DE602004000283D1 - Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform - Google Patents
Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit BumerangformInfo
- Publication number
- DE602004000283D1 DE602004000283D1 DE602004000283T DE602004000283T DE602004000283D1 DE 602004000283 D1 DE602004000283 D1 DE 602004000283D1 DE 602004000283 T DE602004000283 T DE 602004000283T DE 602004000283 T DE602004000283 T DE 602004000283T DE 602004000283 D1 DE602004000283 D1 DE 602004000283D1
- Authority
- DE
- Germany
- Prior art keywords
- lever
- connecting rods
- rear suspension
- aircraft engine
- boomerang shape
- 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 - Fee Related
Links
- 239000000725 suspension Substances 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
- 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
-
- 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
- B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Pivots And Pivotal Connections (AREA)
- Transmission Devices (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Clamps And Clips (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0307893 | 2003-06-30 | ||
FR0307893A FR2856656B1 (fr) | 2003-06-30 | 2003-06-30 | Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang |
Publications (2)
Publication Number | Publication Date |
---|---|
DE602004000283D1 true DE602004000283D1 (de) | 2006-02-02 |
DE602004000283T2 DE602004000283T2 (de) | 2006-08-31 |
Family
ID=33427637
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE602004000283T Expired - Fee Related DE602004000283T2 (de) | 2003-06-30 | 2004-06-25 | Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform |
Country Status (9)
Country | Link |
---|---|
US (1) | US7021585B2 (de) |
EP (1) | EP1493663B1 (de) |
JP (1) | JP2005022641A (de) |
BR (1) | BRPI0402464A (de) |
CA (1) | CA2472312A1 (de) |
DE (1) | DE602004000283T2 (de) |
ES (1) | ES2253728T3 (de) |
FR (1) | FR2856656B1 (de) |
RU (1) | RU2004119904A (de) |
Families Citing this family (66)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2868041B1 (fr) * | 2004-03-25 | 2006-05-26 | Snecma Moteurs Sa | Suspension d'un moteur d'avion |
FR2883839B1 (fr) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | Suspension arriere de turboreacteur |
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 |
FR2891804B1 (fr) * | 2005-10-12 | 2009-05-01 | Airbus France Sas | Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme |
FR2892706B1 (fr) * | 2005-10-31 | 2009-04-24 | Airbus France Sas | Dispositif d'attache avant d'un turboreacteur a un mat de fixation d'un aeronef |
FR2900906B1 (fr) * | 2006-05-09 | 2009-01-09 | Airbus France Sas | Systeme de fixation tolerant aux dommages pour moteur d'aeronef |
FR2903382B1 (fr) * | 2006-07-10 | 2008-10-10 | Airbus France Sas | Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal |
FR2914907B1 (fr) * | 2007-04-16 | 2009-10-30 | Snecma Sa | Suspension souple avec peigne pour turbomoteur |
FR2915175B1 (fr) * | 2007-04-20 | 2009-07-17 | Airbus France Sa | Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson |
FR2917713B1 (fr) * | 2007-06-21 | 2009-09-25 | Airbus France Sas | Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif. |
FR2918644B1 (fr) * | 2007-07-09 | 2009-10-23 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef disposant d'un palonnier articule en quatre points. |
US11486311B2 (en) | 2007-08-01 | 2022-11-01 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US8256707B2 (en) * | 2007-08-01 | 2012-09-04 | United Technologies Corporation | Engine mounting configuration for a turbofan gas turbine engine |
US8844265B2 (en) | 2007-08-01 | 2014-09-30 | United Technologies Corporation | Turbine section of high bypass turbofan |
US20150377123A1 (en) | 2007-08-01 | 2015-12-31 | United Technologies Corporation | Turbine section of high bypass turbofan |
US11242805B2 (en) | 2007-08-01 | 2022-02-08 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11346289B2 (en) | 2007-08-01 | 2022-05-31 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
US11149650B2 (en) | 2007-08-01 | 2021-10-19 | Raytheon Technologies Corporation | Turbine section of high bypass turbofan |
FR2920138B1 (fr) * | 2007-08-24 | 2010-03-12 | Airbus France | Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit |
FR2924094B1 (fr) * | 2007-11-23 | 2010-01-15 | Snecma | Turboreacteur suspendu a un pylone d'aeronef |
FR2924684B1 (fr) * | 2007-12-07 | 2010-01-01 | Snecma | Suspension d'un turboreacteur a un aeronef |
FR2925016B1 (fr) * | 2007-12-12 | 2010-06-18 | Snecma | Suspension d'un turboreacteur a un aeronef |
US8118251B2 (en) * | 2008-01-18 | 2012-02-21 | United Technologies Corporation | Mounting system for a gas turbine engine |
FR2926536B1 (fr) * | 2008-01-23 | 2010-07-30 | Snecma | Accrochage d'un systeme propulsif a un element de structure d'un aeronef |
US8826641B2 (en) * | 2008-01-28 | 2014-09-09 | United Technologies Corporation | Thermal management system integrated pylon |
US9234481B2 (en) * | 2008-01-25 | 2016-01-12 | United Technologies Corporation | Shared flow thermal management system |
US8167237B2 (en) * | 2008-03-21 | 2012-05-01 | United Technologies Corporation | Mounting system for a gas turbine engine |
DE102008021431A1 (de) * | 2008-04-29 | 2009-11-12 | Airbus Deutschland Gmbh | Flugzeug mit einer Energie-Versorgungsvorrichtung |
US8128021B2 (en) * | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
US8695920B2 (en) | 2008-06-02 | 2014-04-15 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8807477B2 (en) | 2008-06-02 | 2014-08-19 | United Technologies Corporation | Gas turbine engine compressor arrangement |
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8511605B2 (en) | 2008-06-02 | 2013-08-20 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8800914B2 (en) | 2008-06-02 | 2014-08-12 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
GB0810589D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
GB0810585D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
GB0810791D0 (en) * | 2008-06-13 | 2008-07-23 | Rolls Royce Plc | Thrust mounting arrangement |
GB0902909D0 (en) * | 2009-02-23 | 2009-04-08 | Rolls Royce Plc | A thrust mount arrangement for an aircraft engine |
FR2952150B1 (fr) * | 2009-11-02 | 2012-02-24 | Airbus Operations Sas | Bielle structurale comportant un mode filtrant des vibrations |
FR2959210B1 (fr) * | 2010-04-21 | 2013-08-23 | Snecma | Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee |
EP3184433B1 (de) * | 2010-06-14 | 2018-07-25 | LORD Corporation | System und verfahren zur montage eines hubschraubermotors |
FR2965549B1 (fr) * | 2010-10-01 | 2013-07-05 | Airbus Operations Sas | Dispositif de reprise de poussee a bielles pour mat d'accrochage d'un moteur d'aeronef, integrant trois rotules alignees |
FR2965796B1 (fr) * | 2010-10-07 | 2013-06-07 | Snecma | Suspension d'un moteur a un mat d'aeronef comportant un arceau de suspension |
US20130074517A1 (en) * | 2011-09-23 | 2013-03-28 | United Technologies Corporation | Gas turbine engine mount assembly |
FR2981047B1 (fr) * | 2011-10-06 | 2013-10-25 | Aircelle Sa | Ensemble propulsif d'aeronef |
US9016623B2 (en) * | 2011-11-30 | 2015-04-28 | The Boeing Company | Jam protection and alleviation for control surface linkage mechanisms |
US20140084129A1 (en) * | 2012-09-27 | 2014-03-27 | United Technologies Corporation | Assembly for mounting a turbine engine case to a pylon |
US8979020B2 (en) * | 2013-06-07 | 2015-03-17 | Pratt & Whitney Canada Corp. | Mounting system for mounting engine nacelle components and associated method |
WO2015010315A1 (en) | 2013-07-26 | 2015-01-29 | Mra Systems, Inc. | Aircraft engine pylon |
WO2015088619A2 (en) | 2013-10-16 | 2015-06-18 | United Technologies Corporation | Geared turbofan engine with targeted modular efficiency |
CN103587709B (zh) * | 2013-10-30 | 2016-06-01 | 中国运载火箭技术研究院 | 一种用于直升机挂载飞行器的挂架系统 |
GB201417202D0 (en) * | 2014-09-30 | 2014-11-12 | Rolls Royce Plc | Gas Turbine Engine Mounting Arrangement |
FR3032180B1 (fr) * | 2015-01-30 | 2018-05-18 | Airbus Operations | Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure |
FR3041996B1 (fr) | 2015-10-05 | 2017-10-27 | Snecma | Systeme de suspension de deux modules d'un ensemble propulsif |
CN109562841B (zh) | 2016-08-08 | 2022-03-18 | 洛德公司 | 用于飞机发动机的安装系统、装置和方法 |
FR3058986B1 (fr) * | 2016-11-21 | 2021-04-16 | Airbus Operations Sas | Attache arriere d'un moteur d'aeronef comportant des temoins de rupture |
FR3060069B1 (fr) * | 2016-12-13 | 2019-05-24 | Airbus Operations Sas | Bielle amortissante convertible en bielle rigide |
FR3086924B1 (fr) * | 2018-10-08 | 2021-02-12 | Safran Aircraft Engines | Turbomachine comportant des moyens de suspension |
EP3663206B1 (de) * | 2018-12-06 | 2023-09-06 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Befestigung zum aufhängen eines flugzeugtriebwerks |
US11970279B2 (en) | 2020-02-21 | 2024-04-30 | General Electric Company | Control system and methods of controlling an engine-mounting link system |
US11939070B2 (en) | 2020-02-21 | 2024-03-26 | General Electric Company | Engine-mounting links that have an adjustable inclination angle |
US11970278B2 (en) | 2020-07-14 | 2024-04-30 | General Electric Company | Thrust mounts with load-balancing thrust link-lever |
FR3114300A1 (fr) * | 2020-09-21 | 2022-03-25 | Airbus Operations (S.A.S.) | Assemblage d’un moteur avec un mat d’aeronef |
FR3123323B1 (fr) * | 2021-05-27 | 2024-05-03 | Safran Aircraft Engines | Structure de liaison et de support d’une turbomachine a un pylone d’aeronef |
FR3127202A1 (fr) * | 2021-09-20 | 2023-03-24 | Airbus Operations (S.A.S.) | Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5320307A (en) * | 1992-03-25 | 1994-06-14 | General Electric Company | Aircraft engine thrust mount |
US5725181A (en) * | 1996-05-01 | 1998-03-10 | The Boeing Company | Aircraft engine thrust mount |
US5873547A (en) * | 1997-05-20 | 1999-02-23 | 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 |
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 |
FR2830516B1 (fr) * | 2001-10-04 | 2004-01-02 | Snecma Moteurs | Suspension de turboreacteur |
FR2830515B1 (fr) * | 2001-10-04 | 2004-01-30 | Snecma Moteurs | Suspension de turboreacteur |
-
2003
- 2003-06-30 FR FR0307893A patent/FR2856656B1/fr not_active Expired - Fee Related
-
2004
- 2004-06-23 CA CA002472312A patent/CA2472312A1/fr not_active Abandoned
- 2004-06-24 US US10/874,349 patent/US7021585B2/en not_active Expired - Lifetime
- 2004-06-24 JP JP2004186205A patent/JP2005022641A/ja not_active Withdrawn
- 2004-06-25 ES ES04291603T patent/ES2253728T3/es not_active Expired - Lifetime
- 2004-06-25 EP EP04291603A patent/EP1493663B1/de not_active Expired - Lifetime
- 2004-06-25 DE DE602004000283T patent/DE602004000283T2/de not_active Expired - Fee Related
- 2004-06-29 RU RU2004119904/11A patent/RU2004119904A/ru not_active Application Discontinuation
- 2004-06-29 BR BR0402464-8A patent/BRPI0402464A/pt not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP1493663A1 (de) | 2005-01-05 |
CA2472312A1 (fr) | 2004-12-30 |
FR2856656A1 (fr) | 2004-12-31 |
JP2005022641A (ja) | 2005-01-27 |
RU2004119904A (ru) | 2005-12-10 |
BRPI0402464A (pt) | 2005-05-24 |
FR2856656B1 (fr) | 2006-12-01 |
US7021585B2 (en) | 2006-04-04 |
ES2253728T3 (es) | 2006-06-01 |
DE602004000283T2 (de) | 2006-08-31 |
US20050067528A1 (en) | 2005-03-31 |
EP1493663B1 (de) | 2005-12-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |