JP2004532950A - 電気的な逆推進器作動装置において一時的な停電中に電力を持続させる装置及び方法 - Google Patents
電気的な逆推進器作動装置において一時的な停電中に電力を持続させる装置及び方法 Download PDFInfo
- Publication number
- JP2004532950A JP2004532950A JP2003505476A JP2003505476A JP2004532950A JP 2004532950 A JP2004532950 A JP 2004532950A JP 2003505476 A JP2003505476 A JP 2003505476A JP 2003505476 A JP2003505476 A JP 2003505476A JP 2004532950 A JP2004532950 A JP 2004532950A
- Authority
- JP
- Japan
- Prior art keywords
- power
- electric motor
- mode
- supply lines
- coupled
- Prior art date
- Legal status (The legal status 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 status listed.)
- Ceased
Links
Images
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)
- Electric Propulsion And Braking For Vehicles (AREA)
- Control Of Motors That Do Not Use Commutators (AREA)
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 (2)
| Publication Number | Publication Date |
|---|---|
| JP2004532950A true JP2004532950A (ja) | 2004-10-28 |
| JP2004532950A5 JP2004532950A5 (https=) | 2005-11-17 |
Family
ID=25381580
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2003505476A Ceased JP2004532950A (ja) | 2001-06-15 | 2002-06-14 | 電気的な逆推進器作動装置において一時的な停電中に電力を持続させる装置及び方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US6439504B1 (https=) |
| EP (1) | EP1395741A1 (https=) |
| JP (1) | JP2004532950A (https=) |
| BR (1) | BR0210433A (https=) |
| WO (1) | WO2002103189A1 (https=) |
Families Citing this family (46)
| 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 |
| FR2846377B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a controle permanent de position |
| FR2846378B1 (fr) * | 2002-10-25 | 2006-06-30 | Hispano Suiza Sa | Inverseur de poussee electromecanique pour turboreacteur a synchronisation des dispositifs de verrouillage |
| FR2846376B1 (fr) * | 2002-10-25 | 2005-01-28 | Hispano Suiza Sa | Platine de maintenance et d'inhibition pour inverseur de poussee |
| 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 |
| WO2008045070A1 (en) | 2006-10-12 | 2008-04-17 | 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 |
| RU2367811C2 (ru) * | 2007-07-30 | 2009-09-20 | Алексей Александрович Комов | Способ регулирования величины обратной тяги газотурбинных двигателей на пробеге четырехдвигательного самолета при использовании реверса тяги двух внутренних двигателей |
| WO2009029401A2 (en) | 2007-08-08 | 2009-03-05 | Rohr, Inc. | Variable area fan nozzle with bypass flow |
| 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 |
| EP3211184B1 (en) * | 2016-02-29 | 2021-05-05 | Raytheon Technologies Corporation | Bowed rotor prevention system and associated method of bowed rotor prevention |
| US10787933B2 (en) | 2016-06-20 | 2020-09-29 | Raytheon Technologies Corporation | Low-power bowed rotor prevention and monitoring system |
| US11148819B2 (en) | 2019-01-23 | 2021-10-19 | H55 Sa | Battery module for electrically-driven aircraft |
| US10322824B1 (en) | 2018-01-25 | 2019-06-18 | 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 |
| US12409756B2 (en) | 2017-04-05 | 2025-09-09 | H55 Sa | Aircraft monitoring system and method for electric or hybrid aircrafts |
| US11065979B1 (en) | 2017-04-05 | 2021-07-20 | H55 Sa | Aircraft monitoring system and method for electric or hybrid aircrafts |
| 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 |
| EP4177456B1 (en) * | 2021-11-04 | 2025-01-15 | Goodrich Actuation Systems Limited | Back-up thrust reverser actuation system control |
| EP4554037A1 (en) * | 2023-11-08 | 2025-05-14 | Hamilton Sundstrand Corporation | Aircraft power system |
Family Cites Families (62)
| 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 |
| WO1994007018A1 (en) | 1992-09-21 | 1994-03-31 | 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 |
| US5550444A (en) * | 1992-12-10 | 1996-08-27 | Twix Equipment Ag | Device and process for the reversible storage of electric energy by its reversible conversion to kinetic energy |
| 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 |
| GB9825651D0 (en) | 1998-11-23 | 1999-01-13 | Lucas Ind Plc | Actuator |
| US6307339B1 (en) | 1998-11-23 | 2001-10-23 | Western-Cullen-Hayes, Inc. | Bi-directionally dynamically braked gate crossing mechanism controller |
| US6211665B1 (en) | 1999-04-13 | 2001-04-03 | Alliedsignal Inc. | Solenoid motion detection circuit |
-
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 BR BR0210433-4A patent/BR0210433A/pt not_active IP Right Cessation
- 2002-06-14 WO PCT/US2002/018796 patent/WO2002103189A1/en not_active Ceased
- 2002-06-14 JP JP2003505476A patent/JP2004532950A/ja not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| BR0210433A (pt) | 2004-08-03 |
| EP1395741A1 (en) | 2004-03-10 |
| WO2002103189A1 (en) | 2002-12-27 |
| US6439504B1 (en) | 2002-08-27 |
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| A01 | Written decision to grant a patent or to grant a registration (utility model) |
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