RU2693957C1 - Способ автоматического управления рабочим режимом газотурбинного двигателя вертолета, соответствующее устройство управления и вертолет, оснащенный таким устройством - Google Patents

Способ автоматического управления рабочим режимом газотурбинного двигателя вертолета, соответствующее устройство управления и вертолет, оснащенный таким устройством Download PDF

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Publication number
RU2693957C1
RU2693957C1 RU2016125745A RU2016125745A RU2693957C1 RU 2693957 C1 RU2693957 C1 RU 2693957C1 RU 2016125745 A RU2016125745 A RU 2016125745A RU 2016125745 A RU2016125745 A RU 2016125745A RU 2693957 C1 RU2693957 C1 RU 2693957C1
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Russia
Prior art keywords
mode
gas turbine
helicopter
turbine engine
combustion chamber
Prior art date
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RU2016125745A
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English (en)
Russian (ru)
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RU2016125745A (ru
Inventor
Каролин СЕВ
Венсан ПУМАРЕД
Ромэн ТИРЬЕ
Original Assignee
Сафран Хеликоптер Энджинз
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Publication of RU2016125745A publication Critical patent/RU2016125745A/ru
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    • 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
    • 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
    • B64D31/09—Initiating means actuated automatically in response to power plant failure
    • 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
    • F02C6/02—Plural gas-turbine plants having a common power output
    • 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

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  • 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)
RU2016125745A 2013-12-20 2014-12-15 Способ автоматического управления рабочим режимом газотурбинного двигателя вертолета, соответствующее устройство управления и вертолет, оснащенный таким устройством RU2693957C1 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1363316 2013-12-20
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

Publications (2)

Publication Number Publication Date
RU2016125745A RU2016125745A (ru) 2018-01-25
RU2693957C1 true RU2693957C1 (ru) 2019-07-08

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RU2016125745A RU2693957C1 (ru) 2013-12-20 2014-12-15 Способ автоматического управления рабочим режимом газотурбинного двигателя вертолета, соответствующее устройство управления и вертолет, оснащенный таким устройством

Country Status (10)

Country Link
US (1) US10435167B2 (cg-RX-API-DMAC7.html)
EP (1) EP3084175B1 (cg-RX-API-DMAC7.html)
JP (1) JP6608825B2 (cg-RX-API-DMAC7.html)
KR (1) KR102263904B1 (cg-RX-API-DMAC7.html)
CN (1) CN105829680B (cg-RX-API-DMAC7.html)
CA (1) CA2933357C (cg-RX-API-DMAC7.html)
FR (1) FR3015574B1 (cg-RX-API-DMAC7.html)
PL (1) PL3084175T3 (cg-RX-API-DMAC7.html)
RU (1) RU2693957C1 (cg-RX-API-DMAC7.html)
WO (1) WO2015092252A1 (cg-RX-API-DMAC7.html)

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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
KR102823707B1 (ko) * 2019-11-28 2025-06-24 한국전자통신연구원 전자 장치, 인터럽트 설정 제어 방법 및 저장 매체
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

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EP2301844A1 (fr) * 2009-09-23 2011-03-30 Eurocopter Procédé et dispositif d'aide au pilotage d'un aéronef en cas de pannes d'un indicateur de première limitation
WO2012059671A2 (fr) * 2010-11-04 2012-05-10 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur a systeme de regulation pour sa mise en oeuvre
RU2462607C2 (ru) * 2007-04-06 2012-09-27 Турбомека Устройство содействия для переходных фаз разгона и торможения
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EP2626537A1 (fr) * 2012-02-07 2013-08-14 Eurocopter Procédé automatique de régulation d'un groupe de motorisation d'aéronef, dispositif et aéronef

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RU2462607C2 (ru) * 2007-04-06 2012-09-27 Турбомека Устройство содействия для переходных фаз разгона и торможения
EP2301844A1 (fr) * 2009-09-23 2011-03-30 Eurocopter Procédé et dispositif d'aide au pilotage d'un aéronef en cas de pannes d'un indicateur de première limitation
WO2012059671A2 (fr) * 2010-11-04 2012-05-10 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur a systeme de regulation pour sa mise en oeuvre
WO2013076434A2 (fr) * 2011-11-25 2013-05-30 Turbomeca Procédé et système de régulation de puissance en cas de défaillance d'au moins un moteur d'aéronef
EP2626537A1 (fr) * 2012-02-07 2013-08-14 Eurocopter Procédé automatique de régulation d'un groupe de motorisation d'aéronef, dispositif et aéronef

Also Published As

Publication number Publication date
CN105829680A (zh) 2016-08-03
JP2017502201A (ja) 2017-01-19
US20160311548A1 (en) 2016-10-27
FR3015574B1 (fr) 2019-05-03
FR3015574A1 (fr) 2015-06-26
JP6608825B2 (ja) 2019-11-20
PL3084175T3 (pl) 2020-11-02
RU2016125745A (ru) 2018-01-25
EP3084175B1 (fr) 2020-06-17
CN105829680B (zh) 2018-12-14
KR20160098289A (ko) 2016-08-18
US10435167B2 (en) 2019-10-08
WO2015092252A1 (fr) 2015-06-25
EP3084175A1 (fr) 2016-10-26
KR102263904B1 (ko) 2021-06-11
CA2933357A1 (fr) 2015-06-25
CA2933357C (fr) 2022-03-29

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