BR0315201A - Inversor de impulsão de dobra dupla - Google Patents
Inversor de impulsão de dobra duplaInfo
- Publication number
- BR0315201A BR0315201A BR0315201-4A BR0315201A BR0315201A BR 0315201 A BR0315201 A BR 0315201A BR 0315201 A BR0315201 A BR 0315201A BR 0315201 A BR0315201 A BR 0315201A
- Authority
- BR
- Brazil
- Prior art keywords
- door
- double fold
- locking
- shutter
- inverter
- 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
- 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
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- 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)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Power-Operated Mechanisms For Wings (AREA)
- Wind Motors (AREA)
Abstract
"INVERSOR DE IMPULSãO DE DOBRA DUPLA". Um inversor e impulsão de ventilador (36) inclui uma porta veneziana externa (54) ligada a uma porta bloqueadora interna 56 por meio de um elo de acionamento (58) em uma configuração de dobra dupla. A porta veneziana (54) fica acondicionada fechada no revestimento externo (38) da nacela de ventilador (16) fora da porta bloqueadora (56) acondicionada fechada no revestimento interno (40) da nacela. Um atuador (60) desdobra de modo a abrir as portas veneziana e bloqueadora, com a porta veneziana (54) estendendo-se em um sentido radial para fora e a porta bloqueadora (56) estendendo-se em um sentido radial para dentro de modo a inverter o fluxo de exaustão de ventilador durante uma operação de inversão de impulsão.
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US41784802P | 2002-10-11 | 2002-10-11 | |
US45671003P | 2003-03-22 | 2003-03-22 | |
US47816303P | 2003-06-13 | 2003-06-13 | |
PCT/US2003/031599 WO2004046533A2 (en) | 2002-10-11 | 2003-10-06 | Bifold door thrust reverser |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0315201A true BR0315201A (pt) | 2005-08-16 |
Family
ID=32329839
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0315201-4A BR0315201A (pt) | 2002-10-11 | 2003-10-06 | Inversor de impulsão de dobra dupla |
Country Status (5)
Country | Link |
---|---|
US (1) | US6895742B2 (pt) |
EP (1) | EP1558840A4 (pt) |
BR (1) | BR0315201A (pt) |
CA (1) | CA2501496A1 (pt) |
WO (1) | WO2004046533A2 (pt) |
Families Citing this family (71)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20040149861A1 (en) * | 2001-06-06 | 2004-08-05 | Strobl William Charles | S & H Cycle Engine |
US6845946B2 (en) * | 2003-02-21 | 2005-01-25 | The Nordam Group, Inc. | Self stowing thrust reverser |
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 |
US7790878B2 (en) * | 2004-10-22 | 2010-09-07 | Alnylam Pharmaceuticals, Inc. | RNAi modulation of RSV, PIV and other respiratory viruses and uses thereof |
US20110101158A1 (en) * | 2005-03-29 | 2011-05-05 | The Boeing Company | Thrust Reversers Including Monolithic Components |
US7571527B2 (en) * | 2005-03-29 | 2009-08-11 | The Boeing Company | Mandrel for fabrication of a monolithic composite nacelle panel |
US7690190B2 (en) * | 2005-05-11 | 2010-04-06 | The Boeing Company | Aircraft systems including cascade thrust reversers |
US20060288688A1 (en) * | 2005-06-22 | 2006-12-28 | Jean-Pierre Lair | Turbofan core thrust spoiler |
US7559507B2 (en) * | 2005-06-27 | 2009-07-14 | The Boeing Company | Thrust reversers including locking assemblies for inhibiting deflection |
JP4667141B2 (ja) * | 2005-07-05 | 2011-04-06 | ヤンマー株式会社 | 旋回作業車 |
US7484356B1 (en) * | 2005-07-26 | 2009-02-03 | Aeronautical Concepts Of Exhaust, Llc | Cascade reverser without blocker doors |
US7600371B2 (en) | 2005-10-18 | 2009-10-13 | The Boeing Company | Thrust reversers including support members for inhibiting deflection |
GB0606982D0 (en) * | 2006-04-07 | 2006-05-17 | Rolls Royce Plc | Aeroengine thrust reverser |
FR2904372B1 (fr) * | 2006-07-26 | 2008-10-31 | Snecma Sa | Tuyere d'ejection des gaz pour turbomachine a double flux ayant une section d'ejection ou de col variable par deplacement du capot secondaire |
US8015797B2 (en) * | 2006-09-21 | 2011-09-13 | Jean-Pierre Lair | Thrust reverser nozzle for a turbofan gas turbine engine |
US8413932B2 (en) * | 2010-04-10 | 2013-04-09 | Aerofex, Inc. | Peripheral control ejector |
US8151551B2 (en) * | 2006-10-12 | 2012-04-10 | United Technologies Corporation | Variable area fan nozzle thrust reverser |
US8127529B2 (en) | 2007-03-29 | 2012-03-06 | United Technologies Corporation | Variable area fan nozzle and thrust reverser |
CN101939528B (zh) * | 2007-08-08 | 2013-07-24 | 罗尔股份有限公司 | 具有旁通流的面积可调风扇喷嘴 |
US9759087B2 (en) | 2007-08-08 | 2017-09-12 | Rohr, Inc. | Translating variable area fan nozzle providing an upstream bypass flow exit |
US7878451B2 (en) * | 2007-11-15 | 2011-02-01 | Spirit Aerosystems, Inc. | Low-leakage seal system for pivot door type thrust reverser |
US8091827B2 (en) | 2007-11-16 | 2012-01-10 | The Nordam Group, Inc. | Thrust reverser door |
US8172175B2 (en) | 2007-11-16 | 2012-05-08 | The Nordam Group, Inc. | Pivoting door thrust reverser for a turbofan gas turbine engine |
US7735778B2 (en) | 2007-11-16 | 2010-06-15 | Pratt & Whitney Canada Corp. | Pivoting fairings for a thrust reverser |
US8052086B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser door |
US8051639B2 (en) * | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser |
US8052085B2 (en) * | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
US8201390B2 (en) * | 2007-12-12 | 2012-06-19 | Spirit Aerosystems, Inc. | Partial cascade thrust reverser |
FR2935354B1 (fr) * | 2008-09-02 | 2011-04-01 | Airbus France | Nacelle pour moteur a double flux |
US8127530B2 (en) | 2008-06-19 | 2012-03-06 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
FR2935444B1 (fr) * | 2008-09-02 | 2010-09-10 | Airbus France | Inverseur de poussee et nacelle pour aeronef muni d'au moins un tel inverseur |
WO2010068636A2 (en) * | 2008-12-08 | 2010-06-17 | Firestar Engineering, Llc | Regeneratively cooled porous media jacket |
US8109467B2 (en) * | 2009-04-24 | 2012-02-07 | United Technologies Corporation | Thrust reverser assembly with shaped drag links |
US8141818B2 (en) * | 2009-07-02 | 2012-03-27 | Honeywell International Inc. | Ram door assemblies |
EP2452064A4 (en) * | 2009-07-07 | 2014-11-19 | Firestar Engineering Llc | HISTORIZED POROSITY FLASHBACK SUPPRESSIVE ELEMENTS FOR MONOPROPELLANT OR PRE-MIXED BIPROPELLANT SYSTEMS |
US8869507B2 (en) * | 2010-01-13 | 2014-10-28 | United Technologies Corporation | Translatable cascade thrust reverser |
US20120079805A1 (en) * | 2010-09-30 | 2012-04-05 | Alan Roy Stuart | Thrust reverser assembly |
US9181898B2 (en) | 2011-09-20 | 2015-11-10 | United Technologies Corporation | Thrust reverser for a gas turbine engine with moveable doors |
FR2982323B1 (fr) * | 2011-11-07 | 2013-11-15 | Aircelle Sa | Dispositif d'inversion de poussee |
US9623976B2 (en) * | 2012-07-25 | 2017-04-18 | Rohr, Inc. | Nacelle for a high bypass ratio engine with multiple flow paths |
US10400621B2 (en) * | 2013-03-04 | 2019-09-03 | United Technologies Corporation | Pivot door thrust reverser with variable area nozzle |
US9163583B2 (en) | 2013-05-01 | 2015-10-20 | Rohr, Inc. | System, apparatus, and method for thrust vectoring |
WO2015080785A2 (en) * | 2013-09-19 | 2015-06-04 | United Technologies Corporation | Extended thrust reverser cascade |
US9765729B2 (en) * | 2013-10-17 | 2017-09-19 | Rohr, Inc. | Thrust reverser fan ramp with blocker door pocket |
US9611808B2 (en) * | 2014-03-21 | 2017-04-04 | Rohr, Inc. | Blocker door lock mechanism of a thrust reverser for a turbofan engine |
US10487690B2 (en) * | 2014-08-18 | 2019-11-26 | Rohr, Inc. | Actively controlled cooling air exhaust door on an aircraft engine nacelle |
US9945324B2 (en) * | 2014-11-06 | 2018-04-17 | Rohr, Inc. | Sleeve linkage for thrust reverser |
US10309343B2 (en) * | 2014-11-06 | 2019-06-04 | Rohr, Inc. | Split sleeve hidden door thrust reverser |
US9784214B2 (en) * | 2014-11-06 | 2017-10-10 | Rohr, Inc. | Thrust reverser with hidden linkage blocker doors |
US10208708B2 (en) | 2015-01-29 | 2019-02-19 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
US10184426B2 (en) * | 2015-06-22 | 2019-01-22 | Rohr, Inc. | Thrust reverser with forward positioned blocker doors |
US10024270B2 (en) * | 2015-10-13 | 2018-07-17 | Rohr, Inc. | Vibration damping drag link fitting for a thrust reverser |
US10077740B2 (en) | 2015-10-16 | 2018-09-18 | The Boeing Company | Folding door thrust reversers for aircraft engines |
US10247136B2 (en) | 2015-12-03 | 2019-04-02 | General Electric Company | Thrust reverser system for a gas turbine engine |
US10473057B2 (en) | 2015-12-14 | 2019-11-12 | Rohr, Inc. | Thrust reverser system with translating elements |
US10302044B2 (en) | 2015-12-18 | 2019-05-28 | Rohr, Inc. | Translating cascade thrust reverser with control of blocker door |
US10648426B2 (en) | 2016-01-14 | 2020-05-12 | Honeywell International Inc. | Single row vane assembly for a thrust reverser |
US10337454B2 (en) * | 2016-01-25 | 2019-07-02 | Honeywell International Inc. | Thrust reverser with asymmetric vane geometry |
US10655564B2 (en) | 2016-05-13 | 2020-05-19 | Rohr, Inc. | Thrust reverser system with hidden blocker doors |
US9976696B2 (en) | 2016-06-21 | 2018-05-22 | Rohr, Inc. | Linear actuator with multi-degree of freedom mounting structure |
CN108661821B (zh) | 2017-03-31 | 2022-03-18 | Mra系统有限责任公司 | 反推力器组件及操作方法 |
FR3067760B1 (fr) * | 2017-06-14 | 2019-06-28 | Airbus Operations | Turboreacteur comportant une nacelle equipee de volets inverseurs |
GB2564891A (en) * | 2017-07-26 | 2019-01-30 | Short Brothers Plc | Nacelle with thrust reverser |
US10731738B2 (en) | 2017-11-27 | 2020-08-04 | Rohr, Inc. | Kinematic system with motion control device |
US11111879B2 (en) * | 2018-01-12 | 2021-09-07 | Rohr, Inc. | Thrust reverser pivot door with extended forward edge |
US10794328B2 (en) | 2018-07-06 | 2020-10-06 | Rohr, Inc. | Thrust reverser with blocker door folding linkage |
EP3667051B1 (en) * | 2018-12-14 | 2023-02-08 | Airbus Operations GmbH | Turbofan engine comprising a thrust reverser unit with tilting beams |
CN109441661A (zh) * | 2018-12-21 | 2019-03-08 | 湖北鸿翼航空科技有限公司 | 一种涡轮风扇发动机短舱外涵道反推力装置 |
US11427341B2 (en) | 2019-09-30 | 2022-08-30 | Rohr, Inc. | Linkage supporting a door of an aircraft propulsion system |
US11511874B2 (en) | 2019-09-30 | 2022-11-29 | Rohr, Inc. | Linkage(s) between inner and outer cowl doors |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1127828A (en) * | 1966-06-29 | 1968-09-18 | Rolls Royce | Fan thrust reverser for jet propulsion plant |
US3503211A (en) * | 1968-04-10 | 1970-03-31 | Rohr Corp | Thrust reverser |
US3614037A (en) * | 1969-09-22 | 1971-10-19 | Boeing Co | Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser |
US3815357A (en) * | 1971-01-28 | 1974-06-11 | Rohr Industries Inc | Thrust reversing apparatus |
US3764096A (en) * | 1972-02-24 | 1973-10-09 | Rohr Industries Inc | Thrust reversing apparatus |
US3739582A (en) * | 1972-04-13 | 1973-06-19 | Rohr Industries Inc | Thrust reversing apparatus |
US3779010A (en) * | 1972-08-17 | 1973-12-18 | Gen Electric | Combined thrust reversing and throat varying mechanism for a gas turbine engine |
US3829020A (en) * | 1973-06-13 | 1974-08-13 | Boeing Co | Translating sleeve variable area nozzle and thrust reverser |
FR2622929A1 (fr) * | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a grilles,a section variable d'ejection |
FR2727468B1 (fr) * | 1994-11-30 | 1996-12-27 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a obstacles aval |
US5706649A (en) * | 1995-04-03 | 1998-01-13 | Boeing North American, Inc. | Multi axis thrust vectoring for turbo fan engines |
US5655360A (en) * | 1995-05-31 | 1997-08-12 | General Electric Company | Thrust reverser with variable nozzle |
FR2741910B1 (fr) * | 1995-11-30 | 1998-01-02 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes a panneau arriere articule |
US5826823A (en) * | 1996-02-07 | 1998-10-27 | Rohr, Inc. | Actuator and safety lock system for pivoting door thrust reverser for aircraft jet engine |
FR2745036B1 (fr) * | 1996-02-15 | 1998-04-03 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes associees a un panneau amont |
FR2764339B1 (fr) * | 1997-06-05 | 1999-07-16 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes associees a une casquette amont mobile |
US5987880A (en) * | 1997-07-08 | 1999-11-23 | Mcdonnell Douglas Corporation | Supersonic engine, multi-port thrust reversing system |
FR2777043B1 (fr) * | 1998-04-02 | 2000-05-12 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes formant ecopes associees a un capotage externe articule |
US6568172B2 (en) * | 2001-09-27 | 2003-05-27 | The Nordam Group, Inc. | Converging nozzle thrust reverser |
-
2003
- 2003-10-06 EP EP03808406A patent/EP1558840A4/en not_active Withdrawn
- 2003-10-06 WO PCT/US2003/031599 patent/WO2004046533A2/en not_active Application Discontinuation
- 2003-10-06 US US10/679,882 patent/US6895742B2/en not_active Expired - Fee Related
- 2003-10-06 BR BR0315201-4A patent/BR0315201A/pt not_active IP Right Cessation
- 2003-10-06 CA CA002501496A patent/CA2501496A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
EP1558840A2 (en) | 2005-08-03 |
WO2004046533A3 (en) | 2004-08-12 |
US6895742B2 (en) | 2005-05-24 |
EP1558840A4 (en) | 2006-03-22 |
WO2004046533A2 (en) | 2004-06-03 |
US20040068978A1 (en) | 2004-04-15 |
CA2501496A1 (en) | 2004-06-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 8A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2160 DE 29/05/2012. |