ATE381668T1 - Kontrollvorrichtung für die betätigung von schubumkehrvorrichtungen an strahltriebwerken - Google Patents
Kontrollvorrichtung für die betätigung von schubumkehrvorrichtungen an strahltriebwerkenInfo
- Publication number
- ATE381668T1 ATE381668T1 AT02731602T AT02731602T ATE381668T1 AT E381668 T1 ATE381668 T1 AT E381668T1 AT 02731602 T AT02731602 T AT 02731602T AT 02731602 T AT02731602 T AT 02731602T AT E381668 T1 ATE381668 T1 AT E381668T1
- Authority
- AT
- Austria
- Prior art keywords
- motor
- thrust reverser
- rotational speed
- control device
- jet engine
- 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)
- Retarders (AREA)
- Control Of Electric Motors In General (AREA)
- Control Of Multiple Motors (AREA)
- Transmission Devices (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Exhaust-Gas Circulating Devices (AREA)
- Plasma Technology (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/846,914 US6519929B2 (en) | 2001-04-30 | 2001-04-30 | System and method for controlling the deployment of jet engine thrust reversers |
Publications (1)
Publication Number | Publication Date |
---|---|
ATE381668T1 true ATE381668T1 (de) | 2008-01-15 |
Family
ID=25299293
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
AT02731602T ATE381668T1 (de) | 2001-04-30 | 2002-04-30 | Kontrollvorrichtung für die betätigung von schubumkehrvorrichtungen an strahltriebwerken |
Country Status (5)
Country | Link |
---|---|
US (2) | US6519929B2 (de) |
EP (1) | EP1386072B1 (de) |
AT (1) | ATE381668T1 (de) |
DE (1) | DE60224175T2 (de) |
WO (1) | WO2002088540A1 (de) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6961369B1 (en) | 1999-11-09 | 2005-11-01 | Aware, Inc. | System and method for scrambling the phase of the carriers in a multicarrier communications system |
US6681559B2 (en) * | 2001-07-24 | 2004-01-27 | Honeywell International, Inc. | Thrust reverser position determination system and method |
US6655125B2 (en) * | 2001-12-05 | 2003-12-02 | Honeywell International Inc. | System architecture for electromechanical thrust reverser actuation systems |
US6935097B2 (en) * | 2003-04-17 | 2005-08-30 | Honeywell International, Inc. | Lock assembly that inhibits thrust reverser movement at or near the stowed position |
US6974107B2 (en) * | 2003-06-18 | 2005-12-13 | Honeywell International, Inc. | Thrust reverser system actuator having an integral torque limiter |
US7946106B2 (en) * | 2004-06-29 | 2011-05-24 | Aircelle | Device for actuating mobile cowls equipping a thrust reverser |
FR2872222B1 (fr) * | 2004-06-29 | 2006-08-25 | Hurel Hispano Sa | Procede d'ouverture d'un capot mobile equipant un inverseur de poussee |
FR2872223B1 (fr) * | 2004-06-29 | 2006-08-25 | Hurel Hispano Sa | Procede de commande pour l'actionnement d'un inverseur de poussee |
FR2887301B1 (fr) * | 2005-06-16 | 2007-08-31 | Aircelle Sa | Systeme de commande electronique pour nacelle |
US7513101B2 (en) * | 2005-10-28 | 2009-04-07 | Honeywell International Inc. | Synchronized motor thrust reverser actuation system |
BRPI0520744A2 (pt) * | 2005-11-21 | 2009-05-26 | Aircelle Sa | processo de comando para a abertura ou o fechamento de um reversor de empuxo de turborreator e reversor de empuxo |
US20070237575A1 (en) * | 2006-04-11 | 2007-10-11 | Honeywell International, Inc. | Flexible shaft inline coupler |
FR2912470B1 (fr) * | 2007-02-14 | 2009-03-20 | Aircelle Sa | Procede de controle des moteurs electriques d'un inverseur de poussee |
FR2913067B1 (fr) * | 2007-02-28 | 2011-05-13 | Aircelle Sa | Procede d'autocalibration pour verins electriques de nacelle de turboreacteur |
GB0706524D0 (en) * | 2007-04-04 | 2007-05-09 | Goodrich Actuation Systems Ltd | Actuator arrangement |
FR2920200B1 (fr) * | 2007-08-20 | 2013-10-04 | Aircelle Sa | Procede et systeme de commande d'au moins un actionneur de capots d'un inverseur de poussee pour turboreacteur |
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 |
FR2922959B1 (fr) * | 2007-10-31 | 2009-12-04 | Airbus France | Systeme de controle et procede de controle. |
FR2932226B1 (fr) * | 2008-06-06 | 2013-08-23 | Aircelle Sa | Procede de synchronisation des actionneurs d'un capot mobile d'inverseur de poussee |
US8170771B2 (en) * | 2008-06-30 | 2012-05-01 | Honeywell International Inc. | Fluid-powered thrust reverser actuation system speed control |
FR2944563B1 (fr) * | 2009-04-16 | 2011-04-22 | Aircelle Sa | Dispositif d'inversion de poussee |
FR2958689B1 (fr) | 2010-04-12 | 2012-04-20 | Aircelle Sa | Systeme de commande d'un dispositif electrique d'une nacelle |
US9086035B2 (en) * | 2012-01-20 | 2015-07-21 | Hamilton Sundstrand Corporation | Integrated thrust reverser actuator and variable area fan nozzle actuator |
US9188081B2 (en) | 2012-04-10 | 2015-11-17 | Honeywell International Inc. | Thrust reverser actuator with primary lock |
US9482180B2 (en) * | 2012-05-24 | 2016-11-01 | The Boeing Company | Thrust reverser system |
FR2999240B1 (fr) * | 2012-12-11 | 2015-01-02 | Aircelle Sa | Systeme de synchronisation pour dispositif d'inversion de poussee |
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 |
FR3016191B1 (fr) * | 2014-01-08 | 2019-07-05 | Safran Aircraft Engines | Procede et programme d'ordinateur pour la surveillance d'un inverseur de poussee a actionneurs hydrauliques |
US11597508B2 (en) | 2021-05-13 | 2023-03-07 | Beta Air, Llc | Aircraft having reverse thrust capabilities |
Family Cites Families (66)
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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 |
GB1334518A (en) * | 1971-01-14 | 1973-10-17 | Rotax Ltd | Actuating systems of thrust reversal buckets for a gas turbine engine |
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 |
US3719324A (en) * | 1971-06-04 | 1973-03-06 | Gen Electric | Velocity sensor feedback mechanism for thrust reverser actuating system |
US3696895A (en) * | 1971-06-24 | 1972-10-10 | Garrett Corp | Fluidic control for motor and brake |
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 |
US4391409A (en) * | 1980-09-30 | 1983-07-05 | The Boeing Company | Positioning and control system for fan thrust reverser cowls in a turbofan engine |
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 |
US4458582A (en) * | 1982-10-18 | 1984-07-10 | Sundstrand Corporation | Automatic rigging arrangement for actuation systems |
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 |
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US5243817A (en) | 1990-07-05 | 1993-09-14 | Rohr, Inc. | Thrust reverser for fan jet aircraft engines |
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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 |
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 |
US6034492A (en) | 1997-04-30 | 2000-03-07 | Nec Corporation | Motor-generator |
FR2762875B1 (fr) | 1997-04-30 | 1999-06-04 | Hispano Suiza Sa | Inverseur de poussee protege en cas de deverrouillage accidentel |
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
- 2001-04-30 US US09/846,914 patent/US6519929B2/en not_active Expired - Fee Related
-
2002
- 2002-04-30 AT AT02731602T patent/ATE381668T1/de not_active IP Right Cessation
- 2002-04-30 DE DE60224175T patent/DE60224175T2/de not_active Expired - Fee Related
- 2002-04-30 WO PCT/US2002/013745 patent/WO2002088540A1/en active IP Right Grant
- 2002-04-30 EP EP02731602A patent/EP1386072B1/de not_active Expired - Lifetime
- 2002-11-04 US US10/287,297 patent/US6564541B2/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6519929B2 (en) | 2003-02-18 |
EP1386072A1 (de) | 2004-02-04 |
US20020157376A1 (en) | 2002-10-31 |
DE60224175D1 (de) | 2008-01-31 |
WO2002088540A1 (en) | 2002-11-07 |
US20030066283A1 (en) | 2003-04-10 |
DE60224175T2 (de) | 2008-12-04 |
EP1386072B1 (de) | 2007-12-19 |
US6564541B2 (en) | 2003-05-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |