PL3084175T3 - Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie - Google Patents

Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie

Info

Publication number
PL3084175T3
PL3084175T3 PL14827845T PL14827845T PL3084175T3 PL 3084175 T3 PL3084175 T3 PL 3084175T3 PL 14827845 T PL14827845 T PL 14827845T PL 14827845 T PL14827845 T PL 14827845T PL 3084175 T3 PL3084175 T3 PL 3084175T3
Authority
PL
Poland
Prior art keywords
helicopter
corresponding control
operating speed
automatically controlling
control device
Prior art date
Application number
PL14827845T
Other languages
English (en)
Inventor
Caroline SEVE
Vincent POUMAREDE
Romain Thiriet
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL3084175T3 publication Critical patent/PL3084175T3/pl

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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/02—Initiating means
    • B64D31/06—Initiating means actuated automatically
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/02—Shutting-down responsive to overspeed
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/32—Application in turbines in gas turbines
    • F05D2220/329—Application in turbines in gas turbines in helicopters
    • 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
    • F05D2270/07—Purpose of the control system to improve fuel economy
    • 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
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • 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
    • F05D2270/09—Purpose of the control system to cope with emergencies
    • F05D2270/093—Purpose of the control system to cope with emergencies of one engine in a multi-engine system
    • 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
    • F05D2270/13—Purpose of the control system to control two or more engines simultaneously
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Control Of Velocity Or Acceleration (AREA)
PL14827845T 2013-12-20 2014-12-15 Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie PL3084175T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1363316A FR3015574B1 (fr) 2013-12-20 2013-12-20 Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif
PCT/FR2014/053351 WO2015092252A1 (fr) 2013-12-20 2014-12-15 Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif
EP14827845.0A EP3084175B1 (fr) 2013-12-20 2014-12-15 Procede de commande automatique du regime de fonctionnement d'un turbomoteur d'un helicoptere, dispositif de commande correspondant et helicoptere equipe d'un tel dispositif

Publications (1)

Publication Number Publication Date
PL3084175T3 true PL3084175T3 (pl) 2020-11-02

Family

ID=50290026

Family Applications (1)

Application Number Title Priority Date Filing Date
PL14827845T PL3084175T3 (pl) 2013-12-20 2014-12-15 Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie

Country Status (10)

Country Link
US (1) US10435167B2 (pl)
EP (1) EP3084175B1 (pl)
JP (1) JP6608825B2 (pl)
KR (1) KR102263904B1 (pl)
CN (1) CN105829680B (pl)
CA (1) CA2933357C (pl)
FR (1) FR3015574B1 (pl)
PL (1) PL3084175T3 (pl)
RU (1) RU2693957C1 (pl)
WO (1) WO2015092252A1 (pl)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3026435B1 (fr) * 2014-09-29 2016-10-21 Turbomeca Dispositif et procede de test d'integrite d'un systeme de reactivation rapide d'un turbomoteur d'un helicoptere
US10604268B2 (en) * 2017-02-22 2020-03-31 Pratt & Whitney Canada Corp. Autothrottle control for turboprop engines
FR3082225B1 (fr) * 2018-06-07 2020-06-05 Safran Helicopter Engines Systeme propulsif asymetrique a recuperation de chaleur
CN109228805B (zh) * 2018-08-22 2021-07-09 上海工程技术大学 一种汽车轮胎紧急自动充气装置
CN109236475B (zh) * 2018-11-15 2020-07-17 中国直升机设计研究所 一种单发直升机涡轴发动机的电气控制系统
US11725597B2 (en) * 2019-02-08 2023-08-15 Pratt & Whitney Canada Corp. System and method for exiting an asymmetric engine operating regime
US11299286B2 (en) 2019-05-15 2022-04-12 Pratt & Whitney Canada Corp. System and method for operating a multi-engine aircraft
CN114508435A (zh) * 2022-02-17 2022-05-17 上海东古智能科技有限公司 一种双冲程汽油航空发动机的控制系统

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2188960C1 (ru) * 2001-08-20 2002-09-10 Кондрашов Борис Михайлович Способ преобразования энергии в силовой установке (варианты), струйно-адаптивном двигателе и газогенераторе
JP2005247008A (ja) * 2004-03-01 2005-09-15 Yamaha Motor Co Ltd 無人ヘリコプタ用制御装置
FR2914697B1 (fr) * 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
US8200375B2 (en) * 2008-02-12 2012-06-12 Stuckman Katherine C Radio controlled aircraft, remote controller and methods for use therewith
FR2950109B1 (fr) * 2009-09-17 2012-07-27 Turbomeca Turbomoteur a arbres paralleles
ITTO20090079U1 (it) 2009-06-10 2010-12-11 Agusta Spa Sistema per la gestione ed il controllo della velocita' di uno o piu' rotori di un aeromobile atto a volare a punto fisso
FR2950324B1 (fr) * 2009-09-23 2011-08-26 Eurocopter France Procede et dispositif d'aide au pilotage d'un aeronef en cas de pannes d'un indicateur de premiere limitation
US20110154805A1 (en) * 2009-12-31 2011-06-30 Craig Heathco Power augmentation system for an engine powered air vehicle
FR2967132B1 (fr) * 2010-11-04 2012-11-09 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre
FR2983319B1 (fr) * 2011-11-25 2014-02-07 Turbomeca Procede et systeme de regulation de puissance en cas de defaillance d'au moins un moteur d'aeronef
US8768598B2 (en) * 2011-12-26 2014-07-01 Textron Innovations Inc. Dual gain digital engine control
FR2986573B1 (fr) * 2012-02-07 2014-02-21 Eurocopter France Procede automatique de regulation d'un groupe de motorisation d'aeronef, dispositif et aeronef
FR2986572B1 (fr) * 2012-02-07 2016-04-29 Eurocopter France Procede automatique de regulation d'un groupe de motorisation d'aeronef, dispositif et aeronef
US9091616B2 (en) * 2013-06-06 2015-07-28 Honeywell International Inc. Engine operations support systems and methods for reducing fuel flow
US10850863B2 (en) * 2014-03-04 2020-12-01 Pratt & Whitney Canada Corp. System and method for operating a multi-engine aircraft in an auxiliary power unit mode
US20150266589A1 (en) * 2014-03-24 2015-09-24 Honeywell International Inc. Aircraft systems and methods with green fuel tanks
US9547990B2 (en) * 2014-08-21 2017-01-17 Honeywell International Inc. Rotary-wing aircraft emergency landing control

Also Published As

Publication number Publication date
US20160311548A1 (en) 2016-10-27
EP3084175A1 (fr) 2016-10-26
US10435167B2 (en) 2019-10-08
CN105829680B (zh) 2018-12-14
KR102263904B1 (ko) 2021-06-11
CA2933357C (fr) 2022-03-29
EP3084175B1 (fr) 2020-06-17
FR3015574B1 (fr) 2019-05-03
JP6608825B2 (ja) 2019-11-20
JP2017502201A (ja) 2017-01-19
KR20160098289A (ko) 2016-08-18
RU2016125745A (ru) 2018-01-25
CN105829680A (zh) 2016-08-03
FR3015574A1 (fr) 2015-06-26
WO2015092252A1 (fr) 2015-06-25
CA2933357A1 (fr) 2015-06-25
RU2693957C1 (ru) 2019-07-08

Similar Documents

Publication Publication Date Title
PL3084175T3 (pl) Sposób automatycznego sterowania trybem pracy silnika turbinowego śmigłowca, odpowiednie urządzenie sterujące i śmigłowiec wyposażony w takie urządzenie
EP3193496A4 (en) Controller, control method, and flight vehicle device
PL3123020T3 (pl) Sposób wykrywania awarii pierwszego silnika turbinowego śmigłowca dwusilnikowego i sterowania drugim silnikiem turbinowym oraz odpowiadające mu urządzenie
PL3071798T3 (pl) Maszyna wirowa i sposób sterowania
EP3015148A4 (en) Control device, control system, and control method of aircraft
PL3123007T3 (pl) Silnik turbinowy, śmigłowiec dwusilnikowy wyposażony w taki silnik turbinowy oraz sposób optymalizacji trybu pracy takiego dwusilnikowego śmigłowca na biegu super-jałowym z mocą zerową
GB2505022B (en) Speed control system and method for operating the same
EP3015692A4 (en) Engine control device
EP3121432A4 (en) Control device and control method for diesel engine
GB2558017B (en) Method for monitoring an aircraft engine operating in a given environment
PL3123008T3 (pl) Silnik turbinowy zawierający urządzenie do sterowanego mechanicznego sprzęgania, śmigłowiec wyposażony w taki silnik turbinowy i sposób optymalizacji trybu biegu jałowego o zerowej mocy w takim śmigłowcu
EP2977596B8 (de) Brennkraftmaschine mit einer regeleinrichtung
PL3339182T3 (pl) Urządzenie do regulacji prędkości obrotowej wału generatora gazu silnika turbinowego wiropłatu, wiropłat wyposażony w takie urządzenie oraz skojarzony z nim sposób regulacji
EP3015693A4 (en) Engine control device
EP2982867A4 (en) DRIVE CONTROL SYSTEM FOR SITE ENGINE, SITE ENGINE WITH DRIVE CONTROL SYSTEM, AND DRIVING CONTROL METHOD FOR SAME
EP3078565A4 (en) Train operation control device, control method, and control program
EP3015685A4 (en) Engine control device
EP3034841A4 (en) Gas turbine engine optimization control device
EP2927131A4 (en) AIRCRAFT CONTROL DEVICE, AIRCRAFT AND AIRCRAFT CONTROL METHOD
GB201307308D0 (en) A method of, and apparatus for, controlling the speed of a vehicle
EP2979944A4 (en) Engine rotation control system
EP3015691A4 (en) Engine control device
EP3150834A4 (en) Engine rotation speed control device
EP3079216A4 (en) Power control system, power control device, and method for controlling power control system
EP3009667A4 (en) Engine start-up device, and engine-start-up control method