DE60207765D1 - Triebwerkaufhängungsvorrichtung an einem Luftfahrzeug - Google Patents
Triebwerkaufhängungsvorrichtung an einem LuftfahrzeugInfo
- Publication number
- DE60207765D1 DE60207765D1 DE60207765T DE60207765T DE60207765D1 DE 60207765 D1 DE60207765 D1 DE 60207765D1 DE 60207765 T DE60207765 T DE 60207765T DE 60207765 T DE60207765 T DE 60207765T DE 60207765 D1 DE60207765 D1 DE 60207765D1
- Authority
- DE
- Germany
- Prior art keywords
- fittings
- attachment structure
- engine
- nacelle stub
- 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 - Lifetime
Links
- 239000000725 suspension Substances 0.000 title 1
- 230000002950 deficient Effects 0.000 abstract 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
- 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
-
- 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
- B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Connection Of Plates (AREA)
- Agricultural Machines (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Vibration Prevention Devices (AREA)
- Vehicle Body Suspensions (AREA)
- Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0101701A FR2820402B1 (fr) | 2001-02-08 | 2001-02-08 | Dispositif d'accrochage d'un moteur sur un aeronef |
FR0101701 | 2001-02-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60207765D1 true DE60207765D1 (de) | 2006-01-12 |
DE60207765T2 DE60207765T2 (de) | 2006-09-07 |
Family
ID=8859767
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60207765T Expired - Lifetime DE60207765T2 (de) | 2001-02-08 | 2002-02-06 | Triebwerkaufhängungsvorrichtung an einem Luftfahrzeug |
Country Status (7)
Country | Link |
---|---|
US (1) | US6601796B2 (de) |
EP (1) | EP1231138B1 (de) |
AT (1) | ATE312017T1 (de) |
CA (1) | CA2369206C (de) |
DE (1) | DE60207765T2 (de) |
ES (1) | ES2254616T3 (de) |
FR (1) | FR2820402B1 (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2830516B1 (fr) * | 2001-10-04 | 2004-01-02 | Snecma Moteurs | Suspension de turboreacteur |
US6607165B1 (en) * | 2002-06-28 | 2003-08-19 | General Electric Company | Aircraft engine mount with single thrust link |
FR2855494B1 (fr) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | Dispositif d'accrocharge arriere de moteur d'avion |
US6843449B1 (en) * | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
FR2867155B1 (fr) | 2004-03-08 | 2007-06-29 | Snecma Moteurs | Suspension d'un moteur a la structure d'un avion |
FR2868041B1 (fr) * | 2004-03-25 | 2006-05-26 | Snecma Moteurs Sa | Suspension d'un moteur d'avion |
FR2873986B1 (fr) * | 2004-08-04 | 2007-12-21 | Airbus France Sas | Ensemble moteur pour aeronef |
FR2883839B1 (fr) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | Suspension arriere de turboreacteur |
GB0507721D0 (en) * | 2005-04-16 | 2005-05-25 | Rolls Royce Plc | Gas turbine engine mounting arrangement |
FR2887521B1 (fr) * | 2005-06-28 | 2007-08-17 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur |
FR2887853B1 (fr) * | 2005-06-29 | 2007-08-17 | Airbus France Sas | Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage |
US20070057128A1 (en) * | 2005-09-14 | 2007-03-15 | Honeywell International, Inc. | Auxiliary power unit case flange to plate adapter |
FR2891253B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Attache arriere d'un moteur d'aeronef a deux manilles |
FR2900906B1 (fr) * | 2006-05-09 | 2009-01-09 | Airbus France Sas | Systeme de fixation tolerant aux dommages pour moteur d'aeronef |
ATE430691T1 (de) * | 2006-10-24 | 2009-05-15 | Eads Constr Aeronauticas Sa | Luftbetankungssonde mit ausfallsicherem roll- und nickscharnier |
FR2915176B1 (fr) * | 2007-04-20 | 2009-07-10 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet |
FR2916424B1 (fr) * | 2007-05-23 | 2009-08-21 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant |
WO2008150202A1 (en) * | 2007-06-08 | 2008-12-11 | Volvo Aero Corporation | A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure |
US8950702B2 (en) * | 2008-01-18 | 2015-02-10 | United Technologies Corporation | Pylon and engine mount configuration |
US8047469B2 (en) * | 2008-03-01 | 2011-11-01 | The Boeing Company | Airframe attachment fitting |
GB0810589D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
US20130074517A1 (en) * | 2011-09-23 | 2013-03-28 | United Technologies Corporation | Gas turbine engine mount assembly |
CN103318415B (zh) * | 2012-03-21 | 2015-10-14 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种航空发动机安装维护用升降装置 |
US20140084129A1 (en) * | 2012-09-27 | 2014-03-27 | United Technologies Corporation | Assembly for mounting a turbine engine case to a pylon |
GB201315968D0 (en) * | 2013-09-09 | 2013-10-23 | Rolls Royce Plc | Aircraft engine mount |
FR3027873B1 (fr) * | 2014-11-03 | 2016-12-23 | Airbus Operations Sas | Attache moteur avant pour un moteur d'aeronef |
FR3096353B1 (fr) * | 2019-05-21 | 2022-02-11 | Airbus Operations Sas | Systeme d’attache moteur avant pour un moteur d’aeronef comportant une poutre realisee en deux parties |
CN113237403A (zh) * | 2021-03-26 | 2021-08-10 | 陕西飞机工业有限责任公司 | 发动机发房下盖支架检测装置及方法 |
FR3128205A1 (fr) * | 2021-10-14 | 2023-04-21 | Airbus Operations | Assemblage d’un mat avec un moteur d’un aéronef |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5275357A (en) | 1992-01-16 | 1994-01-04 | General Electric Company | Aircraft engine mount |
US5320307A (en) * | 1992-03-25 | 1994-06-14 | General Electric Company | Aircraft engine thrust mount |
US5351930A (en) * | 1992-08-11 | 1994-10-04 | Lord Corporation | Mounting for engines and the like |
US5620154A (en) | 1995-05-03 | 1997-04-15 | The Boeing Company | Three link failsafe engine mount |
US5725181A (en) * | 1996-05-01 | 1998-03-10 | The Boeing Company | Aircraft engine thrust mount |
FR2770486B1 (fr) * | 1997-11-06 | 2000-01-28 | Aerospatiale | Dispositif d'accrochage d'un moteur sur un aeronef |
FR2774358B1 (fr) * | 1998-02-04 | 2000-04-21 | Aerospatiale | Dispositif d'accrochage d'un moteur d'aeronef |
FR2793767B1 (fr) * | 1999-05-17 | 2001-09-21 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef |
FR2793769B1 (fr) * | 1999-05-19 | 2001-09-07 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef a un mat |
FR2806699B1 (fr) * | 2000-03-22 | 2002-05-10 | Aerospatiale Matra Airbus | Dispositif de reprise de poussee apte a relier un turbomoteur et un mat d'aeronef |
US6401448B1 (en) * | 2000-08-31 | 2002-06-11 | General Electric Company | System for mounting aircraft engines |
-
2001
- 2001-02-08 FR FR0101701A patent/FR2820402B1/fr not_active Expired - Lifetime
-
2002
- 2002-01-23 US US10/052,439 patent/US6601796B2/en not_active Expired - Lifetime
- 2002-01-23 CA CA2369206A patent/CA2369206C/en not_active Expired - Fee Related
- 2002-02-06 AT AT02290284T patent/ATE312017T1/de not_active IP Right Cessation
- 2002-02-06 ES ES02290284T patent/ES2254616T3/es not_active Expired - Lifetime
- 2002-02-06 EP EP02290284A patent/EP1231138B1/de not_active Expired - Lifetime
- 2002-02-06 DE DE60207765T patent/DE60207765T2/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
CA2369206A1 (en) | 2002-08-08 |
CA2369206C (en) | 2010-06-01 |
ES2254616T3 (es) | 2006-06-16 |
US6601796B2 (en) | 2003-08-05 |
EP1231138B1 (de) | 2005-12-07 |
US20020104924A1 (en) | 2002-08-08 |
DE60207765T2 (de) | 2006-09-07 |
EP1231138A1 (de) | 2002-08-14 |
FR2820402A1 (fr) | 2002-08-09 |
FR2820402B1 (fr) | 2003-05-02 |
ATE312017T1 (de) | 2005-12-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
R082 | Change of representative |
Ref document number: 1231138 Country of ref document: EP Representative=s name: HENKEL, BREUER & PARTNER, 80333 MUENCHEN, DE |