ATE444896T1 - Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel - Google Patents
Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügelInfo
- Publication number
- ATE444896T1 ATE444896T1 AT07788901T AT07788901T ATE444896T1 AT E444896 T1 ATE444896 T1 AT E444896T1 AT 07788901 T AT07788901 T AT 07788901T AT 07788901 T AT07788901 T AT 07788901T AT E444896 T1 ATE444896 T1 AT E444896T1
- Authority
- AT
- Austria
- Prior art keywords
- turbine engine
- fan casing
- suspensing
- mast
- covering
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
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
-
- 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
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/16—Aircraft characterised by the type or position of power plants of jet type
- B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Catching Or Destruction (AREA)
- Micromachines (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Toys (AREA)
- Tires In General (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0605448A FR2902406B1 (fr) | 2006-06-20 | 2006-06-20 | Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef |
PCT/FR2007/001009 WO2007147965A2 (fr) | 2006-06-20 | 2007-06-18 | Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE444896T1 true ATE444896T1 (de) | 2009-10-15 |
Family
ID=37726661
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT07788901T ATE444896T1 (de) | 2006-06-20 | 2007-06-18 | Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel |
Country Status (11)
Country | Link |
---|---|
US (1) | US8366039B2 (de) |
EP (1) | EP2029429B1 (de) |
JP (1) | JP5097772B2 (de) |
CN (1) | CN101472797B (de) |
AT (1) | ATE444896T1 (de) |
BR (1) | BRPI0712635A2 (de) |
CA (1) | CA2653067C (de) |
DE (1) | DE602007002714D1 (de) |
FR (1) | FR2902406B1 (de) |
RU (1) | RU2391260C1 (de) |
WO (1) | WO2007147965A2 (de) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8769924B2 (en) * | 2008-05-30 | 2014-07-08 | United Technologies Corporation | Gas turbine engine assembly including accessory components within the nacelle |
FR2948635B1 (fr) * | 2009-07-31 | 2011-08-26 | Airbus Operations Sas | Assemblage pour aeronef comprenant un mat d'accrochage de turbomachine dont les moyens d'attache sur la voilure sont agences en t |
FR2961173B1 (fr) | 2010-06-09 | 2012-06-22 | Airbus Operations Sas | Nacelle incorporant une entree d'air au niveau d'une casquette |
CN102826218B (zh) * | 2012-09-11 | 2016-06-15 | 江西洪都航空工业集团有限责任公司 | 一种双发飞机后体整流结构 |
US9404507B2 (en) * | 2013-04-15 | 2016-08-02 | Mra Systems, Inc. | Inner cowl structure for aircraft turbine engine |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
CN103569367B (zh) * | 2013-11-13 | 2015-08-26 | 中国航空工业集团公司西安飞机设计研究所 | 机翼吊装涡扇发动机飞机的发动机挂架 |
US9656761B2 (en) | 2014-04-30 | 2017-05-23 | The Boeing Company | Lipskin for a nacelle and methods of making the same |
US9604438B2 (en) | 2014-04-30 | 2017-03-28 | The Boeing Company | Methods and apparatus for noise attenuation in an engine nacelle |
US9938852B2 (en) | 2014-04-30 | 2018-04-10 | The Boeing Company | Noise attenuating lipskin assembly and methods of assembling the same |
US9708072B2 (en) * | 2014-04-30 | 2017-07-18 | The Boeing Company | Aircraft engine nacelle bulkheads and methods of assembling the same |
US20150321766A1 (en) * | 2014-05-06 | 2015-11-12 | The Boeing Company | Nacelle-To-Pylon Fairing |
JP6437347B2 (ja) * | 2015-02-27 | 2018-12-12 | 三菱重工業株式会社 | 推力発生装置及び航空機 |
US20160356180A1 (en) * | 2015-06-03 | 2016-12-08 | The Boeing Company | Nacelle inlet having an angle or curved aft bulkhead |
FR3040043B1 (fr) | 2015-08-12 | 2019-04-12 | Sogeclair Sa | Mat de moteur d'aeronef a ossature multifonctionnelle integree |
US9896217B2 (en) * | 2016-01-07 | 2018-02-20 | The Boeing Company | Enhanced performance jet engine mounting struts |
US10611490B2 (en) * | 2016-11-02 | 2020-04-07 | Rohr, Inc. | Fan cowl fairing restraining system |
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 |
FR3085353A1 (fr) * | 2018-09-04 | 2020-03-06 | Airbus Operations | Ensemble turbomachine d'aeronef comportant un capot articule |
CN109163624B (zh) * | 2018-09-27 | 2024-02-13 | 宁波天擎航天科技有限公司 | 一种可分离的火箭推进系统 |
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 |
CN110439707B (zh) * | 2019-07-26 | 2021-10-01 | 中国航发沈阳发动机研究所 | 一种飞机尾部弹性片组件 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3318554A (en) * | 1964-09-22 | 1967-05-09 | Rolls Royce | Mounting arrangement for engines |
GB1318748A (en) | 1970-08-11 | 1973-05-31 | Secr Defence | Gas turgine ducted fan engines for aircraft |
GB1516980A (en) * | 1974-12-24 | 1978-07-05 | Rolls Royce | Mounting ducted fan gas turbine engines on aircraft |
US4603821A (en) * | 1983-12-30 | 1986-08-05 | The Boeing Company | System for mounting a jet engine |
FR2661213B1 (fr) | 1990-04-19 | 1992-07-03 | Snecma | Moteur d'aviation a tres grand taux de dilution et du type dit contrafan avant. |
US5524847A (en) * | 1993-09-07 | 1996-06-11 | United Technologies Corporation | Nacelle and mounting arrangement for an aircraft engine |
FR2730275B1 (fr) * | 1995-02-03 | 1997-03-28 | Aerospatiale | Dispositif d'etancheite entre une entree d'air et un carter de soufflante de turboreacteur a double flux |
FR2732074B1 (fr) * | 1995-03-21 | 1997-06-06 | Aerospatiale | Turboreacteur a double flux a nacelle flottante |
GB9602130D0 (en) * | 1996-02-02 | 1996-04-03 | Rolls Royce Plc | Improved method of combining ducted fan gas turbine engine modules and aircraft structure |
US6659878B2 (en) * | 2001-03-30 | 2003-12-09 | General Electric Company | Method and apparatus for coupling male threads to female threads |
GB2375513B (en) * | 2001-05-19 | 2005-03-23 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
US6652222B1 (en) * | 2002-09-03 | 2003-11-25 | Pratt & Whitney Canada Corp. | Fan case design with metal foam between Kevlar |
FR2851226B1 (fr) * | 2003-02-19 | 2005-05-20 | Snecma Moteurs | Structure porteuse pour un turbopropulseur et ensemble comportant une telle structure porteuse |
US7090165B2 (en) * | 2003-06-02 | 2006-08-15 | Rolls-Royce Plc | Aeroengine nacelle |
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. |
US8033094B2 (en) * | 2004-12-01 | 2011-10-11 | United Technologies Corporation | Cantilevered tip turbine engine |
GB0608983D0 (en) * | 2006-05-06 | 2006-06-14 | Rolls Royce Plc | Aeroengine mount |
-
2006
- 2006-06-20 FR FR0605448A patent/FR2902406B1/fr not_active Expired - Fee Related
-
2007
- 2007-06-18 RU RU2009101507/11A patent/RU2391260C1/ru not_active IP Right Cessation
- 2007-06-18 WO PCT/FR2007/001009 patent/WO2007147965A2/fr active Application Filing
- 2007-06-18 EP EP07788901A patent/EP2029429B1/de active Active
- 2007-06-18 BR BRPI0712635-2A patent/BRPI0712635A2/pt not_active Application Discontinuation
- 2007-06-18 DE DE602007002714T patent/DE602007002714D1/de active Active
- 2007-06-18 CA CA2653067A patent/CA2653067C/fr not_active Expired - Fee Related
- 2007-06-18 AT AT07788901T patent/ATE444896T1/de not_active IP Right Cessation
- 2007-06-18 JP JP2009515913A patent/JP5097772B2/ja not_active Expired - Fee Related
- 2007-06-18 US US12/305,903 patent/US8366039B2/en active Active
- 2007-06-18 CN CN2007800226595A patent/CN101472797B/zh active Active
Also Published As
Publication number | Publication date |
---|---|
BRPI0712635A2 (pt) | 2012-05-29 |
US8366039B2 (en) | 2013-02-05 |
EP2029429B1 (de) | 2009-10-07 |
DE602007002714D1 (de) | 2009-11-19 |
US20100176250A1 (en) | 2010-07-15 |
FR2902406A1 (fr) | 2007-12-21 |
WO2007147965A3 (fr) | 2008-02-14 |
CN101472797B (zh) | 2011-07-06 |
WO2007147965A2 (fr) | 2007-12-27 |
RU2391260C1 (ru) | 2010-06-10 |
CN101472797A (zh) | 2009-07-01 |
JP2009541115A (ja) | 2009-11-26 |
FR2902406B1 (fr) | 2008-07-18 |
CA2653067A1 (fr) | 2007-12-27 |
JP5097772B2 (ja) | 2012-12-12 |
EP2029429A2 (de) | 2009-03-04 |
CA2653067C (fr) | 2013-12-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ATE444896T1 (de) | Verkleidung für einen mast zur aufhängung eines turbinenmotors von einem flugzeugflügel | |
ATE452823T1 (de) | Strukturgondel | |
WO2008093003A8 (fr) | Nacelle pour turboréacteur double flux | |
RU2011121662A (ru) | Самолет с двигателями, частично интегрированными в фюзеляж | |
RU2009104473A (ru) | Силовая установка летательного аппарата, содержащая соединительный аэродинамический обтекатель, смонтированный на двух отдельных элементах | |
BRPI0815705A2 (pt) | Conjunto motor para aeronave, e, aeronave. | |
MX2009005314A (es) | Sistema aplicado a las rejillas frontales y posteriores de ventiladores. | |
EP2241504A3 (de) | Flugzeugtriebwerkgondel | |
EP2080700A3 (de) | Pylon- und Motorträgerkonfiguration | |
GB0606518D0 (en) | Aircraft with aerodynamic lift generating device | |
RU2728673C2 (ru) | Защитный элемент передней кромки | |
EP2341216A3 (de) | Turbinenschaufel mit einer Verstärkung der Aufprallzone | |
ATE515436T1 (de) | Befestigung einer triebwerksgondelstruktur mittels einer verstärkten messerschneiden-rillen- kupplung | |
GB2464658A (en) | Wingtip feathers,including forward swept feathers,and associated aircraft systems and methods | |
BRPI0716353A2 (pt) | "conjuntos de pÁ propulsora e mÉtodos de montagem de um conjunto de pÁs propusoras" | |
RU2010134976A (ru) | Воздухозаборник для гондолы летательного аппарата и двигательная установка, содержащая данный воздухозаборник | |
WO2014099088A3 (en) | Environmental defense shield | |
WO2009024662A3 (fr) | Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur | |
RU2018114902A (ru) | Лопатка, содержащая сложенный экран передней кромки и способ изготовления лопатки | |
US10294958B2 (en) | Fan blade assembly | |
WO2010061071A3 (fr) | Nacelle integree sur aile volante | |
RU2013101809A (ru) | Система спрямления воздушного потока для гондолы двигателя летательного аппарата | |
RU2011123482A (ru) | Гондола турбореактивного двигателя | |
EP2365199A3 (de) | Aerodynamisch geformtes Stütz- und/oder Verkleidungselement im Nebenstromkanal eines Gasturbinentriebwerks | |
RU2007144088A (ru) | Летательный аппарат с низким уровнем шума, в частности, при взлете и посадке |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |