PL3123017T3 - Hydrauliczne urządzenie do awaryjnego rozruchu silnika turbinowego, układ napędowy śmigłowca wielosilnikowego wyposażony w takie urządzenie i odpowiadający śmigłowiec - Google Patents

Hydrauliczne urządzenie do awaryjnego rozruchu silnika turbinowego, układ napędowy śmigłowca wielosilnikowego wyposażony w takie urządzenie i odpowiadający śmigłowiec

Info

Publication number
PL3123017T3
PL3123017T3 PL15717550T PL15717550T PL3123017T3 PL 3123017 T3 PL3123017 T3 PL 3123017T3 PL 15717550 T PL15717550 T PL 15717550T PL 15717550 T PL15717550 T PL 15717550T PL 3123017 T3 PL3123017 T3 PL 3123017T3
Authority
PL
Poland
Prior art keywords
helicopter
engine
propulsion system
emergency starting
turbine engine
Prior art date
Application number
PL15717550T
Other languages
English (en)
Inventor
Romain Thiriet
Bertrand MOINE
Camel SERGHINE
François POREL
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 PL3123017T3 publication Critical patent/PL3123017T3/pl

Links

Classifications

    • 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
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/27Fluid drives
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • 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
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/14Gas-turbine plants having means for storing energy, e.g. for meeting peak loads
    • 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
    • F02C7/00Features, 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
    • F02C7/26Starting; Ignition
    • F02C7/268Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275Mechanical drives
    • 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
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/329Application in turbines in gas turbines in helicopters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/42Storage of energy
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/85Starting
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/09Purpose of the control system to cope with emergencies
    • F05D2270/093Purpose of the control system to cope with emergencies of one engine in a multi-engine system
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
PL15717550T 2014-03-27 2015-03-20 Hydrauliczne urządzenie do awaryjnego rozruchu silnika turbinowego, układ napędowy śmigłowca wielosilnikowego wyposażony w takie urządzenie i odpowiadający śmigłowiec PL3123017T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1452643A FR3019221B1 (fr) 2014-03-27 2014-03-27 Dispositif hydraulique de demarrage d'urgence d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant
EP15717550.6A EP3123017B1 (fr) 2014-03-27 2015-03-20 Dispositif hydraulique de démarrage d'urgence d'un turbomoteur, système propulsif d'un hélicoptère multi-moteur équipé d'un tel dispositif et hélicoptère correspondant
PCT/FR2015/050696 WO2015145040A1 (fr) 2014-03-27 2015-03-20 Dispositif hydraulique de démarrage d'urgence d'un turbomoteur, système propulsif d'un hélicoptère multi-moteur équipé d'un tel dispositif et hélicoptère correspondant

Publications (1)

Publication Number Publication Date
PL3123017T3 true PL3123017T3 (pl) 2019-02-28

Family

ID=50877473

Family Applications (1)

Application Number Title Priority Date Filing Date
PL15717550T PL3123017T3 (pl) 2014-03-27 2015-03-20 Hydrauliczne urządzenie do awaryjnego rozruchu silnika turbinowego, układ napędowy śmigłowca wielosilnikowego wyposażony w takie urządzenie i odpowiadający śmigłowiec

Country Status (11)

Country Link
US (1) US10422285B2 (pl)
EP (1) EP3123017B1 (pl)
JP (1) JP6637898B2 (pl)
KR (1) KR102305967B1 (pl)
CN (1) CN106414910B (pl)
CA (1) CA2941989C (pl)
ES (1) ES2685300T3 (pl)
FR (1) FR3019221B1 (pl)
PL (1) PL3123017T3 (pl)
RU (1) RU2672219C2 (pl)
WO (1) WO2015145040A1 (pl)

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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
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
FR3062882B1 (fr) 2017-02-15 2019-10-18 Safran Helicopter Engines Systeme propulsif d'un helicoptere monomoteur
US11174793B2 (en) 2018-09-19 2021-11-16 Raytheon Technologies Corporation Hydraulic starter assembly for a gas turbine engine
US11628942B2 (en) 2019-03-01 2023-04-18 Pratt & Whitney Canada Corp. Torque ripple control for an aircraft power train
CA3132266A1 (en) 2019-03-01 2020-09-10 Pratt & Whitney Canada Corp. Distributed propulsion configurations for aircraft having mixed drive systems
US11732639B2 (en) 2019-03-01 2023-08-22 Pratt & Whitney Canada Corp. Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
WO2020190344A2 (en) 2019-03-18 2020-09-24 United Technologies Advanced Projects Inc. Architectures for hybrid-electric propulsion
US11299286B2 (en) 2019-05-15 2022-04-12 Pratt & Whitney Canada Corp. System and method for operating a multi-engine aircraft
US11486472B2 (en) 2020-04-16 2022-11-01 United Technologies Advanced Projects Inc. Gear sytems with variable speed drive

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FR1151717A (fr) 1956-06-20 1958-02-05 écrou indessérable
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Also Published As

Publication number Publication date
US10422285B2 (en) 2019-09-24
CN106414910A (zh) 2017-02-15
RU2672219C2 (ru) 2018-11-12
KR20160140621A (ko) 2016-12-07
RU2016136369A (ru) 2018-04-27
EP3123017B1 (fr) 2018-06-27
JP2017519928A (ja) 2017-07-20
US20170016398A1 (en) 2017-01-19
CA2941989A1 (fr) 2015-10-01
KR102305967B1 (ko) 2021-09-28
FR3019221B1 (fr) 2018-10-12
CA2941989C (fr) 2022-05-31
JP6637898B2 (ja) 2020-01-29
WO2015145040A1 (fr) 2015-10-01
RU2016136369A3 (pl) 2018-09-27
CN106414910B (zh) 2018-05-15
EP3123017A1 (fr) 2017-02-01
ES2685300T3 (es) 2018-10-08
FR3019221A1 (fr) 2015-10-02

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