DE69703644T2 - Einrichtung zur Regelung des Schubes eines mehrmotorigen Flugzeuges - Google Patents

Einrichtung zur Regelung des Schubes eines mehrmotorigen Flugzeuges

Info

Publication number
DE69703644T2
DE69703644T2 DE69703644T DE69703644T DE69703644T2 DE 69703644 T2 DE69703644 T2 DE 69703644T2 DE 69703644 T DE69703644 T DE 69703644T DE 69703644 T DE69703644 T DE 69703644T DE 69703644 T2 DE69703644 T2 DE 69703644T2
Authority
DE
Germany
Prior art keywords
thrust
controlling
engine aircraft
aircraft
engine
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.)
Expired - Lifetime
Application number
DE69703644T
Other languages
English (en)
Other versions
DE69703644D1 (de
Inventor
Panxika Larramendy
Patrick Zaccaria
Thierry Clavel
Francois Garavel
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Aerospatiale Matra
Original Assignee
Aerospatiale Matra
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 Aerospatiale Matra filed Critical Aerospatiale Matra
Publication of DE69703644D1 publication Critical patent/DE69703644D1/de
Application granted granted Critical
Publication of DE69703644T2 publication Critical patent/DE69703644T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02Initiating means
    • B64D31/06Initiating means actuated automatically
    • B64D31/09Initiating means actuated automatically in response to power plant failure
    • B64D31/10Initiating means actuated automatically in response to power plant failure for preventing asymmetric thrust
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/42Control of fuel supply specially adapted for the control of two or more plants simultaneously
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0072Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements to counteract a motor failure
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Multiple Motors (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
  • Feedback Control In General (AREA)
  • Safety Devices In Control Systems (AREA)
DE69703644T 1996-09-09 1997-09-02 Einrichtung zur Regelung des Schubes eines mehrmotorigen Flugzeuges Expired - Lifetime DE69703644T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9610965A FR2753171B1 (fr) 1996-09-09 1996-09-09 Dispositif de controle de la poussee d'un aeronef a plusieurs moteurs

Publications (2)

Publication Number Publication Date
DE69703644D1 DE69703644D1 (de) 2001-01-11
DE69703644T2 true DE69703644T2 (de) 2001-05-10

Family

ID=9495563

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69703644T Expired - Lifetime DE69703644T2 (de) 1996-09-09 1997-09-02 Einrichtung zur Regelung des Schubes eines mehrmotorigen Flugzeuges

Country Status (6)

Country Link
US (1) US5927655A (de)
EP (1) EP0828206B1 (de)
CA (1) CA2216669C (de)
DE (1) DE69703644T2 (de)
ES (1) ES2153641T3 (de)
FR (1) FR2753171B1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015198A1 (de) * 2009-08-05 2011-02-10 Man Diesel & Turbo Se Mehrmotorenanlage und verfahren zum betreiben dieser

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GB2338793B (en) * 1998-06-25 2002-02-13 Secretary Trade Ind Brit Force measurement system
US6282466B1 (en) * 1998-11-03 2001-08-28 The Boeing Company Method of automated thrust-based roll guidance limiting
FR2806791B1 (fr) * 2000-03-23 2002-05-31 Aerospatiale Matra Airbus Procede pour determiner une vitesse minimale de controle d'un aeronef
FR2855281B1 (fr) * 2003-05-19 2005-08-05 Airbus France Dispositif de reglage d'au moins un parametre, en particulier d'un systeme de pilotage automatique d'un aeronef.
FR2890645B1 (fr) * 2005-09-13 2007-10-12 Airbus France Sas Dispositif de protection d'energie pour un avion.
FR2898584B1 (fr) * 2006-03-15 2008-12-19 Airbus France Sas Procede et dispositif de commande de la poussee d'un aeronef multimoteur
FR2914075B1 (fr) * 2007-03-22 2009-04-24 Airbus France Sas Procede et dispositif de limitation de la commande de roulis d'un aeronef en fonction d'une dissymetrie de poussee
GB0813561D0 (en) * 2008-07-24 2008-09-03 Rolls Royce Plc Developments in or relating to power demand management
NL2002064C (nl) * 2008-10-07 2010-04-08 Robertus Gerardus De Boer Gedifferentieerde stuwkracht startmethode voor een vliegtuig.
FR2937008B1 (fr) * 2008-10-09 2010-11-05 Airbus France Procede et dispositif pour la protection d'energie d'un aeronef.
FR2946015B1 (fr) * 2009-06-02 2011-07-15 Airbus France Systeme de gestion automatique de modes de controle de moteurs d'un aeronef multimoteur.
US8352099B1 (en) * 2009-07-09 2013-01-08 The Boeing Company Varying engine thrust for directional control of an aircraft experiencing engine thrust asymmetry
FR2967213B1 (fr) * 2010-11-10 2012-10-26 Eurocopter France Procede de commande pour systeme de securite survitesse de moteurs d'aeronef et circuit de commande pour mettre en oeuvre ledit procede
CN103502096B (zh) * 2011-04-28 2015-09-16 波音公司 一种用于限制运行在推力不对称的情况下的多发动机飞机的发动机产生的推力的系统和方法
US20140222310A1 (en) * 2012-10-09 2014-08-07 United Technologies Corporation Engine monitor for a multi-engine system
CN103192981A (zh) * 2013-04-12 2013-07-10 北京航空航天大学 电动低噪短距起降连翼飞机
GB201405894D0 (en) * 2014-04-02 2014-05-14 Rolls Royce Plc Aircraft vapour trail control system
EP2957976B1 (de) * 2014-06-20 2018-01-31 Patents Factory Ltd. Sp. z o.o. Verfahren und System zur Kompensation einer asymmetrischen Konfiguration eines Nurflügelträgers für Flugeinheiten
EP3018054B1 (de) * 2014-11-07 2019-01-02 Airbus Defence and Space, S.A. Verfahren zur Steuerung eines Flugzeugpropellersystems während der Schubumkehr
FR3065443B1 (fr) 2017-04-19 2021-01-01 Airbus Group Sas Methode pour la gestion de la dissymetrie au sein d’un systeme de propulsion distribuee

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1344276A (fr) * 1962-07-04 1963-11-29 Fr D Entretien Et De Reparatio Correcteur automatique du gouvernail de direction d'un aérodyne en cas de panne de l'un de ses turbo-moteurs
US4034938A (en) * 1975-04-22 1977-07-12 The Boeing Company Automatic performance reserve (APR) system having means indicative of system armed condition
US3987279A (en) * 1975-04-22 1976-10-19 The Boeing Company Automatic performance reserve (APR) system
US4106730A (en) * 1976-10-01 1978-08-15 The Boeing Company Engine out control system for STOL aircraft
US4845617A (en) * 1987-06-01 1989-07-04 United Technologies Corporation Autofeather state maintenance
US4884205A (en) * 1987-08-04 1989-11-28 Hernandez Diaz Jorge H Method and apparatus for limiting adverse yaw-induced roll during engine failure in multiengine aircraft
FR2710026B1 (fr) * 1993-09-17 1995-12-08 Aerospatiale Dispositif de surveillance du système propulsif d'un aéronef.

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2011015198A1 (de) * 2009-08-05 2011-02-10 Man Diesel & Turbo Se Mehrmotorenanlage und verfahren zum betreiben dieser
CN102472190A (zh) * 2009-08-05 2012-05-23 曼柴油机和涡轮机欧洲股份公司 多发动机设备及其工作方法
CN102472190B (zh) * 2009-08-05 2015-08-19 曼柴油机和涡轮机欧洲股份公司 多发动机设备及其工作方法

Also Published As

Publication number Publication date
CA2216669C (fr) 2005-04-12
US5927655A (en) 1999-07-27
DE69703644D1 (de) 2001-01-11
EP0828206B1 (de) 2000-12-06
CA2216669A1 (fr) 1998-03-09
EP0828206A1 (de) 1998-03-11
ES2153641T3 (es) 2001-03-01
FR2753171A1 (fr) 1998-03-13
FR2753171B1 (fr) 1998-11-13

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Legal Events

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