ATE346792T1 - Triebwerkaufhängungsvorrichtung an einem luftfahrzeug - Google Patents
Triebwerkaufhängungsvorrichtung an einem luftfahrzeugInfo
- Publication number
- ATE346792T1 ATE346792T1 AT02291911T AT02291911T ATE346792T1 AT E346792 T1 ATE346792 T1 AT E346792T1 AT 02291911 T AT02291911 T AT 02291911T AT 02291911 T AT02291911 T AT 02291911T AT E346792 T1 ATE346792 T1 AT E346792T1
- Authority
- AT
- Austria
- Prior art keywords
- aircraft
- links
- mounting device
- engine mounting
- pylon
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pivots And Pivotal Connections (AREA)
- Vehicle Body Suspensions (AREA)
- Connection Of Plates (AREA)
- Load-Engaging Elements For Cranes (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Jib Cranes (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR0110261A FR2828167B1 (fr) | 2001-07-31 | 2001-07-31 | Dispositif d'accrochage d'un moteur sur un aeronef |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE346792T1 true ATE346792T1 (de) | 2006-12-15 |
Family
ID=8866134
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT02291911T ATE346792T1 (de) | 2001-07-31 | 2002-07-29 | Triebwerkaufhängungsvorrichtung an einem luftfahrzeug |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US6682015B2 (de) |
| EP (1) | EP1281615B1 (de) |
| AT (1) | ATE346792T1 (de) |
| CA (1) | CA2394462C (de) |
| DE (1) | DE60216375T2 (de) |
| ES (1) | ES2277993T3 (de) |
| FR (1) | FR2828167B1 (de) |
Families Citing this family (52)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2818614B1 (fr) * | 2000-12-21 | 2003-01-31 | Snecma Moteurs | Piece de suspension d'un turboreacteur |
| FR2830516B1 (fr) * | 2001-10-04 | 2004-01-02 | Snecma Moteurs | Suspension de turboreacteur |
| FR2855495B1 (fr) * | 2003-05-27 | 2006-11-24 | Snecma Moteurs | Dispositif d'accrochage avant de moteur d'avion |
| FR2855494B1 (fr) * | 2003-05-27 | 2006-09-22 | Snecma Moteurs | Dispositif d'accrocharge arriere de moteur d'avion |
| FR2862612B1 (fr) * | 2003-11-25 | 2006-02-17 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
| FR2862611B1 (fr) * | 2003-11-25 | 2007-03-09 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
| US6843449B1 (en) * | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
| FR2869874B1 (fr) * | 2004-05-04 | 2006-06-23 | Snecma Moteurs Sa | Moteur d'avion avec des moyens de suspension a la structure d'un avion |
| GB0414043D0 (en) * | 2004-06-23 | 2004-07-28 | Rolls Royce Plc | Securing arrangement |
| FR2883839B1 (fr) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | Suspension arriere de turboreacteur |
| 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 |
| FR2891245B1 (fr) * | 2005-09-26 | 2007-10-26 | Airbus France Sas | Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur |
| FR2891253B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Attache arriere d'un moteur d'aeronef a deux manilles |
| FR2891249B1 (fr) * | 2005-09-28 | 2009-05-01 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
| GB0608983D0 (en) * | 2006-05-06 | 2006-06-14 | Rolls Royce Plc | Aeroengine mount |
| FR2900906B1 (fr) * | 2006-05-09 | 2009-01-09 | Airbus France Sas | Systeme de fixation tolerant aux dommages pour moteur d'aeronef |
| 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 |
| 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 |
| FR2917712B1 (fr) * | 2007-06-20 | 2009-09-25 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere formant palonnier. |
| 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. |
| 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 |
| GB2459483B (en) * | 2008-04-24 | 2010-06-30 | Rolls Royce Plc | Engine mounting arrangement |
| FR2931800B1 (fr) * | 2008-05-29 | 2010-07-30 | Airbus France | Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees |
| GB0810585D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
| GB0810589D0 (en) * | 2008-06-11 | 2008-07-16 | Rolls Royce Plc | Engine mounting arrangement |
| US8721185B2 (en) * | 2010-10-28 | 2014-05-13 | Joao Carlos Marchesan | Constructive arrangement added to a support for assembling agricultural tilting bearings |
| FR2969578B1 (fr) * | 2010-12-27 | 2013-02-08 | Snecma | Dispositif de suspension d'un turboreacteur |
| EP2587003A1 (de) * | 2011-10-25 | 2013-05-01 | Siemens Aktiengesellschaft | Gasturbinenmotor mit Stützstrebenanordnung |
| FR2989952B1 (fr) * | 2012-04-27 | 2014-04-18 | Aircelle Sa | Nacelle de turboreacteur a section aval |
| US10436063B2 (en) * | 2012-08-17 | 2019-10-08 | United Technologies Corporation | Assembly for mounting a turbine engine to an airframe |
| FR3000529B1 (fr) * | 2012-12-28 | 2015-03-06 | Airbus Operations Sas | Dispositif de liaison souple pour ensemble propulsif d'aeronef |
| JP6137846B2 (ja) * | 2013-01-25 | 2017-05-31 | 三菱航空機株式会社 | パイロンと翼を連結するリンク部材、航空機のパイロンおよび航空機 |
| CN103101628B (zh) * | 2013-02-06 | 2015-05-27 | 中国商用飞机有限责任公司 | 一种与飞机吊挂一体化的前安装节 |
| US8979020B2 (en) * | 2013-06-07 | 2015-03-17 | Pratt & Whitney Canada Corp. | Mounting system for mounting engine nacelle components and associated method |
| GB201315968D0 (en) | 2013-09-09 | 2013-10-23 | Rolls Royce Plc | Aircraft engine mount |
| FR3016608B1 (fr) * | 2014-01-21 | 2016-02-26 | Airbus Operations Sas | Attache moteur pour aeronef. |
| US10351224B2 (en) * | 2015-09-23 | 2019-07-16 | The Boeing Company | External structure mounting system for use with an aircraft |
| CN106314807B (zh) * | 2016-08-23 | 2018-08-21 | 西北工业大学 | 一种吸气式超燃冲压发动机的推力架结构 |
| RU178347U1 (ru) * | 2017-07-21 | 2018-03-30 | федеральное государственное бюджетное образовательное учреждение высшего образования "Санкт-Петербургский государственный морской технический университет" | Кронштейн турбокомпрессора судового дизеля |
| FR3073204A1 (fr) * | 2017-11-08 | 2019-05-10 | Airbus Operations | Systeme d'attache moteur d'un moteur d'aeronef |
| FR3073823B1 (fr) * | 2017-11-21 | 2019-11-08 | Airbus Operations | Attache moteur arriere pour un moteur d'aeronef |
| DE102017129060A1 (de) * | 2017-12-06 | 2019-06-06 | Rolls-Royce Deutschland Ltd & Co Kg | Integrierte Tragstruktur für ein Flugzeugtriebwerk und dessen Zubehörkomponenten |
| US10512206B2 (en) | 2017-12-11 | 2019-12-24 | Marchesan Implementos E Maquinas Agricolas Tatu S.A. | Agricultural tilting bearing assembly and improved support bracket for connecting the same to agricultural equipment |
| USD880279S1 (en) * | 2017-12-11 | 2020-04-07 | Marchesan Implementos E Maquinas Agricolas Tatu S.A. | Support bracket |
| FR3096344A1 (fr) | 2019-05-21 | 2020-11-27 | Airbus Operations | Systeme d’attache moteur avant pour un moteur d’aeronef comportant une fixation directe entre le mat reacteur et le moteur |
| FR3096348B1 (fr) * | 2019-05-21 | 2021-10-15 | Airbus Operations Sas | Systeme d’attache moteur avant pour un moteur d’aeronef comportant des systemes de bielles a deux bielles |
| FR3106126B1 (fr) * | 2020-01-10 | 2022-01-07 | Safran Aircraft Engines | Assemblage entre un pylône d’aéronef et une turbomachine |
| US11697506B2 (en) | 2020-05-15 | 2023-07-11 | General Electric Company | Methods and apparatus for gas turbine bending isolation |
| FR3123050A1 (fr) * | 2021-05-20 | 2022-11-25 | Airbus Sas | Système de réservoir comportant un châssis, un réservoir de dihydrogène et des moyens de fixation du réservoir au châssis |
| US20240124147A1 (en) * | 2022-10-13 | 2024-04-18 | General Electric Company | Gas turbine engine mount |
| FR3150505A1 (fr) * | 2023-06-28 | 2025-01-03 | Airbus Operations | Système d’attache moteur avant pour un moteur d’aéronef qui comporte une structure compacte |
| EP4491518B1 (de) * | 2023-07-10 | 2026-02-25 | Airbus Operations (S.A.S.) | Flugzeugtriebwerkanordnung mit einer hauptstange zur motorbefestigung, sowie zwei parallel an einer querverstärkung vor einer primärstruktur eines masts |
Family Cites Families (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2635751B1 (fr) * | 1988-09-01 | 1991-01-04 | Snecma | Dispositif de fixation d'une biellette de suspension d'un turboreacteur |
| GB9125011D0 (en) * | 1991-11-25 | 1992-01-22 | Rolls Royce Plc | A mounting arrangement for a gas turbine engine |
| US5275357A (en) | 1992-01-16 | 1994-01-04 | General Electric Company | Aircraft engine mount |
| US5277382A (en) * | 1992-10-13 | 1994-01-11 | General Electric Company | Aircraft engine forward mount |
| FR2698068B1 (fr) * | 1992-11-16 | 1995-02-03 | Airbus Ind | Avion et autre aéronef à moteur pourvu d'ailes. |
| US5649417A (en) * | 1995-03-24 | 1997-07-22 | The Boeing Company | Fail-safe engine mount system |
| US5620154A (en) | 1995-05-03 | 1997-04-15 | The Boeing Company | Three link failsafe engine mount |
| US5927644A (en) * | 1997-10-08 | 1999-07-27 | General Electric Company | Double failsafe engine mount |
| FR2775465B1 (fr) * | 1998-03-02 | 2000-05-26 | Aerospatiale | Dispositif d'accrochage d'un moteur sur un pylone d'aeronef |
| US6189830B1 (en) * | 1999-02-26 | 2001-02-20 | The Boeing Company | Tuned engine mounting system for jet aircraft |
| FR2793769B1 (fr) * | 1999-05-19 | 2001-09-07 | Aerospatiale Airbus | Dispositif d'accrochage d'un moteur d'aeronef a un mat |
| US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
| 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 |
-
2001
- 2001-07-31 FR FR0110261A patent/FR2828167B1/fr not_active Expired - Fee Related
-
2002
- 2002-07-19 CA CA2394462A patent/CA2394462C/en not_active Expired - Fee Related
- 2002-07-29 ES ES02291911T patent/ES2277993T3/es not_active Expired - Lifetime
- 2002-07-29 US US10/208,884 patent/US6682015B2/en not_active Expired - Lifetime
- 2002-07-29 DE DE60216375T patent/DE60216375T2/de not_active Expired - Lifetime
- 2002-07-29 EP EP02291911A patent/EP1281615B1/de not_active Expired - Lifetime
- 2002-07-29 AT AT02291911T patent/ATE346792T1/de not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| US20030025033A1 (en) | 2003-02-06 |
| US6682015B2 (en) | 2004-01-27 |
| DE60216375D1 (de) | 2007-01-11 |
| EP1281615A1 (de) | 2003-02-05 |
| FR2828167B1 (fr) | 2003-11-21 |
| FR2828167A1 (fr) | 2003-02-07 |
| DE60216375T2 (de) | 2007-09-20 |
| ES2277993T3 (es) | 2007-08-01 |
| EP1281615B1 (de) | 2006-11-29 |
| CA2394462A1 (en) | 2003-01-31 |
| CA2394462C (en) | 2010-06-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |