BRPI0401809A - Dispositivo de fixação dianteiro de motor de avião - Google Patents
Dispositivo de fixação dianteiro de motor de aviãoInfo
- Publication number
- BRPI0401809A BRPI0401809A BR0401809-5A BRPI0401809A BRPI0401809A BR PI0401809 A BRPI0401809 A BR PI0401809A BR PI0401809 A BRPI0401809 A BR PI0401809A BR PI0401809 A BRPI0401809 A BR PI0401809A
- Authority
- BR
- Brazil
- Prior art keywords
- hand
- fastening device
- aircraft engine
- engine front
- front fastening
- Prior art date
Links
- 238000010276 construction Methods 0.000 abstract 1
- 238000004519 manufacturing process Methods 0.000 abstract 1
- 239000000725 suspension Substances 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 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
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Transmission Devices (AREA)
- Vibration Prevention Devices (AREA)
- Connection Of Plates (AREA)
- Toys (AREA)
Abstract
"DISPOSITIVO DE FIXAçãO DIANTEIRO DE MOTOR DE AVIãO". A presente invenção tem como objetivo uma suspensão ou um dispositivo de fixação, em especial dianteiro, de um turbomotor (1) no montante de um avião que compreende uma virola superior (12, 12<39>) provida de meios de fixação no montante, uma primeira (16) e uma segunda (18) bielas ligadas cada uma delas com o motor por um lado por uma primeira ligação com articulação (161, 181; 161<39>, 181<39>) e com a virola (12, 12<39>) por outro lado por uma segunda ligação com articulação (165, 185; 165<39>, 185<39>). O dispositivo é caracterizado pelo fato de que cada biela (16, 18) compreende uma terceira ligação (167, 187; 167<39>, 187<39>) de reserva. A invenção permite a realização de elementos com a mesma forma. Assegura-se desse modo uma intercambiabilidade entre esses elementos e uma redução dos custos de produção e de gestão. Por outro lado são reduzidos os riscos de erro na montagem.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0306436A FR2855495B1 (fr) | 2003-05-27 | 2003-05-27 | Dispositif d'accrochage avant de moteur d'avion |
Publications (2)
Publication Number | Publication Date |
---|---|
BRPI0401809A true BRPI0401809A (pt) | 2005-01-18 |
BRPI0401809B1 BRPI0401809B1 (pt) | 2013-09-24 |
Family
ID=33104491
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0401809-5B1A BRPI0401809B1 (pt) | 2003-05-27 | 2004-05-24 | dispositivo de fixaÇço dianteiro de motor de aviço |
Country Status (10)
Country | Link |
---|---|
US (1) | US7165743B2 (pt) |
EP (1) | EP1481896B1 (pt) |
JP (1) | JP4272106B2 (pt) |
BR (1) | BRPI0401809B1 (pt) |
CA (1) | CA2469868C (pt) |
DE (1) | DE602004006463T2 (pt) |
ES (1) | ES2285378T3 (pt) |
FR (1) | FR2855495B1 (pt) |
RU (1) | RU2346855C2 (pt) |
UA (1) | UA85533C2 (pt) |
Families Citing this family (42)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2862612B1 (fr) * | 2003-11-25 | 2006-02-17 | Airbus France | Dispositif d'accrochage d'un moteur sous une voilure d'aeronef |
US20060032974A1 (en) * | 2004-08-16 | 2006-02-16 | Honeywell International Inc. | Modular installation kit for auxiliary power unit |
FR2883839B1 (fr) * | 2005-03-29 | 2007-06-29 | Snecma Moteurs Sa | Suspension arriere de turboreacteur |
FR2883940B1 (fr) * | 2005-03-31 | 2008-10-10 | Airbus France Sas | Bielle structurale creuse et procede de fabrication d'une telle bielle |
US20070057128A1 (en) * | 2005-09-14 | 2007-03-15 | Honeywell International, Inc. | Auxiliary power unit case flange to plate adapter |
FR2891243B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2891253B1 (fr) * | 2005-09-28 | 2007-10-26 | Airbus France Sas | Attache arriere d'un moteur d'aeronef a deux manilles |
GB0603539D0 (en) * | 2006-02-22 | 2006-04-05 | Airbus Uk Ltd | Control surface failsafe drop link |
GB2443554A (en) * | 2006-11-06 | 2008-05-07 | Goodrich Corp | Aircraft cargo monitoring system |
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 |
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. |
FR2924094B1 (fr) * | 2007-11-23 | 2010-01-15 | Snecma | Turboreacteur suspendu a un pylone d'aeronef |
US8950702B2 (en) * | 2008-01-18 | 2015-02-10 | United Technologies Corporation | Pylon and engine mount configuration |
FR2926536B1 (fr) * | 2008-01-23 | 2010-07-30 | Snecma | Accrochage d'un systeme propulsif a un element de structure d'un aeronef |
US8672260B2 (en) * | 2009-12-02 | 2014-03-18 | United Technologies Corporation | Single plane mount system for gas turbine engine |
KR101767071B1 (ko) * | 2010-06-14 | 2017-08-10 | 로오드 코포레이션 | 헬리콥터 엔진 장착 시스템 및 방법 |
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 |
ES2398861B1 (es) * | 2010-10-08 | 2014-04-29 | Airbus Operations, S.L. | Concepto de unión intercambiable para un cono de un fuselaje trasero de un avión. |
FR2973339B1 (fr) * | 2011-03-29 | 2014-08-22 | Snecma | Dispositif de suspension d'une turbomachine a un avion |
FR2974065B1 (fr) * | 2011-04-14 | 2013-05-10 | Snecma | Procede de montage d'un moteur d'aeronef sur un pylone et attache moteur pour la mise en oeuvre d'un tel procede. |
US20130074517A1 (en) * | 2011-09-23 | 2013-03-28 | United Technologies Corporation | Gas turbine engine mount assembly |
US9016623B2 (en) * | 2011-11-30 | 2015-04-28 | The Boeing Company | Jam protection and alleviation for control surface linkage mechanisms |
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 |
FR2997142B1 (fr) * | 2012-10-18 | 2014-12-05 | Epsilon Composite | Procede de realisation d'un embout goupille d'une piece longitudinale, embout ainsi obtenu |
FR3000467A1 (fr) * | 2012-12-28 | 2014-07-04 | Airbus Operations Sas | Manille a trois points a capacite de filtrage de vibrations et attache moteur d'aeronef equipee d'une telle manille |
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 |
US10144524B2 (en) * | 2013-06-14 | 2018-12-04 | Rohr, Inc. | Assembly for mounting a turbine engine to a pylon |
CN105392700B (zh) | 2013-07-26 | 2018-12-18 | Mra系统有限责任公司 | 飞行器发动机吊架 |
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 |
FR3041935B1 (fr) * | 2015-10-05 | 2017-12-15 | Airbus Operations Sas | Ensemble moteur pour aeronef comprenant au moins deux attaches moteur arriere decalees axialement l'une de l'autre |
FR3059645B1 (fr) * | 2016-12-02 | 2018-12-07 | Safran Aircraft Engines | Dispositif de suspension pour turbomachine |
CN107521706A (zh) * | 2017-07-28 | 2017-12-29 | 中国航空工业集团公司西安飞机设计研究所 | 发动机辅助安装接头 |
DE102017129060A1 (de) * | 2017-12-06 | 2019-06-06 | Rolls-Royce Deutschland Ltd & Co Kg | Integrierte Tragstruktur für ein Flugzeugtriebwerk und dessen Zubehörkomponenten |
FR3081836B1 (fr) * | 2018-06-01 | 2020-11-06 | Airbus Operations Sas | Ensemble propulsif d'aeronef et procede de verification de l'integrite d'une attache moteur de l'ensemble propulsif |
FR3086924B1 (fr) * | 2018-10-08 | 2021-02-12 | Safran Aircraft Engines | Turbomachine comportant des moyens de suspension |
US11479104B2 (en) | 2019-07-24 | 2022-10-25 | Honeywell International Inc. | System and method for gas turbine engine mount with seal |
FR3102976B1 (fr) * | 2019-11-13 | 2023-11-24 | Safran Aircraft Engines | Avion à suspension instrumentée |
US11821253B2 (en) * | 2020-11-12 | 2023-11-21 | The Boeing Company | Aircraft door common stop fitting |
CN117020611B (zh) * | 2023-09-01 | 2024-03-19 | 昆山帕捷汽车零部件有限公司 | 一种发动机连接杆上螺栓和卡环的预锁紧的装配机 |
Family Cites Families (10)
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 |
US5303880A (en) * | 1992-10-28 | 1994-04-19 | General Electric Company | Aircraft engine pin mount |
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 |
US5860623A (en) * | 1995-05-03 | 1999-01-19 | The Boeing Company | Three link failsafe engine mount |
US6189830B1 (en) * | 1999-02-26 | 2001-02-20 | The Boeing Company | Tuned engine mounting system for jet aircraft |
US6330995B1 (en) * | 2000-02-29 | 2001-12-18 | General Electric Company | Aircraft engine mount |
FR2828167B1 (fr) * | 2001-07-31 | 2003-11-21 | Airbus France | Dispositif d'accrochage d'un moteur sur un aeronef |
-
2003
- 2003-05-27 FR FR0306436A patent/FR2855495B1/fr not_active Expired - Fee Related
-
2004
- 2004-05-12 US US10/843,306 patent/US7165743B2/en not_active Expired - Lifetime
- 2004-05-13 JP JP2004143229A patent/JP4272106B2/ja not_active Expired - Lifetime
- 2004-05-17 DE DE602004006463T patent/DE602004006463T2/de not_active Expired - Lifetime
- 2004-05-17 ES ES04291253T patent/ES2285378T3/es not_active Expired - Lifetime
- 2004-05-17 EP EP04291253A patent/EP1481896B1/fr not_active Expired - Lifetime
- 2004-05-24 BR BRPI0401809-5B1A patent/BRPI0401809B1/pt active IP Right Grant
- 2004-05-25 CA CA2469868A patent/CA2469868C/fr not_active Expired - Lifetime
- 2004-05-26 UA UA20040504029A patent/UA85533C2/ru unknown
- 2004-05-26 RU RU2004116113/11A patent/RU2346855C2/ru active
Also Published As
Publication number | Publication date |
---|---|
CA2469868A1 (fr) | 2004-11-27 |
EP1481896A1 (fr) | 2004-12-01 |
CA2469868C (fr) | 2012-10-02 |
DE602004006463D1 (de) | 2007-06-28 |
JP4272106B2 (ja) | 2009-06-03 |
JP2004352233A (ja) | 2004-12-16 |
US7165743B2 (en) | 2007-01-23 |
UA85533C2 (ru) | 2009-02-10 |
US20040251381A1 (en) | 2004-12-16 |
EP1481896B1 (fr) | 2007-05-16 |
RU2004116113A (ru) | 2005-11-10 |
RU2346855C2 (ru) | 2009-02-20 |
BRPI0401809B1 (pt) | 2013-09-24 |
DE602004006463T2 (de) | 2008-01-17 |
FR2855495B1 (fr) | 2006-11-24 |
FR2855495A1 (fr) | 2004-12-03 |
ES2285378T3 (es) | 2007-11-16 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0401809A (pt) | Dispositivo de fixação dianteiro de motor de avião | |
BRPI0401808A (pt) | Dispositivo de fixação de um turbomotor no montante de um avião | |
ES2378702B1 (es) | Herrajes para la cogida del estabilizador vertical de cola de una aeronave. | |
DE602006010069D1 (de) | Motoraufhängung für ein flugzeug zur platzierung zwischen einem motor und einer motoraufhängungsstruktur | |
BRPI0418220A (pt) | conjunto de montagem de componente respiratório | |
BRPI0402464A (pt) | Suspensão de turbomotor a um montante de avião | |
FR2936489B1 (fr) | Troncon central d'aeronef avec carenage ventral travaillant | |
FR2902406B1 (fr) | Carenage pour mat de suspension d'un turbomoteur a une aile d'aeronef | |
BRPI0712175A2 (pt) | piso pressurizado de aeronave | |
ATE392361T1 (de) | Seitenleitwerkeinheit für flugzeug und damit versehenes flugzeug | |
US2355053A (en) | Ophthalmic mounting | |
RU2011115027A (ru) | Хвостовая часть самолета, содержащая конструкцию для поддержки двигателей, которая проходит через фюзеляж и соединена с ним по меньшей мере одной соединительной тягой | |
ATE341484T1 (de) | Aufhängevorrichtung eines flugzeugtriebwerks an einem flügelpylon | |
DE60303507D1 (de) | Aufhängung eines triebwerks unter einer flugzeugtragfläche | |
BRPI0618235A2 (pt) | suspensão de braço de arraste | |
RU2012107090A (ru) | Балка подвески турбинного двигателя к конструкции летательного аппарата | |
BRPI0709090A2 (pt) | arranjo de asa de aeronave, e, aeronave | |
RU2008149985A (ru) | Промежуточный корпус для реактивного двигателя летательного аппарата, усовершенствованной конструкции | |
RU2010139660A (ru) | Силовая установка летательного аппарата, содержащая турбоактивный двигатель с усиливающими конструкциями, соединяющими корпус вентилятора с центральным корпусом | |
BRPI0913722B1 (pt) | Dobradiça para o capô do compartimento motor de um veículo automotivo e veículo automotivo incluindo a referida dobradiça de capô | |
BR112014004578A2 (pt) | conjunto formado por um turbomotor e seu sistema de fixação a uma estrutura de aeronave | |
CN204554715U (zh) | 一种灯体与灯杆的连接结构 | |
RU120223U1 (ru) | Универсальный силовой узел для установки полумодели в аэродинамической трубе | |
CN105818986A (zh) | 挂件架、悬挂系统及无人直升机 | |
CN205602141U (zh) | 挂件架、悬挂系统及无人直升机 |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25D | Requested change of name of applicant approved |
Owner name: SNECMA (FR) Free format text: ALTERADO DE: SNECMA MOTEURS |
|
B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 24/05/2004, OBSERVADAS AS CONDICOES LEGAIS. |