BRPI0401808A - Dispositivo de fixação de um turbomotor no montante de um avião - Google Patents
Dispositivo de fixação de um turbomotor no montante de um aviãoInfo
- Publication number
- BRPI0401808A BRPI0401808A BR0401808-7A BRPI0401808A BRPI0401808A BR PI0401808 A BRPI0401808 A BR PI0401808A BR PI0401808 A BRPI0401808 A BR PI0401808A BR PI0401808 A BRPI0401808 A BR PI0401808A
- Authority
- BR
- Brazil
- Prior art keywords
- small connecting
- connecting rods
- turbomotor
- suspension
- engine
- Prior art date
Links
- 239000000725 suspension Substances 0.000 abstract 2
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)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Supercharger (AREA)
- Clamps And Clips (AREA)
- Axle Suspensions And Sidecars For Cycles (AREA)
Abstract
"DISPOSITIVO DE FIXAçãO DE UM TURBOMOTOR NO MONTANTE DE UM AVIãO". A presente invenção tem como objetivo uma suspensão ou um dispositivo de fixação traseiro de um turbomotor (1) no montante de um avião que compreende uma virola superior (12) provida de meios de fixação no montante, na qual são articuladas, por segundas ligações (163, 183) com articulação, três pequenas bielas dispostas transversalmente ao eixo longitudinal do motor, uma primeira (16) e uma segunda (18) pequenas bielas de um lado e de outro do eixo do motor e uma terceira pequena biela (17) entre elas duas, as pequenas bielas sendo elas próprias ligadas ao motor por primeiras ligações (161, 181) com articulações. A suspensão é caracterizada pelo fato de que as primeira (16) e segunda (18) pequenas bielas compreendem cada uma delas uma terceira (167, 187) ligação de reserva e que a virola superior (12) é formada por uma viga (120) fixada rigidamente ao montante. A solução da invenção permite a realização de pequenas bielas idênticas e assegurar a intercambiabilidade das mesmas reduzindo assim os riscos de erro na montagem.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0306435A FR2855494B1 (fr) | 2003-05-27 | 2003-05-27 | Dispositif d'accrocharge arriere de moteur d'avion |
Publications (2)
Publication Number | Publication Date |
---|---|
BRPI0401808A true BRPI0401808A (pt) | 2005-01-18 |
BRPI0401808B1 BRPI0401808B1 (pt) | 2013-12-31 |
Family
ID=33104490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0401808-7B1A BRPI0401808B1 (pt) | 2003-05-27 | 2004-05-24 | Dispositivo de fixação de um turbomotor no montante de um avião |
Country Status (10)
Country | Link |
---|---|
US (1) | US6988692B2 (pt) |
EP (1) | EP1481895B1 (pt) |
JP (1) | JP2004352231A (pt) |
BR (1) | BRPI0401808B1 (pt) |
CA (1) | CA2469943C (pt) |
DE (1) | DE602004002891T2 (pt) |
ES (1) | ES2276247T3 (pt) |
FR (1) | FR2855494B1 (pt) |
RU (1) | RU2346856C2 (pt) |
UA (1) | UA80689C2 (pt) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
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 |
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 |
FR2891243B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
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 |
GB0603539D0 (en) * | 2006-02-22 | 2006-04-05 | Airbus Uk Ltd | Control surface failsafe drop link |
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 |
US7762509B2 (en) * | 2007-10-18 | 2010-07-27 | United Technologies Corp. | Gas turbine engine systems involving rotatable annular supports |
US8950702B2 (en) * | 2008-01-18 | 2015-02-10 | United Technologies Corporation | Pylon and engine mount configuration |
DE102008021431A1 (de) * | 2008-04-29 | 2009-11-12 | Airbus Deutschland Gmbh | Flugzeug mit einer Energie-Versorgungsvorrichtung |
FR2933070B1 (fr) * | 2008-06-25 | 2010-08-20 | Snecma | Systeme propulsif d'aeronef |
FR2959210B1 (fr) * | 2010-04-21 | 2013-08-23 | Snecma | Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee |
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. |
FR2989952B1 (fr) | 2012-04-27 | 2014-04-18 | Aircelle Sa | Nacelle de turboreacteur a section aval |
WO2015010315A1 (en) | 2013-07-26 | 2015-01-29 | Mra Systems, Inc. | Aircraft engine pylon |
CN107108039B (zh) * | 2015-01-07 | 2019-08-30 | 洛德公司 | 飞行器发动机安装架 |
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 |
FR3053660A1 (fr) * | 2016-07-08 | 2018-01-12 | Airbus Operations | Attache moteur d'aeronef comprenant au moins un ecrou transversal et aeronef comprenant ladite attache moteur |
FR3086925B1 (fr) * | 2018-10-08 | 2020-09-11 | Safran Aircraft Engines | Ensemble de suspension pour une turbomachine |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5176339A (en) * | 1991-09-30 | 1993-01-05 | Lord Corporation | Resilient pivot type aircraft mounting |
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 |
US5860623A (en) * | 1995-05-03 | 1999-01-19 | The Boeing Company | Three link failsafe engine mount |
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 |
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 |
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 |
FR2820402B1 (fr) * | 2001-02-08 | 2003-05-02 | Eads Airbus Sa | Dispositif d'accrochage d'un moteur sur un aeronef |
FR2828167B1 (fr) * | 2001-07-31 | 2003-11-21 | Airbus France | Dispositif d'accrochage d'un moteur sur un aeronef |
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 |
US6843449B1 (en) * | 2004-02-09 | 2005-01-18 | General Electric Company | Fail-safe aircraft engine mounting system |
-
2003
- 2003-05-27 FR FR0306435A patent/FR2855494B1/fr not_active Expired - Fee Related
-
2004
- 2004-05-05 US US10/838,243 patent/US6988692B2/en not_active Expired - Lifetime
- 2004-05-13 JP JP2004143227A patent/JP2004352231A/ja active Pending
- 2004-05-17 ES ES04291252T patent/ES2276247T3/es not_active Expired - Lifetime
- 2004-05-17 DE DE602004002891T patent/DE602004002891T2/de not_active Expired - Lifetime
- 2004-05-17 EP EP04291252A patent/EP1481895B1/fr not_active Expired - Lifetime
- 2004-05-24 BR BRPI0401808-7B1A patent/BRPI0401808B1/pt not_active IP Right Cessation
- 2004-05-25 CA CA2469943A patent/CA2469943C/fr not_active Expired - Fee Related
- 2004-05-26 RU RU2004116111/11A patent/RU2346856C2/ru not_active IP Right Cessation
- 2004-05-26 UA UA20040504031A patent/UA80689C2/uk unknown
Also Published As
Publication number | Publication date |
---|---|
FR2855494B1 (fr) | 2006-09-22 |
FR2855494A1 (fr) | 2004-12-03 |
CA2469943A1 (fr) | 2004-11-27 |
US6988692B2 (en) | 2006-01-24 |
US20040251379A1 (en) | 2004-12-16 |
DE602004002891D1 (de) | 2006-12-07 |
JP2004352231A (ja) | 2004-12-16 |
EP1481895B1 (fr) | 2006-10-25 |
DE602004002891T2 (de) | 2007-09-06 |
RU2346856C2 (ru) | 2009-02-20 |
BRPI0401808B1 (pt) | 2013-12-31 |
UA80689C2 (en) | 2007-10-25 |
EP1481895A1 (fr) | 2004-12-01 |
ES2276247T3 (es) | 2007-06-16 |
CA2469943C (fr) | 2012-01-03 |
RU2004116111A (ru) | 2005-11-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B11A | Dismissal acc. art.33 of ipl - examination not requested within 36 months of filing | ||
B04C | Request for examination: application reinstated [chapter 4.3 patent gazette] | ||
B25D | Requested change of name of applicant approved |
Owner name: SNECMA (FR) Free format text: ALTERADO DE: SNECMA MOTEURS |
|
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. |
|
B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE A 15A ANUIDADE. |
|
B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |
Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2516 DE 26-03-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |