BRPI0818257A2 - Reversor de empuxo tipo cascata e nacela de avião - Google Patents
Reversor de empuxo tipo cascata e nacela de aviãoInfo
- Publication number
- BRPI0818257A2 BRPI0818257A2 BRPI0818257A BRPI0818257A2 BR PI0818257 A2 BRPI0818257 A2 BR PI0818257A2 BR PI0818257 A BRPI0818257 A BR PI0818257A BR PI0818257 A2 BRPI0818257 A2 BR PI0818257A2
- Authority
- BR
- Brazil
- Prior art keywords
- thrust reverser
- cascade thrust
- airplane nacelle
- nacelle
- airplane
- 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
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- 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
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/827—Sound absorbing structures or liners
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Soundproofing, Sound Blocking, And Sound Damping (AREA)
- Special Spraying Apparatus (AREA)
- Body Structure For Vehicles (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0707501A FR2922958B1 (fr) | 2007-10-25 | 2007-10-25 | Inverseur de poussee a grilles |
PCT/FR2008/001264 WO2009066037A1 (fr) | 2007-10-25 | 2008-09-10 | Inverseur de poussee a grilles |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0818257A2 true BRPI0818257A2 (pt) | 2015-04-14 |
Family
ID=39491381
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0818257 BRPI0818257A2 (pt) | 2007-10-25 | 2008-09-10 | Reversor de empuxo tipo cascata e nacela de avião |
Country Status (8)
Country | Link |
---|---|
US (1) | US9140211B2 (pt) |
EP (1) | EP2209980A1 (pt) |
CN (1) | CN101835969B (pt) |
BR (1) | BRPI0818257A2 (pt) |
CA (1) | CA2702010A1 (pt) |
FR (1) | FR2922958B1 (pt) |
RU (1) | RU2472960C2 (pt) |
WO (1) | WO2009066037A1 (pt) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2949141B1 (fr) * | 2009-08-14 | 2011-07-15 | Aircelle Sa | Dispositif d'inversion de poussee |
FR2965588B1 (fr) * | 2010-10-04 | 2015-05-01 | Aircelle Sa | Ensemble propulsif d'aeronef |
FR2978497B1 (fr) * | 2011-07-27 | 2013-08-16 | Aircelle Sa | Cadre arriere pour une structure d'inversion de poussee a grilles de deviation d'une nacelle de turboreacteur |
FR2994586B1 (fr) * | 2012-08-20 | 2014-08-08 | Aircelle Sa | Ensemble de poussee a grilles pour turboreacteur d'aeronef |
FR3007078B1 (fr) * | 2013-06-12 | 2015-06-05 | Aircelle Sa | Ferrure pour l'attache d'un verin d'un inverseur a portes d'une nacelle de turboreacteur et nacelle de turboreacteur |
FR3024753B1 (fr) * | 2014-08-11 | 2016-08-26 | Snecma | Ensemble de liaison pour parties de carter d'une turbomachine |
FR3031726B1 (fr) * | 2015-01-21 | 2017-02-24 | Aircelle Sa | Systeme pour la pose et la depose d’un ensemble propulsif sur un mat d’un aeronef |
US20180128206A1 (en) * | 2016-11-09 | 2018-05-10 | General Electric Company | Gas turbine engine |
FR3069891B1 (fr) | 2017-08-07 | 2021-03-19 | Safran Nacelles | Grille d’inverseur de poussee pour nacelle d’aeronef |
RU2654531C1 (ru) * | 2017-09-29 | 2018-05-21 | Акционерное общество "ТВЭЛ" (АО "ТВЭЛ") | Тепловыделяющая сборка ядерного реактора |
FR3094757A1 (fr) * | 2019-04-04 | 2020-10-09 | Airbus Operations | Turboreacteur comportant une nacelle equipee d’un systeme inverseur et une grille de cascades mobile |
FR3122904B1 (fr) * | 2021-05-17 | 2023-04-28 | Safran Nacelles | Inverseur de poussée à grilles mobiles, comprenant une structure arrière de support de grilles intégrant une fonction acoustique |
Family Cites Families (40)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3241771A (en) * | 1963-09-18 | 1966-03-22 | Gen Electric | Thrust deflector and reverser |
US3241312A (en) * | 1963-09-18 | 1966-03-22 | Gen Electric | Thrust deflector |
US3241313A (en) * | 1963-09-18 | 1966-03-22 | Gen Electric | Thrust deflector |
US3248878A (en) * | 1963-09-18 | 1966-05-03 | Gen Electric | Thrust deflector and reverser |
US3281082A (en) * | 1963-10-16 | 1966-10-25 | Rolls Royce | Nozzles, e.g. deflecting jet discharge nozzles for jet propulsion engines |
US3292880A (en) * | 1964-09-01 | 1966-12-20 | Gen Electric | Thrust deflecting mechanism |
US3292864A (en) * | 1965-01-21 | 1966-12-20 | Gen Electric | Thrust reverser and deflector |
US3262270A (en) * | 1965-06-07 | 1966-07-26 | Gen Electric | Thrust reverser |
US3262271A (en) * | 1965-07-30 | 1966-07-26 | Gen Electric | Thrust reverser |
US3500645A (en) * | 1968-04-10 | 1970-03-17 | Rohr Corp | Thrust reverser |
US3717304A (en) * | 1970-05-06 | 1973-02-20 | Rolls Royce | Thrust reverser for fluid flow engine |
US3797785A (en) * | 1972-08-31 | 1974-03-19 | Rohr Industries Inc | Thrust modulating apparatus |
US4026105A (en) * | 1975-03-25 | 1977-05-31 | The Boeing Company | Jet engine thrust reverser |
US4193569A (en) * | 1976-02-12 | 1980-03-18 | Nichols William B | Process and apparatuses for landing aircraft on water covered landing surfaces |
US4458863A (en) * | 1980-03-10 | 1984-07-10 | The Boeing Company | Strut supported inlet |
FR2496766A1 (fr) * | 1980-12-23 | 1982-06-25 | Snecma | Dispositif de guidage de carenage mobile d'un systeme d'inversion de poussee |
US4778110A (en) * | 1982-09-30 | 1988-10-18 | Rohr Industries, Inc. | Modular composite cascade assembly |
US4596621A (en) * | 1984-01-03 | 1986-06-24 | The Boeing Company | Method of making a composite bond cascade for a thrust reverser unit of an aircraft engine nacelle |
GB2196911B (en) * | 1986-10-30 | 1990-03-14 | Rolls Royce Plc | Thrust reverser |
GB9014381D0 (en) * | 1990-06-28 | 1990-08-22 | Short Brothers Plc | A composite structural component |
US5313788A (en) * | 1991-08-07 | 1994-05-24 | General Electric Company | Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine |
GB2323065B (en) * | 1993-03-13 | 1998-12-09 | Rolls Royce Plc | Vectorable nozzle for aircraft |
FR2736390B1 (fr) * | 1995-07-05 | 1997-08-08 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a une coquille |
FR2758161B1 (fr) * | 1997-01-09 | 1999-02-05 | Hispano Suiza Sa | Inverseur de poussee a grilles a installation de verin de commande optimisee |
US5927647A (en) * | 1997-09-24 | 1999-07-27 | Rohr, Inc. | Blocker door frame pressure structure for translating cowl of cascade thrust reverser for aircraft jet engine |
FR2783018B1 (fr) * | 1998-09-03 | 2000-10-13 | Hispano Suiza Sa | Nacelle de turboreacteur a double flux a element mobile mis a la masse |
US6170254B1 (en) * | 1998-12-18 | 2001-01-09 | Rohr, Inc. | Translating sleeve for cascade type thrust reversing system for fan gas turbine engine for an aircraft |
US6311928B1 (en) * | 2000-01-05 | 2001-11-06 | Stage Iii Technologies, L.C. | Jet engine cascade thrust reverser for use with mixer/ejector noise suppressor |
FR2804474B1 (fr) * | 2000-01-27 | 2002-06-28 | Hispano Suiza Sa | Inverseur de poussee a grilles aubagees de deviation a structure arriere fixe |
US6681559B2 (en) * | 2001-07-24 | 2004-01-27 | Honeywell International, Inc. | Thrust reverser position determination system and method |
FR2830051B1 (fr) * | 2001-09-27 | 2003-11-07 | Hurel Hispano Le Havre | Systeme de verrouillage sur un inverseur de poussee a grilles |
US6557799B1 (en) * | 2001-11-09 | 2003-05-06 | The Boeing Company | Acoustic treated thrust reverser bullnose fairing assembly |
US7146796B2 (en) * | 2003-09-05 | 2006-12-12 | The Nordam Group, Inc. | Nested latch thrust reverser |
US7264203B2 (en) * | 2003-10-02 | 2007-09-04 | The Nordam Group, Inc. | Spider actuated thrust reverser |
FR2872222B1 (fr) * | 2004-06-29 | 2006-08-25 | Hurel Hispano Sa | Procede d'ouverture d'un capot mobile equipant un inverseur de poussee |
US7093424B2 (en) * | 2004-08-24 | 2006-08-22 | Honeywell International, Inc. | Thrust reverser system electro-mechanical brake manual release mechanism |
US7409820B2 (en) * | 2004-11-16 | 2008-08-12 | Honeywell International Inc. | Electrical thrust reverser tertiary lock system including a voltage limiting circuit |
US7435180B2 (en) * | 2005-01-10 | 2008-10-14 | Honeywell International Inc. | Thrust reverser actuator system flex shaft assembly |
GB0606982D0 (en) * | 2006-04-07 | 2006-05-17 | Rolls Royce Plc | Aeroengine thrust reverser |
US20070237575A1 (en) * | 2006-04-11 | 2007-10-11 | Honeywell International, Inc. | Flexible shaft inline coupler |
-
2007
- 2007-10-25 FR FR0707501A patent/FR2922958B1/fr active Active
-
2008
- 2008-09-10 BR BRPI0818257 patent/BRPI0818257A2/pt not_active IP Right Cessation
- 2008-09-10 CN CN200880112995.3A patent/CN101835969B/zh active Active
- 2008-09-10 WO PCT/FR2008/001264 patent/WO2009066037A1/fr active Application Filing
- 2008-09-10 CA CA2702010A patent/CA2702010A1/fr not_active Abandoned
- 2008-09-10 US US12/739,344 patent/US9140211B2/en active Active
- 2008-09-10 EP EP08851663A patent/EP2209980A1/fr not_active Withdrawn
- 2008-09-10 RU RU2010120236/06A patent/RU2472960C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
WO2009066037A1 (fr) | 2009-05-28 |
US9140211B2 (en) | 2015-09-22 |
RU2472960C2 (ru) | 2013-01-20 |
CN101835969B (zh) | 2014-08-13 |
RU2010120236A (ru) | 2011-11-27 |
US20100251693A1 (en) | 2010-10-07 |
CN101835969A (zh) | 2010-09-15 |
FR2922958B1 (fr) | 2009-11-20 |
FR2922958A1 (fr) | 2009-05-01 |
EP2209980A1 (fr) | 2010-07-28 |
CA2702010A1 (fr) | 2009-05-28 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application fees: dismissal - article 86 of industrial property law |
Free format text: REFERENTE A 8A ANUIDADE. |
|
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |