WO2009087282A3 - Inverseur de poussée à portes pour turboréacteur - Google Patents
Inverseur de poussée à portes pour turboréacteur Download PDFInfo
- Publication number
- WO2009087282A3 WO2009087282A3 PCT/FR2008/001364 FR2008001364W WO2009087282A3 WO 2009087282 A3 WO2009087282 A3 WO 2009087282A3 FR 2008001364 W FR2008001364 W FR 2008001364W WO 2009087282 A3 WO2009087282 A3 WO 2009087282A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- thrust reverser
- door
- jet engine
- type thrust
- doors
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Wing Frames And Configurations (AREA)
- Hinges (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Power-Operated Mechanisms For Wings (AREA)
Abstract
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/811,318 US20100281849A1 (en) | 2008-01-08 | 2008-10-01 | Door-type thrust reverser for a jet engine |
CN2008801234292A CN101910598A (zh) | 2008-01-08 | 2008-10-01 | 用于喷气发动机的门式推力反向器 |
EP08870411A EP2232040A2 (fr) | 2008-01-08 | 2008-10-01 | Inverseur de poussée à portes pour turboréacteur |
CA2705361A CA2705361A1 (fr) | 2008-01-08 | 2008-10-01 | Inverseur de poussee a portes pour turboreacteur |
BRPI0822149-9A BRPI0822149A2 (pt) | 2008-01-08 | 2008-10-01 | Reversor de empuxo e nacela para motor a jato |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0800083A FR2926112A1 (fr) | 2008-01-08 | 2008-01-08 | Inverseur de poussee a portes pour turboreacteur |
FR08/00083 | 2008-01-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009087282A2 WO2009087282A2 (fr) | 2009-07-16 |
WO2009087282A3 true WO2009087282A3 (fr) | 2009-09-03 |
Family
ID=39512820
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/FR2008/001364 WO2009087282A2 (fr) | 2008-01-08 | 2008-10-01 | Inverseur de poussée à portes pour turboréacteur |
Country Status (8)
Country | Link |
---|---|
US (1) | US20100281849A1 (fr) |
EP (1) | EP2232040A2 (fr) |
CN (1) | CN101910598A (fr) |
BR (1) | BRPI0822149A2 (fr) |
CA (1) | CA2705361A1 (fr) |
FR (1) | FR2926112A1 (fr) |
RU (1) | RU2010132307A (fr) |
WO (1) | WO2009087282A2 (fr) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2980825B1 (fr) * | 2011-09-29 | 2013-09-13 | Aircelle Sa | Porte d'inverseur de poussee a ouvertures laterales |
FR2982324B1 (fr) * | 2011-11-09 | 2013-11-15 | Aircelle Sa | Inverseur de poussee a portes jumelles |
GB2510635B (en) * | 2013-02-12 | 2017-11-01 | Ge Aviat Systems Ltd | Method for predicting faults in an aircraft thrust reverser system |
CN103267642B (zh) * | 2013-05-24 | 2015-08-19 | 北京航空航天大学 | 一种适用于测量1n至300n推力的发动机推力架 |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020145078A1 (en) * | 2001-04-05 | 2002-10-10 | Hurel Hispano-Le-Havre | System for the synchronized locking of the doors of a thrust reverser |
WO2004097202A2 (fr) * | 2003-03-22 | 2004-11-11 | The Nordam Group, Inc | Inverseur de poussee a verrouillage reciproque par articulation |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3279182A (en) * | 1965-06-07 | 1966-10-18 | Gen Electric | Thrust reverser |
US4026105A (en) * | 1975-03-25 | 1977-05-31 | The Boeing Company | Jet engine thrust reverser |
GB9120658D0 (en) * | 1991-09-27 | 1991-11-06 | Short Brothers Plc | Ducted fan turbine engine |
FR2748778B1 (fr) * | 1996-05-15 | 1998-06-19 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes associees a un panneau amont |
FR2756868B1 (fr) * | 1996-12-05 | 1999-01-08 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes maintenues dans les lignes de nacelle |
FR2846375B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes |
US8127532B2 (en) * | 2008-11-26 | 2012-03-06 | The Boeing Company | Pivoting fan nozzle nacelle |
-
2008
- 2008-01-08 FR FR0800083A patent/FR2926112A1/fr not_active Withdrawn
- 2008-10-01 US US12/811,318 patent/US20100281849A1/en not_active Abandoned
- 2008-10-01 WO PCT/FR2008/001364 patent/WO2009087282A2/fr active Application Filing
- 2008-10-01 BR BRPI0822149-9A patent/BRPI0822149A2/pt not_active IP Right Cessation
- 2008-10-01 RU RU2010132307/06A patent/RU2010132307A/ru not_active Application Discontinuation
- 2008-10-01 CN CN2008801234292A patent/CN101910598A/zh active Pending
- 2008-10-01 EP EP08870411A patent/EP2232040A2/fr not_active Withdrawn
- 2008-10-01 CA CA2705361A patent/CA2705361A1/fr not_active Abandoned
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20020145078A1 (en) * | 2001-04-05 | 2002-10-10 | Hurel Hispano-Le-Havre | System for the synchronized locking of the doors of a thrust reverser |
WO2004097202A2 (fr) * | 2003-03-22 | 2004-11-11 | The Nordam Group, Inc | Inverseur de poussee a verrouillage reciproque par articulation |
Also Published As
Publication number | Publication date |
---|---|
RU2010132307A (ru) | 2012-02-20 |
EP2232040A2 (fr) | 2010-09-29 |
FR2926112A1 (fr) | 2009-07-10 |
CA2705361A1 (fr) | 2009-07-16 |
US20100281849A1 (en) | 2010-11-11 |
BRPI0822149A2 (pt) | 2015-06-23 |
WO2009087282A2 (fr) | 2009-07-16 |
CN101910598A (zh) | 2010-12-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
WO2008039734A3 (fr) | Système de protection de couplage | |
GB2425516B (en) | Thrust vectoring missile turbojet | |
WO2008145832A3 (fr) | Dispositif de verrouillage d'une partie ouvrante de nacelle de turboréacteur par rapport à une partie fixe, et nacelle équipée d'un tel dispositif | |
FR2914700B1 (fr) | Inverseur de poussee pour moteur a reaction | |
GB0616740D0 (en) | Aircraft engine thrust reverser | |
BRPI1011276A2 (pt) | reversor de empuxo e nacela para motorista a jato turboventilador. | |
CA2812580C (fr) | Nacelle dotee de portes de capot articulees permettant d'acceder au moteur | |
BR112012027996A2 (pt) | reversor de empuxo para uma nacela de motor de turbina, e nacela de motor de turbina | |
GB0619615D0 (en) | A door for opening and closing a door aperture in an aircraft | |
EP2050948A3 (fr) | Ensemble d'un moteur à turbine à gaz avec une tuyère à section variable et procédé de réglage de cette tuyère | |
GB0606982D0 (en) | Aeroengine thrust reverser | |
EP1903205A3 (fr) | Buse d'inverseur de poussée pour un moteur à turbine à gaz de réacteur à double flux | |
GB0608985D0 (en) | Aeroengine thrust reverser | |
DE60301007D1 (de) | Elektromechanische Schubumkehrvorrichtung mit einer dauerhafte Positionskontrolle für einen Flugzeugstriebwerk | |
BRPI0921975A2 (pt) | reversor de empuxo para nacela de motor turbofan, nacela de motor turbofan e aeronave. | |
WO2008076276A3 (fr) | Ensemble de rotor et son procédé de raccordement | |
GB2425573B (en) | Fladed supersonic missile turbojet | |
BRPI0817588A2 (pt) | Atuador linear telescópio e reversor de empuxo nacela de motor turbojato | |
GB2443948B (en) | Turbofan engine cowl assembly and method of operating the same | |
GB2425574B (en) | Supersonic missile turbojet engine | |
GB0722174D0 (en) | Turbofan engine cowl assembly and method of operating the same | |
ATE523674T1 (de) | Flugzeugmotorgondeleinlassöffnung | |
EP2060765A3 (fr) | Carénages pivotants pour inverseur de poussée | |
GB0722369D0 (en) | turbofan engine nozzle assembly and method for perating the same | |
WO2011066365A3 (fr) | Rail de support pour buse de soufflante à section variable |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
WWE | Wipo information: entry into national phase |
Ref document number: 200880123429.2 Country of ref document: CN |
|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 08870411 Country of ref document: EP Kind code of ref document: A2 |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2705361 Country of ref document: CA |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2008870411 Country of ref document: EP |
|
WWE | Wipo information: entry into national phase |
Ref document number: 12811318 Country of ref document: US |
|
NENP | Non-entry into the national phase |
Ref country code: DE |
|
WWE | Wipo information: entry into national phase |
Ref document number: 2010132307 Country of ref document: RU |
|
ENP | Entry into the national phase |
Ref document number: PI0822149 Country of ref document: BR Kind code of ref document: A2 Effective date: 20100707 |