KR102258405B1 - 단발 엔진 헬리콥터의 고체 추진체 추진 시스템을 보조하기 위한 장치, 이러한 장치를 구비하는 단발 엔진 헬리콥터 - Google Patents

단발 엔진 헬리콥터의 고체 추진체 추진 시스템을 보조하기 위한 장치, 이러한 장치를 구비하는 단발 엔진 헬리콥터 Download PDF

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Publication number
KR102258405B1
KR102258405B1 KR1020167030416A KR20167030416A KR102258405B1 KR 102258405 B1 KR102258405 B1 KR 102258405B1 KR 1020167030416 A KR1020167030416 A KR 1020167030416A KR 20167030416 A KR20167030416 A KR 20167030416A KR 102258405 B1 KR102258405 B1 KR 102258405B1
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South Korea
Prior art keywords
engine
turbine
helicopter
drive turbine
power transmission
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Expired - Fee Related
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KR1020167030416A
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English (en)
Korean (ko)
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KR20170002400A (ko
Inventor
로망 티리에
카멀 세르그힌느
패트릭 마르코니
쟝 루이 베스
파스칼 길메
기욤 데미종
필리프 바랫
프랑소와 당귀
쟝-미셸 산니노
드 샤노 니콜라스 마뤼소
Original Assignee
사프란 에어크래프트 엔진
사프란 헬리콥터 엔진스
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Publication of KR20170002400A publication Critical patent/KR20170002400A/ko
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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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/006—Safety devices
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • 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
    • B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F02C7/277—Mechanical drives the starter being a separate turbine
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • 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
    • F05D2270/092—Purpose of the control system to cope with emergencies in particular blow-out and relight
    • 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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Control Of Vehicle Engines Or Engines For Specific Uses (AREA)
  • Control Of Eletrric Generators (AREA)
KR1020167030416A 2014-04-08 2015-04-03 단발 엔진 헬리콥터의 고체 추진체 추진 시스템을 보조하기 위한 장치, 이러한 장치를 구비하는 단발 엔진 헬리콥터 Expired - Fee Related KR102258405B1 (ko)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1453123A FR3019588B1 (fr) 2014-04-08 2014-04-08 Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant
FR1453123 2014-04-08
PCT/FR2015/050878 WO2015155450A1 (fr) 2014-04-08 2015-04-03 Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif

Publications (2)

Publication Number Publication Date
KR20170002400A KR20170002400A (ko) 2017-01-06
KR102258405B1 true KR102258405B1 (ko) 2021-05-31

Family

ID=51483532

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020167030416A Expired - Fee Related KR102258405B1 (ko) 2014-04-08 2015-04-03 단발 엔진 헬리콥터의 고체 추진체 추진 시스템을 보조하기 위한 장치, 이러한 장치를 구비하는 단발 엔진 헬리콥터

Country Status (10)

Country Link
US (1) US20170114723A1 (https=)
EP (1) EP3129619B1 (https=)
JP (1) JP6740137B2 (https=)
KR (1) KR102258405B1 (https=)
CN (1) CN106536350B (https=)
CA (1) CA2944839C (https=)
ES (1) ES2719437T3 (https=)
FR (1) FR3019588B1 (https=)
RU (1) RU2684693C2 (https=)
WO (1) WO2015155450A1 (https=)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3019524B1 (fr) * 2014-04-03 2017-12-08 Turbomeca Chaine motrice pour helicoptere incorporant un module moteur pyrotechnique d'assistance et helicoptere la comportant
IL242061B (en) * 2015-10-13 2020-05-31 Newrocket Ltd Thrusting rockets
FR3050765B1 (fr) * 2016-04-28 2018-04-27 Safran Helicopter Engines Systeme auxiliaire d'entrainement d'un arbre d'un systeme propulsif d'un helicoptere
FR3050815B1 (fr) * 2016-04-28 2019-05-24 Safran Helicopter Engines Systeme d'allumage et dispositif d'entrainement mecanique associe
FR3062881B1 (fr) 2017-02-15 2019-03-15 Safran Helicopter Engines Procede et systeme de commande d'un dispositif d'urgence
FR3062882B1 (fr) * 2017-02-15 2019-10-18 Safran Helicopter Engines Systeme propulsif d'un helicoptere monomoteur
US11001384B2 (en) * 2017-10-02 2021-05-11 Bell Helicopter Textron Inc. Hybrid power systems for aircraft
FR3081150B1 (fr) * 2018-05-18 2020-06-12 Safran Helicopter Engines Architecture de puissance d'un aeronef
FR3104333A1 (fr) * 2019-12-10 2021-06-11 Airbus Operations (S.A.S.) Aéronef comprenant une source de secours d’énergie électrique.
FR3104136A1 (fr) * 2019-12-10 2021-06-11 Airbus Operations (S.A.S.) Système de propulsion d’un aéronef
FR3117450B1 (fr) 2020-12-11 2024-03-01 Safran Helicopter Engines Système propulsif hybride pour un hélicoptère
US11794914B2 (en) 2021-07-19 2023-10-24 Pratt & Whitney Canada Corp. Emergency power unit for electric aircraft
FR3166166A1 (fr) * 2024-09-06 2026-03-13 Safran Helicopter Engines Groupe propulsif pour un aeronef comprenant un turbomoteur et un reducteur

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2460246A (en) 2008-05-21 2009-11-25 Matthew P Wood A helicopter emergency power system

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GB605971A (en) * 1944-12-30 1948-08-04 British Thomson Houston Co Ltd Improvements relating to speed governors for rotary wing aircraft
US2460246A (en) * 1945-04-07 1949-01-25 Redmond Company Inc Speed-responsive rheostat
US2986879A (en) * 1957-06-12 1961-06-06 Bendix Corp Solid propellant starter
FR1422328A (fr) * 1964-11-13 1965-12-24 Sud Aviation Perfectionnements apportés aux mécanismes de transmission de puissance et leurs applications, notamment aux hélicoptères
US3455182A (en) * 1967-04-12 1969-07-15 Garrett Corp Helicopter lift augmentation means
GB1389403A (en) * 1971-06-01 1975-04-03 Westland Aircraft Ltd Helicopter power transmission systems
US5020316A (en) * 1989-05-19 1991-06-04 Coltec Industries Inc. Helicopter control with multiple schedule rotor speed decay anticipator
JPH05193579A (ja) * 1992-01-20 1993-08-03 Mitsubishi Heavy Ind Ltd ターボシャフト・エンジン
RU2065381C1 (ru) * 1993-01-19 1996-08-20 Вертолетный научно-технический комплекс им.Н.И.Камова Главный редуктор вертолета
JP2003056368A (ja) * 2001-08-09 2003-02-26 Kawasaki Heavy Ind Ltd ガスタービン駆動方法および駆動装置
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FR2922860B1 (fr) * 2007-10-26 2010-01-22 Eurocopter France Amelioration aux giravions equipes de turbomoteurs
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
FR2990004B1 (fr) 2012-04-27 2014-04-18 Turbomeca Procede et systeme de demarrage d'urgence d'architecture generatrice d'energie
FR2992024B1 (fr) * 2012-06-15 2017-07-21 Turbomeca Procede et architecture de transfert d'energie optimise entre un moteur auxiliaire de puissance et les moteurs principaux d'un helicoptere
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Also Published As

Publication number Publication date
FR3019588B1 (fr) 2019-06-14
RU2684693C2 (ru) 2019-04-11
CA2944839C (fr) 2022-11-01
RU2016142637A (ru) 2018-05-08
EP3129619A1 (fr) 2017-02-15
CA2944839A1 (fr) 2015-10-15
CN106536350B (zh) 2021-10-19
RU2016142637A3 (https=) 2018-10-29
FR3019588A1 (fr) 2015-10-09
ES2719437T3 (es) 2019-07-10
JP6740137B2 (ja) 2020-08-12
US20170114723A1 (en) 2017-04-27
CN106536350A (zh) 2017-03-22
JP2017521589A (ja) 2017-08-03
EP3129619B1 (fr) 2019-02-27
KR20170002400A (ko) 2017-01-06
WO2015155450A1 (fr) 2015-10-15

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