BR0213349A - sistema de controle para movimentar um reversor de empuxo - Google Patents
sistema de controle para movimentar um reversor de empuxoInfo
- Publication number
- BR0213349A BR0213349A BRPI0213349-0A BR0213349A BR0213349A BR 0213349 A BR0213349 A BR 0213349A BR 0213349 A BR0213349 A BR 0213349A BR 0213349 A BR0213349 A BR 0213349A
- Authority
- BR
- Brazil
- Prior art keywords
- thrust
- thrust reverser
- components
- moving
- control system
- Prior art date
Links
- 230000005540 biological transmission Effects 0.000 abstract 1
- 230000007246 mechanism Effects 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
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
-
- 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
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
- F15B11/00—Servomotor systems without provision for follow-up action; Circuits therefor
- F15B11/16—Servomotor systems without provision for follow-up action; Circuits therefor with two or more servomotors
- F15B11/22—Synchronisation of the movement of two or more servomotors
-
- 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
- F05D2270/00—Control
- F05D2270/01—Purpose of the control system
- F05D2270/11—Purpose of the control system to prolong engine life
- F05D2270/114—Purpose of the control system to prolong engine life by limiting mechanical stresses
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Transmission Devices (AREA)
- Retarders (AREA)
- Structure Of Transmissions (AREA)
Abstract
"SISTEMA DE CONTROLE PARA MOVIMENTAR UM REVERSOR DE EMPUXO". Um sistema reversor de empuxo que possui um ou mais componentes movediços de reversor de empuxo para redirecionar o empuxo de um motor a jato. O sistema reversor de empuxo possui um limitador de torque acoplado entre mecanismos de sincronia que acoplam mecanicamente atuadores usados para acionar o reversor de empuxo. O limitador de torque reduz o potencial quanto à transmissão de torque excessivo entre diferentes componentes movediços do reversor de empuxo, e reduz a probabilidade de danos secundários ao sistema devido a um emperramento no sistema. Desse modo, o custo e/ou peso associados com cada um dos componentes que compõem o sistema pode ser reduzido.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/981,011 US6598386B2 (en) | 2001-10-16 | 2001-10-16 | Jet engine thrust reverser system having torque limited synchronization |
PCT/US2002/032965 WO2003033898A1 (en) | 2001-10-16 | 2002-10-16 | Jet engine thrust reverser system having torque limited synchronization |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0213349A true BR0213349A (pt) | 2006-05-23 |
Family
ID=25528030
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0213349-0A BR0213349A (pt) | 2001-10-16 | 2002-10-16 | sistema de controle para movimentar um reversor de empuxo |
Country Status (6)
Country | Link |
---|---|
US (1) | US6598386B2 (pt) |
EP (1) | EP1436497A1 (pt) |
JP (1) | JP2005506483A (pt) |
BR (1) | BR0213349A (pt) |
CA (1) | CA2463817A1 (pt) |
WO (1) | WO2003033898A1 (pt) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6598386B2 (en) | 2001-10-16 | 2003-07-29 | Honeywell International, Inc. | Jet engine thrust reverser system having torque limited synchronization |
US6655125B2 (en) * | 2001-12-05 | 2003-12-02 | Honeywell International Inc. | System architecture for electromechanical thrust reverser actuation systems |
FR2835021B1 (fr) * | 2002-01-24 | 2004-04-16 | Snecma Moteurs | Ensemble d'actionnement a verins hydrauliques synchronises |
US6666307B1 (en) * | 2002-08-05 | 2003-12-23 | Honeywell International, Inc. | Thrust reverser system with a pass-through torque activated brake |
FR2846375B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes |
FR2846377B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position |
US6786315B1 (en) * | 2003-03-28 | 2004-09-07 | Honeywell International, Inc. | Thrust reverser system with sequential torque decoupler |
US6966175B2 (en) * | 2003-05-09 | 2005-11-22 | The Nordam Group, Inc. | Rotary adjustable exhaust nozzle |
US6974107B2 (en) * | 2003-06-18 | 2005-12-13 | Honeywell International, Inc. | Thrust reverser system actuator having an integral torque limiter |
US7264203B2 (en) * | 2003-10-02 | 2007-09-04 | The Nordam Group, Inc. | Spider actuated thrust reverser |
GB0421568D0 (en) * | 2004-09-29 | 2004-10-27 | Smiths Group Plc | Drive assemblies |
US20070237575A1 (en) * | 2006-04-11 | 2007-10-11 | Honeywell International, Inc. | Flexible shaft inline coupler |
US7721551B2 (en) * | 2006-06-29 | 2010-05-25 | United Technologies Corporation | Fan variable area nozzle for a gas turbine engine fan nacelle |
FR2920202B1 (fr) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | Systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur |
FR2933126B1 (fr) * | 2008-06-25 | 2012-11-02 | Snecma | Actionnement d'un inverseur de poussee dans une turbomachine |
GB0917065D0 (en) * | 2009-09-29 | 2009-11-11 | Goodrich Actuation Systems Ltd | Thrust reverser actuation |
US20110296812A1 (en) * | 2010-06-08 | 2011-12-08 | Honeywell International Inc. | Thrust reverser actuation system architecture |
US8549834B2 (en) | 2010-10-21 | 2013-10-08 | United Technologies Corporation | Gas turbine engine with variable area fan nozzle |
US9038367B2 (en) | 2011-09-16 | 2015-05-26 | United Technologies Corporation | Fan case thrust reverser |
US10145335B2 (en) | 2012-09-28 | 2018-12-04 | United Technologies Corporation | Turbomachine thrust reverser |
CA2913527C (en) * | 2013-06-07 | 2018-01-09 | Ge Aviation Systems Llc | Engine with a thrust reverser lockout mechanism |
FR3007800B1 (fr) * | 2013-07-01 | 2017-10-20 | Aircelle Sa | Inverseur de poussee d’une nacelle de turboreacteur, comprenant des grilles partiellement integrees dans les capots |
KR101441414B1 (ko) | 2013-07-15 | 2014-09-25 | 국방과학연구소 | 가변노즐의 지상 시험장치 |
FR3008741B1 (fr) | 2013-07-17 | 2017-04-28 | Aircelle Sa | Systeme inverseur de poussee electrique pour nacelle de moteur d'aeronef et nacelle de moteur d'aeronef ainsi equipee |
FR3028295B1 (fr) * | 2014-11-06 | 2020-01-17 | Safran Electronics & Defense | Systeme d'actionnement d'une structure mobile d'un inverseur de poussee d'un aeronef, inverseur de poussee et reacteur comprenant un tel systeme. |
EP3269971A1 (en) * | 2016-07-13 | 2018-01-17 | Goodrich Actuation Systems Limited | Hydraulically driven thrust reverser |
US10773795B2 (en) * | 2018-09-24 | 2020-09-15 | The Boeing Company | Distributed linear hydraulic high lift actuation system with synchronization members |
US11215140B2 (en) * | 2019-12-18 | 2022-01-04 | Rolls-Royce Deutschland Ltd & Co. Kg | Exhaust nozzle of a gas turbine engine |
US11781502B2 (en) * | 2020-05-05 | 2023-10-10 | Rohr, Inc. | Actuation system for a thrust reverser of an aircraft propulsion system |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2660281A (en) * | 1949-02-25 | 1953-11-24 | Bendix Aviat Corp | Slip clutch for screw actuators |
US2819589A (en) * | 1954-04-01 | 1958-01-14 | Gen Motors Corp | Fluid pressure actuator and synchronizing means therefor |
US3596740A (en) * | 1970-01-27 | 1971-08-03 | Trw Inc | Torque limiter |
US4442928A (en) * | 1981-10-02 | 1984-04-17 | The Bendix Corporation | Actuator |
US4714006A (en) | 1982-02-24 | 1987-12-22 | Pneumo Corporation | Fluid actuator with feedback mechanism |
US4459121A (en) | 1982-03-12 | 1984-07-10 | The Garrett Corporation | Torque limiting clutch |
DE3222674C2 (de) | 1982-06-16 | 1984-04-05 | MTU Motoren- und Turbinen-Union München GmbH, 8000 München | Einrichtung zum Verstellen von Schubumkehrern |
US4458582A (en) * | 1982-10-18 | 1984-07-10 | Sundstrand Corporation | Automatic rigging arrangement for actuation systems |
US4579039A (en) | 1983-12-12 | 1986-04-01 | Sundstrand Corporation | Power drive unit |
JPS61502882A (ja) | 1984-08-01 | 1986-12-11 | サンドストランド・コ−ポレ−ション | 多段機関飛行機に対するスラスト操作装置 |
US4898265A (en) | 1988-01-27 | 1990-02-06 | Sundstrand Corporation | Torque limiter |
GB9106515D0 (en) * | 1991-03-27 | 1991-05-22 | Lucas Ind Plc | Device for operation of a gas turbine engine thrust reverser system |
EP0536954B1 (en) | 1991-10-10 | 1996-01-24 | Lucas Industries Public Limited Company | A lock for a thrust reverser mechanism, a thrust reverser mechanism, and a thrust reverser |
US5609020A (en) | 1995-05-15 | 1997-03-11 | The Boeing Company | Thrust reverser synchronization shaft lock |
US5769362A (en) | 1996-05-01 | 1998-06-23 | Safe Flight Instrument Corporation | Aircraft control mechanism for a speed brake |
FR2760047B1 (fr) | 1997-02-27 | 1999-05-07 | Hispano Suiza Sa | Inverseur de poussee de turboreacteur a portes associees a un dispositif de synchronisation de commande |
US6598386B2 (en) | 2001-10-16 | 2003-07-29 | Honeywell International, Inc. | Jet engine thrust reverser system having torque limited synchronization |
-
2001
- 2001-10-16 US US09/981,011 patent/US6598386B2/en not_active Expired - Fee Related
-
2002
- 2002-10-16 CA CA002463817A patent/CA2463817A1/en not_active Abandoned
- 2002-10-16 JP JP2003536604A patent/JP2005506483A/ja active Pending
- 2002-10-16 WO PCT/US2002/032965 patent/WO2003033898A1/en active Application Filing
- 2002-10-16 EP EP02801737A patent/EP1436497A1/en not_active Withdrawn
- 2002-10-16 BR BRPI0213349-0A patent/BR0213349A/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2463817A1 (en) | 2003-04-24 |
US20030070416A1 (en) | 2003-04-17 |
US6598386B2 (en) | 2003-07-29 |
JP2005506483A (ja) | 2005-03-03 |
WO2003033898A1 (en) | 2003-04-24 |
EP1436497A1 (en) | 2004-07-14 |
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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 6A E 7A ANUIDADES |
|
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 2060 DE 29/06/2010. |