JPS6345429A - ヘリコプタのエンジン運転パラメ−タ制御方法及び電子燃料制御装置 - Google Patents

ヘリコプタのエンジン運転パラメ−タ制御方法及び電子燃料制御装置

Info

Publication number
JPS6345429A
JPS6345429A JP62195137A JP19513787A JPS6345429A JP S6345429 A JPS6345429 A JP S6345429A JP 62195137 A JP62195137 A JP 62195137A JP 19513787 A JP19513787 A JP 19513787A JP S6345429 A JPS6345429 A JP S6345429A
Authority
JP
Japan
Prior art keywords
engine
speed
rotor speed
normal threshold
limit
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.)
Pending
Application number
JP62195137A
Other languages
English (en)
Japanese (ja)
Inventor
ロバート・ウェイン・ライス
ニコラス・ディーン・ラポス
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of JPS6345429A publication Critical patent/JPS6345429A/ja
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/28—Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0858—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft specially adapted for vertical take-off of aircraft
    • 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
    • F05D2270/02—Purpose of the control system to control rotational speed (n)
    • 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
    • F05D2270/052—Torque
    • 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
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/112—Purpose of the control system to prolong engine life by limiting temperatures

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Eletrric Generators (AREA)
  • Catching Or Destruction (AREA)
  • Controls For Constant Speed Travelling (AREA)
JP62195137A 1986-08-04 1987-08-04 ヘリコプタのエンジン運転パラメ−タ制御方法及び電子燃料制御装置 Pending JPS6345429A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US89268986A 1986-08-04 1986-08-04
US892689 1986-08-04

Publications (1)

Publication Number Publication Date
JPS6345429A true JPS6345429A (ja) 1988-02-26

Family

ID=25400361

Family Applications (1)

Application Number Title Priority Date Filing Date
JP62195137A Pending JPS6345429A (ja) 1986-08-04 1987-08-04 ヘリコプタのエンジン運転パラメ−タ制御方法及び電子燃料制御装置

Country Status (6)

Country Link
JP (1) JPS6345429A (it)
BR (1) BR8701672A (it)
DE (1) DE3725687A1 (it)
FR (1) FR2602270A1 (it)
GB (1) GB2193535A (it)
IT (1) IT1228547B (it)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5258505A (en) * 1991-07-26 1993-11-02 Canon Kabushiki Kaisha Trisazo compounds, and dye compositions containing same

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8730187D0 (en) * 1987-12-24 1988-02-03 Rolls Royce Plc Overspeed limiter for gas turbine aeroengine
GB2262623B (en) * 1991-12-17 1995-04-26 Rolls Royce Plc Aircraft engine management system
US6012676A (en) * 1998-03-31 2000-01-11 Sikorsky Aircraft Corporation Integrated fire and flight control system with automatic engine torque limiting
FR2878288B1 (fr) 2004-11-25 2007-01-19 Eurocopter France Procede et dispositif pour optimiser l'enveloppe de performances d'un turbomoteur
FR2888287B1 (fr) * 2005-07-07 2011-04-08 Eurocopter France Procede d'optimisation de l'enveloppe de perfomances d'un turbomoteur.
DE102009016106A1 (de) * 2009-02-20 2010-08-26 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zum Messen der Beanspruchung rotierender Wellen von Turbomaschinen und Flugtriebwerken und Vorrichtung zur Durchführung des Verfahrens
DE102009016105B4 (de) * 2009-02-20 2017-11-16 Rolls-Royce Deutschland Ltd & Co Kg Verfahren und Vorrichtung zum Messen der Beanspruchung rotierender Wellen
FR2966881B1 (fr) 2010-10-29 2013-08-30 Eurocopter France Installation motrice d'un aeronef, aeronef, et procede de pilotage dudit aeronef.
FR2985715B1 (fr) 2012-01-12 2013-12-27 Eurocopter France Installation motrice d'un aeronef, aeronef, et procede de pilotage dudit aeronef
FR3000989A1 (fr) 2013-01-16 2014-07-18 Eurocopter France Systeme de surveillance du demarrage d'un aeronef a voilure tournante, aeronef et procede mettant en oeuvre ce systeme
US9771167B2 (en) 2013-01-16 2017-09-26 Airbus Helicopters Monitor system for monitoring the starting of a rotary wing aircraft, an aircraft, and a method using the system
FR3034403B1 (fr) 2015-03-31 2017-03-31 Airbus Helicopters Procede et dispositif pour arreter un turbomoteur en fonctionnement nominal

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5258505A (en) * 1991-07-26 1993-11-02 Canon Kabushiki Kaisha Trisazo compounds, and dye compositions containing same

Also Published As

Publication number Publication date
GB2193535A (en) 1988-02-10
IT8721567A0 (it) 1987-08-03
BR8701672A (pt) 1988-01-05
IT1228547B (it) 1991-06-20
DE3725687A1 (de) 1988-02-18
GB8718303D0 (en) 1987-09-09
FR2602270A1 (fr) 1988-02-05

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