BR0210433A - Sistema para controlar o movimento de um reversor de empuxo, método de sustentação da energia elétrica na uma ou mais linhas de suprimento durante uma interrupção momentânea da energia elétrica proveniente da fonte de energia, método de sustentação da energia elétrica durante uma interrupção momentânea de energia em um sistema de atuação do reversor de empuxo - Google Patents
Sistema para controlar o movimento de um reversor de empuxo, método de sustentação da energia elétrica na uma ou mais linhas de suprimento durante uma interrupção momentânea da energia elétrica proveniente da fonte de energia, método de sustentação da energia elétrica durante uma interrupção momentânea de energia em um sistema de atuação do reversor de empuxoInfo
- Publication number
- BR0210433A BR0210433A BR0210433-4A BR0210433A BR0210433A BR 0210433 A BR0210433 A BR 0210433A BR 0210433 A BR0210433 A BR 0210433A BR 0210433 A BR0210433 A BR 0210433A
- Authority
- BR
- Brazil
- Prior art keywords
- electricity
- power
- thrust reverser
- during
- momentary interruption
- 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
- F02K1/76—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Control Of Multiple Motors (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
Abstract
"SISTEMA PARA CONTROLAR O MOVIMENTO DE UM REVERSOR DE EMPUXO, MéTODO DE SUSTENTAçãO DA ENERGIA ELéTRICA NA UMA OU MAIS LINHAS DE SUPRIMENTO DURANTE UMA INTERRUPçãO MOMENTâNEA DA ENERGIA ELéTRICA PROVENIENTE DA FONTE DE ENERGIA, MéTODO DE SUSTENTAçãO DA ENERGIA ELéTRICA DURANTE UMA INTERRUPçãO MOMENTâNEA DE ENERGIA EM UM SISTEMA DE ATUAçãO DO REVERSOR DE EMPUXO". Um sistema elétrico de atuação do reversor de empuxo inclui um motor elétrico que é controlado para operar tanto em um modo motorização e em um modo geração. Durante as operações normais do sistema de atuação, o motor elétrico é controlado para operar em modo motorização para movimentar um ou mais dos componentes movediços do reversor de empuxo. Durante um evento de interrupção de energia, no qual a fonte de energia primária do motor é perdida, o motor é controlado para operar em modo geração. A energia elétrica gerada pelo motor durante sua operação em modo geração mantém os mecanismos de travamento do sistema reversor de empuxo em uma condição energizada, destravada.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/882,905 US6439504B1 (en) | 2001-06-15 | 2001-06-15 | System and method for sustaining electric power during a momentary power interruption in an electric thrust reverser actuation system |
PCT/US2002/018796 WO2002103189A1 (en) | 2001-06-15 | 2002-06-14 | System and method for sustaining electic power during a momentary power interruption in an electric thrust reverser actuation system |
Publications (1)
Publication Number | Publication Date |
---|---|
BR0210433A true BR0210433A (pt) | 2004-08-03 |
Family
ID=25381580
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR0210433-4A BR0210433A (pt) | 2001-06-15 | 2002-06-14 | Sistema para controlar o movimento de um reversor de empuxo, método de sustentação da energia elétrica na uma ou mais linhas de suprimento durante uma interrupção momentânea da energia elétrica proveniente da fonte de energia, método de sustentação da energia elétrica durante uma interrupção momentânea de energia em um sistema de atuação do reversor de empuxo |
Country Status (5)
Country | Link |
---|---|
US (1) | US6439504B1 (pt) |
EP (1) | EP1395741A1 (pt) |
JP (1) | JP2004532950A (pt) |
BR (1) | BR0210433A (pt) |
WO (1) | WO2002103189A1 (pt) |
Families Citing this family (42)
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FR2846375B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromacanique pour turboreacteur a asservissement du deplacement des portes |
FR2846378B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a synchronisation des dispositifs de verrouillage |
FR2846377B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position |
US7409820B2 (en) | 2004-11-16 | 2008-08-12 | Honeywell International Inc. | Electrical thrust reverser tertiary lock system including a voltage limiting circuit |
US7484356B1 (en) * | 2005-07-26 | 2009-02-03 | Aeronautical Concepts Of Exhaust, Llc | Cascade reverser without blocker doors |
US7456594B2 (en) | 2006-06-09 | 2008-11-25 | Honeywell International Inc. | Electric motor brake engagement holdup system |
US8151551B2 (en) * | 2006-10-12 | 2012-04-10 | United Technologies Corporation | Variable area fan nozzle thrust reverser |
FR2912470B1 (fr) * | 2007-02-14 | 2009-03-20 | Aircelle Sa | Procede de controle des moteurs electriques d'un inverseur de poussee |
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 |
FR2920142B1 (fr) * | 2007-08-20 | 2009-09-18 | Aircelle Sa | Dispositif et procede de commande de l'alimentation d'au moins un actionneur de maintenance d'un aeronef |
FR2922959B1 (fr) * | 2007-10-31 | 2009-12-04 | Airbus France | Systeme de controle et procede de controle. |
FR2927310B1 (fr) * | 2008-02-13 | 2010-07-30 | Aircelle Sa | Systeme de commande pour nacelle de turboreacteur |
FR2932226B1 (fr) * | 2008-06-06 | 2013-08-23 | Aircelle Sa | Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee |
FR2944509B1 (fr) * | 2009-04-16 | 2012-10-19 | Aircelle Sa | Systeme d'actionnement pour nacelle de turboreacteur |
FR2944564B1 (fr) * | 2009-04-16 | 2011-04-22 | Aircelle Sa | Systeme de controle pour nacelle de turboreacteur |
FR2944563B1 (fr) * | 2009-04-16 | 2011-04-22 | Aircelle Sa | Dispositif d'inversion de poussee |
FR2946395B1 (fr) * | 2009-06-04 | 2016-03-04 | Airbus France | Procede pour la detection de l'ouverture d'un inverseur de poussee de turboreacteur d'aeronef |
FR2958689B1 (fr) * | 2010-04-12 | 2012-04-20 | Aircelle Sa | Systeme de commande d'un dispositif electrique d'une nacelle |
US8875486B2 (en) | 2010-05-17 | 2014-11-04 | Rohr, Inc. | Guide system for nacelle assembly |
US8511973B2 (en) | 2010-06-23 | 2013-08-20 | Rohr, Inc. | Guide system for nacelle assembly |
WO2013024512A1 (en) * | 2011-08-18 | 2013-02-21 | Hitachi, Ltd. | Storage apparatus with redundant power supply |
FR3005489B1 (fr) | 2013-05-07 | 2017-03-17 | Airbus Operations Sas | Dispositif de commande d'une tuyere a section variable d'un aeronef |
FR3005488B1 (fr) * | 2013-05-07 | 2015-05-29 | Airbus Operations Sas | Dispositif de commande d'une tuyere a section variable d'un aeronef |
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 |
FR3010387B1 (fr) * | 2013-09-10 | 2015-10-09 | Airbus Operations Sas | Aeronef comprenant un dispositif de commande d'une tuyere a section variable alimente par deux alimentations electriques independantes |
US10487690B2 (en) * | 2014-08-18 | 2019-11-26 | Rohr, Inc. | Actively controlled cooling air exhaust door on an aircraft engine nacelle |
FR3021300A1 (fr) * | 2014-10-20 | 2015-11-27 | Aircelle Sa | Systeme d’actionnement pour inverseur de poussee |
DE102015206985A1 (de) * | 2015-04-17 | 2016-10-20 | Rolls-Royce Deutschland Ltd & Co Kg | Triebwerksverkleidung einer Fluggasturbine |
FR3045013B1 (fr) * | 2015-12-14 | 2019-05-17 | Safran Nacelles | Systeme de commande hydraulique d’un inverseur de poussee comprenant un module de concentration des donnees |
EP3193003A1 (en) * | 2016-01-15 | 2017-07-19 | Goodrich Actuation Systems Ltd. | Thrust reverser actuation system architecture |
US10598047B2 (en) * | 2016-02-29 | 2020-03-24 | United Technologies Corporation | Low-power bowed rotor prevention system |
US10787933B2 (en) | 2016-06-20 | 2020-09-29 | Raytheon Technologies Corporation | Low-power bowed rotor prevention and monitoring system |
US10479223B2 (en) | 2018-01-25 | 2019-11-19 | H55 Sa | Construction and operation of electric or hybrid aircraft |
US11063323B2 (en) | 2019-01-23 | 2021-07-13 | H55 Sa | Battery module for electrically-driven aircraft |
US11065979B1 (en) | 2017-04-05 | 2021-07-20 | H55 Sa | Aircraft monitoring system and method for electric or hybrid aircrafts |
US11148819B2 (en) | 2019-01-23 | 2021-10-19 | H55 Sa | Battery module for electrically-driven aircraft |
US10854866B2 (en) | 2019-04-08 | 2020-12-01 | H55 Sa | Power supply storage and fire management in electrically-driven aircraft |
US11114705B2 (en) * | 2018-11-21 | 2021-09-07 | Honeywell International Inc. | Current measurement and voltage control approach |
RU2744587C1 (ru) * | 2020-06-03 | 2021-03-11 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Отказобезопасная электромеханическая система управления реверсивным устройством газотурбинного двигателя |
US11814187B2 (en) | 2020-12-21 | 2023-11-14 | General Electric Company | Hybrid electric propulsor equipped with a hydraulic coupling |
EP4177456A1 (en) * | 2021-11-04 | 2023-05-10 | Goodrich Actuation Systems Limited | Back-up thrust reverser actuation system control |
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-
2001
- 2001-06-15 US US09/882,905 patent/US6439504B1/en not_active Expired - Fee Related
-
2002
- 2002-06-14 EP EP02744328A patent/EP1395741A1/en not_active Withdrawn
- 2002-06-14 JP JP2003505476A patent/JP2004532950A/ja not_active Ceased
- 2002-06-14 WO PCT/US2002/018796 patent/WO2002103189A1/en active Application Filing
- 2002-06-14 BR BR0210433-4A patent/BR0210433A/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
JP2004532950A (ja) | 2004-10-28 |
US6439504B1 (en) | 2002-08-27 |
EP1395741A1 (en) | 2004-03-10 |
WO2002103189A1 (en) | 2002-12-27 |
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Legal Events
Date | Code | Title | Description |
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B08F | Application fees: application dismissed [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 7A E 8A ANUIDADE(S). |
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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 2082 DE 30/11/2010. |