ATE307281T1 - Systeme et methode de determination de la position d'un inverseur de poussee - Google Patents

Systeme et methode de determination de la position d'un inverseur de poussee

Info

Publication number
ATE307281T1
ATE307281T1 AT02750263T AT02750263T ATE307281T1 AT E307281 T1 ATE307281 T1 AT E307281T1 AT 02750263 T AT02750263 T AT 02750263T AT 02750263 T AT02750263 T AT 02750263T AT E307281 T1 ATE307281 T1 AT E307281T1
Authority
AT
Austria
Prior art keywords
motor
thrust reverser
rotational position
poussee
inverseur
Prior art date
Application number
AT02750263T
Other languages
English (en)
Inventor
Andrew T Johnson
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
Application granted granted Critical
Publication of ATE307281T1 publication Critical patent/ATE307281T1/de

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
    • F02K1/64—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
    • F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2200/00—Mathematical features
    • F05B2200/10—Basic functions
    • F05B2200/11—Sum
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2270/00—Control
    • F05B2270/10—Purpose of the control system
    • F05B2270/103—Purpose of the control system to affect the output of the engine
    • F05B2270/1031—Thrust
    • 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
    • F05D2200/00—Mathematical features
    • F05D2200/10—Basic functions
    • F05D2200/11—Sum
    • 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
    • F05D2270/05—Purpose of the control system to affect the output of the engine
    • F05D2270/051—Thrust
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/62—Electrical actuators
    • 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
    • F05D2270/60—Control system actuates means
    • F05D2270/66—Mechanical actuators
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Position Or Direction (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Multiple Motors (AREA)
  • Control Of Fluid Gearings (AREA)
  • Control Of Transmission Device (AREA)
  • Paper (AREA)
  • Nonmetallic Welding Materials (AREA)
  • Control Of Electric Motors In General (AREA)
AT02750263T 2001-07-24 2002-07-23 Systeme et methode de determination de la position d'un inverseur de poussee ATE307281T1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US30752701P 2001-07-24 2001-07-24
US10/199,020 US6681559B2 (en) 2001-07-24 2002-07-19 Thrust reverser position determination system and method
PCT/US2002/023431 WO2003010430A1 (en) 2001-07-24 2002-07-23 Thrust reverser position determination system and method

Publications (1)

Publication Number Publication Date
ATE307281T1 true ATE307281T1 (de) 2005-11-15

Family

ID=23190137

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02750263T ATE307281T1 (de) 2001-07-24 2002-07-23 Systeme et methode de determination de la position d'un inverseur de poussee

Country Status (8)

Country Link
US (1) US6681559B2 (de)
EP (1) EP1409866B1 (de)
JP (1) JP2005522610A (de)
AT (1) ATE307281T1 (de)
BR (1) BR0211465A (de)
CA (1) CA2455554A1 (de)
DE (1) DE60206768T2 (de)
WO (1) WO2003010430A1 (de)

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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
FR2872223B1 (fr) * 2004-06-29 2006-08-25 Hurel Hispano Sa Procede de commande pour l'actionnement d'un inverseur de poussee
US7946106B2 (en) * 2004-06-29 2011-05-24 Aircelle Device for actuating mobile cowls equipping a thrust reverser
US7409820B2 (en) * 2004-11-16 2008-08-12 Honeywell International Inc. Electrical thrust reverser tertiary lock system including a voltage limiting circuit
FR2887301B1 (fr) * 2005-06-16 2007-08-31 Aircelle Sa Systeme de commande electronique pour nacelle
WO2007057524A1 (fr) * 2005-11-21 2007-05-24 Aircelle Procede de commande pour l’actionnement d’un inverseur de poussee
US7525266B2 (en) * 2006-01-30 2009-04-28 Honeywell International Inc. Inverter loop latch with integrated AC detection reset
WO2008045072A1 (en) 2006-10-12 2008-04-17 United Technologies Corporation Dual function cascade integrated variable area fan nozzle and thrust reverser
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
EP2578864B1 (de) * 2007-08-08 2014-09-24 Rohr, Inc. Veränderliche Gebläsedüse mit Bypass-Strom
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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
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
FR2922958B1 (fr) * 2007-10-25 2009-11-20 Aircelle Sa Inverseur de poussee a grilles
FR2927310B1 (fr) * 2008-02-13 2010-07-30 Aircelle Sa Systeme de commande pour nacelle de turboreacteur
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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.
US10378479B2 (en) * 2015-10-19 2019-08-13 General Electric Company Variable effective area fan nozzle
US10415504B2 (en) 2016-02-09 2019-09-17 Honeywell International Inc. Translating cowl thrust reverser system with over-stow unlocking capability
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Also Published As

Publication number Publication date
US6681559B2 (en) 2004-01-27
JP2005522610A (ja) 2005-07-28
EP1409866A1 (de) 2004-04-21
DE60206768T2 (de) 2006-06-29
US20030019206A1 (en) 2003-01-30
WO2003010430A1 (en) 2003-02-06
DE60206768D1 (de) 2005-11-24
CA2455554A1 (en) 2003-02-06
EP1409866B1 (de) 2005-10-19
BR0211465A (pt) 2004-11-09

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