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 empuxo

Info

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
Application number
BR0210433-4A
Other languages
English (en)
Inventor
Terry J Ahrendt
Original Assignee
Honeywell Int Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Honeywell Int Inc filed Critical Honeywell Int Inc
Publication of BR0210433A publication Critical patent/BR0210433A/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54Nozzles having means for reversing jet thrust
    • F02K1/76Control or regulation of thrust reversers
    • F02K1/763Control 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.
BR0210433-4A 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 BR0210433A (pt)

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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6655125B2 (en) * 2001-12-05 2003-12-02 Honeywell International Inc. System architecture for electromechanical thrust reverser actuation systems
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

Family Cites Families (62)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1175346A (en) 1912-07-17 1916-03-14 Westinghouse Electric & Mfg Co Control system for electric motors.
US2912632A (en) 1957-08-23 1959-11-10 Ite Circuit Breaker Ltd Motor reversing and dynamic braking circuit
US3514952A (en) 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine
US3515361A (en) 1966-09-12 1970-06-02 Albert W Blackburn Control of aircraft by deflection of propulsion gases
US3621763A (en) 1969-07-17 1971-11-23 Pneumo Dynamics Corp Fan thrust reverser actuator
US3618880A (en) 1970-05-11 1971-11-09 Boeing Co Speed brake system for aircraft spoilers
US3815357A (en) 1971-01-28 1974-06-11 Rohr Industries Inc Thrust reversing apparatus
GB1350084A (en) 1971-02-18 1974-04-18 Rank Organisation Ltd Servomechanisms
US3714535A (en) 1971-06-25 1973-01-30 Bendix Corp Servo displacement limiter with reversing capabilities
US3936226A (en) 1974-06-07 1976-02-03 United Technologies Corporation Control system for variable pitch fan propulsor with reverse pitch
US3932058A (en) 1974-06-07 1976-01-13 United Technologies Corporation Control system for variable pitch fan propulsor
US4005822A (en) 1975-12-22 1977-02-01 Rohr Industries, Inc. Fan duct thrust reverser
GB1534583A (en) 1976-06-08 1978-12-06 Short Bros Ltd Reversal of thrust in gas turbine engines
DE2716411C3 (de) 1977-04-13 1981-11-12 Siemens AG, 1000 Berlin und 8000 München Anordnung zur Erzeugung von Drehbewegungen um einen vorgebbaren Winkel mit Hilfe eines Gleichstrommotors
US4191094A (en) 1978-04-26 1980-03-04 Sundstrand Corporation Power drive unit
FR2435604A1 (fr) 1978-07-25 1980-04-04 Snecma Dispositif de commande hydraulique d'inversion de poussee pour moteur a reaction
US4284930A (en) 1979-10-19 1981-08-18 Westinghouse Electric Corp. Motor control apparatus and method
US4458863A (en) 1980-03-10 1984-07-10 The Boeing Company Strut supported inlet
GB2075447B (en) 1980-04-30 1983-10-26 Rolls Royce Thrust deflectors for gas turbine engines
US4383647A (en) 1980-08-22 1983-05-17 The Bendix Corporation Integrated hydraulic control circuit for jet engine thrust reverser and variable exhaust nozzle
FR2488335B1 (fr) 1980-08-11 1986-01-31 Snecma Dispositif detecteur de position d'un inverseur de poussee de turboreacteur et de son verrouillage
FR2500537B1 (fr) 1981-02-24 1985-07-05 Astech Dispositif de securite pour inverseur de poussee associe a un moteur a reaction d'aeronef
US4442928A (en) 1981-10-02 1984-04-17 The Bendix Corporation Actuator
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
US4546783A (en) 1983-05-02 1985-10-15 Flo Trend Shares, Inc. Apparatus for washing drill cuttings
US4788531A (en) 1983-11-17 1988-11-29 The Boeing Company Automatic fault reporting system
GB2154291B (en) 1984-02-14 1987-08-12 Rolls Royce Anti rotation device
DE3431583A1 (de) 1984-08-28 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur automatischen beseitigung von steuerkraftfehlern bei luftfahrzeugen, insbesondere hubschraubern
US4585189A (en) 1984-10-22 1986-04-29 Lockheed Corporation Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
US4656407A (en) 1985-06-14 1987-04-07 A.R.A. Manufacturing Company Of Delware, Inc. Electric motor servo control system and method
US4651621A (en) 1986-03-20 1987-03-24 Allied Corporation Control system for an air motor
US4827248A (en) 1987-06-30 1989-05-02 The Boeing Company Proximity sensor with automatic gap control
US5243817A (en) 1990-07-05 1993-09-14 Rohr, Inc. Thrust reverser for fan jet aircraft engines
GB9015373D0 (en) 1990-07-12 1990-08-29 Rolls Royce Plc Gas turbine engine thrust reverser control
US5213286A (en) 1990-10-10 1993-05-25 General Electric Company Door for aircraft nacelle
US5282719A (en) 1991-05-13 1994-02-01 Alliedsignal Inc. Quad mode fan pitch actuation system for a gas turbine engine
FR2679605A1 (fr) 1991-07-24 1993-01-29 Snecma Inverseur de poussee de turboreacteur muni d'un dispositif de securite integre au systeme de commande hydraulique.
US5313788A (en) 1991-08-07 1994-05-24 General Electric Company Thrust reversing arrangement for a long duct mixed flow exhaust turbofan engine
EP0664852B1 (en) 1992-09-21 1996-08-14 The Boeing Company Mechanical lock for jet engine thrust reverser
US5267436A (en) 1992-09-28 1993-12-07 United Technologies Corporation Vectoring nozzle control of gas turbine engines
JPH07504318A (ja) * 1992-12-10 1995-05-11 ツヴィックス エクィップメント アーゲー 電気エネルギーの可逆変換によってそれを可逆的に蓄積するための装置及び方法
US5327055A (en) 1993-03-08 1994-07-05 International Business Machines Corporation Mechanical brake hold circuit for an electric motor
FR2711733B1 (fr) 1993-10-22 1996-01-26 Hurel Dubois Avions Inverseur de poussée à portes pour moteur d'avion à réaction équipées d'un volet auxiliaire.
US6121740A (en) 1994-06-27 2000-09-19 Ford Global Technologies, Inc. Control of regeneration energy from an electric motor
FR2722534B1 (fr) 1994-07-13 1996-08-14 Hispano Suiza Sa Inverseur de poussee de turboreacteur double flux, a obstacles externes
US5826823A (en) 1996-02-07 1998-10-27 Rohr, Inc. Actuator and safety lock system for pivoting door thrust reverser for aircraft jet engine
US5798458A (en) 1996-10-11 1998-08-25 Raytheon Ti Systems, Inc. Acoustic catastrophic event detection and data capture and retrieval system for aircraft
FR2755730B1 (fr) 1996-11-14 1999-01-08 Hispano Suiza Sa Systeme de commande electrique pour inverseur de poussee de turboreacteur
US5813218A (en) 1996-11-26 1998-09-29 Rooke Corp. Thrust reverser door lock vent and method
FR2756868B1 (fr) 1996-12-05 1999-01-08 Hispano Suiza Sa Inverseur de poussee de turboreacteur a portes maintenues dans les lignes de nacelle
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
FR2762875B1 (fr) 1997-04-30 1999-06-04 Hispano Suiza Sa Inverseur de poussee protege en cas de deverrouillage accidentel
US6034492A (en) 1997-04-30 2000-03-07 Nec Corporation Motor-generator
FR2764643B1 (fr) 1997-06-12 1999-07-16 Hispano Suiza Sa Inverseur de poussee a portes de turboreacteur a section variable d'ejection
US6021636A (en) 1997-07-25 2000-02-08 Alliedsignal Inc. Lightweight tertiary thrust reverser lock assembly with a blocking member
US6042053A (en) 1997-10-31 2000-03-28 The Boeing Company Automatic restow system for aircraft thrust reverser
US6178867B1 (en) 1998-08-26 2001-01-30 Alliedsignal Inc. Synchronized travel of independent actuators
US6240246B1 (en) 1998-10-30 2001-05-29 Alliedsignal, Inc. Anti-resonance mixing filter
US6307339B1 (en) 1998-11-23 2001-10-23 Western-Cullen-Hayes, Inc. Bi-directionally dynamically braked gate crossing mechanism controller
GB9825651D0 (en) 1998-11-23 1999-01-13 Lucas Ind Plc Actuator
US6211665B1 (en) 1999-04-13 2001-04-03 Alliedsignal Inc. Solenoid motion detection circuit

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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