11-16 | Safran Aircraft Engines | Berceau bipartite a coulissement pour turbopropulseur |
US10793281B2 (en) | 2017-02-10 | 2020-10-06 | General Electric Company | Propulsion system for an aircraft |
US11149578B2 (en) | 2017-02-10 | 2021-10-19 | General Electric Company | Propulsion system for an aircraft |
US10822103B2 (en) | 2017-02-10 | 2020-11-03 | General Electric Company | Propulsor assembly for an aircraft |
US10137981B2 (en) | 2017-03-31 | 2018-11-27 | General Electric Company | Electric propulsion system for an aircraft |
US10762726B2 (en) | 2017-06-13 | 2020-09-01 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
FR3072946A1 (fr) | 2017-10-27 | 2019-05-03 | Airbus Operations | Structure primaire de mat de support d'un groupe propulseur d'aeronef en caisson formee par assemblage de deux demi-coquilles |
FR3079215B1 (fr) * | 2018-03-22 | 2020-11-20 | Airbus Operations Sas | Carenage avant d'un mat d'aeronef comprenant une coiffe mobile et aeronef equipe dudit carenage avant |
FR3081837B1 (fr) * | 2018-06-05 | 2020-11-27 | Airbus Operations Sas | Ensemble turbomachine d'aeronef comportant un capot articule |
US11156128B2 (en) | 2018-08-22 | 2021-10-26 | General Electric Company | Embedded electric machine |
FR3085353A1 (fr) * | 2018-09-04 | 2020-03-06 | Airbus Operations | Ensemble turbomachine d'aeronef comportant un capot articule |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
FR3089954B1 (fr) * | 2018-12-12 | 2021-01-08 | Airbus Operations Sas | Ensemble de motorisation pour un aeronef comprenant un support de charge |
FR3090581A1 (fr) | 2018-12-21 | 2020-06-26 | Airbus Operations (S.A.S.) | Ensemble propulsif d’un aéronef comprenant un carénage de jonction entre une nacelle et un mât de l’aéronef équipé d’un capot amovible et aéronef équipé dudit ensemble propulsif |
FR3096352B1 (fr) * | 2019-05-24 | 2021-06-11 | Airbus Operations Sas | Ensemble de motorisation pour un aeronef comprenant un support de charge |
US11548653B2 (en) * | 2019-10-08 | 2023-01-10 | Rohr, Inc. | Support structure for inner cowls of an aircraft propulsion system |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1533551A (en) * | 1974-11-08 | 1978-11-29 | Gen Electric | Gas turbofan engines |
US4147029A (en) * | 1976-01-02 | 1979-04-03 | General Electric Company | Long duct mixed flow gas turbine engine |
US4458863A (en) * | 1980-03-10 | 1984-07-10 | The Boeing Company | Strut supported inlet |
US4603821A (en) * | 1983-12-30 | 1986-08-05 | The Boeing Company | System for mounting a jet engine |
US4825648A (en) * | 1987-03-02 | 1989-05-02 | General Electric Company | Turbofan engine having a split cowl |
US5524847A (en) * | 1993-09-07 | 1996-06-11 | United Technologies Corporation | Nacelle and mounting arrangement for an aircraft engine |
FR2734540B1 (fr) * | 1995-05-24 | 1997-08-08 | Aerospatiale | Nacelle de moteur d'aeronef comportant un capot de nacelle |
KR970021800A (ko) * | 1995-10-09 | 1997-05-28 | 패트릭 에스. 랭커스터 | 동력학적으로 균형잡힌 구동축 조립체 및 그것을 균형잡는 방법 |
US5864922A (en) * | 1996-08-08 | 1999-02-02 | The Boeing Company | Self centering hinge |
FR2772342B1 (fr) * | 1997-12-16 | 2000-02-18 | Aerospatiale | Ensemble propulseur a capots de soufflante munis de securites de maintien et de positionnement, pour aeronef |
CN1258462C (zh) * | 2003-01-15 | 2006-06-07 | 肖立峰 | 旋流喷气飞行器 |
FR2856379B1 (fr) | 2003-06-18 | 2006-11-24 | Airbus France | Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit |
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. |
-
2006
- 2006-07-11 FR FR0652912A patent/FR2903666B1/fr not_active Expired - Fee Related
-
2007
- 2007-07-10 DE DE602007009232T patent/DE602007009232D1/de active Active
- 2007-07-10 US US12/307,142 patent/US8162254B2/en active Active
- 2007-07-10 RU RU2009104473/11A patent/RU2433070C2/ru not_active IP Right Cessation
- 2007-07-10 CA CA2657402A patent/CA2657402C/en not_active Expired - Fee Related
- 2007-07-10 JP JP2009518875A patent/JP2009542518A/ja active Pending
- 2007-07-10 EP EP07787297A patent/EP2038176B1/de not_active Ceased
- 2007-07-10 AT AT07787297T patent/ATE481320T1/de not_active IP Right Cessation
- 2007-07-10 WO PCT/EP2007/057022 patent/WO2008006826A1/fr active Application Filing
- 2007-07-10 CN CN2007800255738A patent/CN101484359B/zh not_active Expired - Fee Related
- 2007-07-10 BR BRPI0714033-9A patent/BRPI0714033A2/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2657402C (en) | 2014-10-14 |
JP2009542518A (ja) | 2009-12-03 |
RU2009104473A (ru) | 2010-08-20 |
CN101484359A (zh) | 2009-07-15 |
CN101484359B (zh) | 2011-05-11 |
RU2433070C2 (ru) | 2011-11-10 |
FR2903666B1 (fr) | 2008-10-10 |
BRPI0714033A2 (pt) | 2012-12-18 |
DE602007009232D1 (de) | 2010-10-28 |
US8162254B2 (en) | 2012-04-24 |
CA2657402A1 (en) | 2008-01-17 |
FR2903666A1 (fr) | 2008-01-18 |
WO2008006826A1 (fr) | 2008-01-17 |
EP2038176A1 (de) | 2009-03-25 |
EP2038176B1 (de) | 2010-09-15 |
US20090283631A1 (en) | 2009-11-19 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE481320T1 (de) | Motoranordnung für ein luftfahrzeug mit an zwei getrennten elementen angebrachter aerodynamischer kupplungsverteilung | |
DE602007003362D1 (de) | Triebwerksanordnung für ein flugzeug mit stützgestell für eine auf zwei separaten elementen montierte lüfterhaube | |
ATE452823T1 (de) | Strukturgondel | |
BRPI0815705A2 (pt) | Conjunto motor para aeronave, e, aeronave. | |
WO2008043903A3 (fr) | Nacelle pour turboréacteur double flux | |
RU2009125710A (ru) | Гондола для двухконтурного турбореактивного двигателя | |
EP2051009A3 (de) | Keramische Brennkammerauskleidung für einen Gasturbinenmotor | |
DE602007004959D1 (de) | Abdeckstruktur für einen lufteinlass | |
EP2251540A3 (de) | Montagesystem für Zweistromtriebwerk | |
BRPI0811239A2 (pt) | Conjunto motor para aeronave, e, aeronave | |
UA88281C2 (ru) | Модуль турбины для газотурбинного двигателя, компрессор, соединенный с модулем, газотурбинный двигатель, который содержит модуль турбины | |
FR2980173B1 (fr) | Ensemble arriere de nacelle pour turboreacteur | |
ATE428632T1 (de) | Flugzeugmotoranordnung | |
GB2478500A (en) | Turbine blade assembly including a damper | |
RU2008149987A (ru) | Выступающая часть промежуточного корпуса, предназначенная для авиационного реактивного двигателя, содержащая разделенную на секторы кольцевую канавку для вмещения крышек гондолы | |
ATE444896T1 (de) | Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel | |
ATE445771T1 (de) | Triebwerk für ein flugzeug | |
ATE392361T1 (de) | Seitenleitwerkeinheit für flugzeug und damit versehenes flugzeug | |
ATE538033T1 (de) | Gondelrückseitenbaugruppe für einen turbostrahlmotor | |
EP2537755A3 (de) | Montageanordnung | |
EP2128402A3 (de) | Nacelleanordnung einer Gasturbine | |
GB2415749B (en) | A gas turbine engine including an exhaust duct comprising a diffuser for diffusing the exhaust gas produced by the engine | |
RU2011116970A (ru) | Гондола турбореактивного двигателя | |
EP2155555A4 (de) | Montageelement für einen gasturbinenmotor sowie struktur und flugzeug mit einem solchen montageelement | |
US9611758B2 (en) | Gas turbine engine systems involving integrated fluid conduits |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |