PL3224141T3 - Zespół napędowy z selektywnymi środkami sprzęgającymi - Google Patents

Zespół napędowy z selektywnymi środkami sprzęgającymi

Info

Publication number
PL3224141T3
PL3224141T3 PL15817948T PL15817948T PL3224141T3 PL 3224141 T3 PL3224141 T3 PL 3224141T3 PL 15817948 T PL15817948 T PL 15817948T PL 15817948 T PL15817948 T PL 15817948T PL 3224141 T3 PL3224141 T3 PL 3224141T3
Authority
PL
Poland
Prior art keywords
drive unit
selective coupling
selective
coupling
drive
Prior art date
Application number
PL15817948T
Other languages
English (en)
Inventor
Olivier Lafargue
Didier CHARTRAIN
Camel SERGHINE
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 PL3224141T3 publication Critical patent/PL3224141T3/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
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/24—Aircraft characterised by the type or position of power plants using steam or spring force
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • 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
    • B64D31/14—Transmitting means between initiating means and power plants
    • 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
    • B64D35/02—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions specially adapted for specific power plants
    • 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
    • B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • 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
    • 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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K5/00—Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
PL15817948T 2014-11-27 2015-11-24 Zespół napędowy z selektywnymi środkami sprzęgającymi PL3224141T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1461585A FR3029172B1 (fr) 2014-11-27 2014-11-27 Groupe propulseur a moyens d'accouplement selectif
EP15817948.1A EP3224141B1 (fr) 2014-11-27 2015-11-24 Groupe propulseur à moyens d'accouplement sélectif
PCT/FR2015/053180 WO2016083720A1 (fr) 2014-11-27 2015-11-24 Groupe propulseur à moyens d'accouplement sélectif

Publications (1)

Publication Number Publication Date
PL3224141T3 true PL3224141T3 (pl) 2020-03-31

Family

ID=52988151

Family Applications (1)

Application Number Title Priority Date Filing Date
PL15817948T PL3224141T3 (pl) 2014-11-27 2015-11-24 Zespół napędowy z selektywnymi środkami sprzęgającymi

Country Status (10)

Country Link
US (1) US10662875B2 (pl)
EP (1) EP3224141B1 (pl)
JP (1) JP6745267B2 (pl)
KR (1) KR102534791B1 (pl)
CN (1) CN107000848B (pl)
CA (1) CA2968476C (pl)
FR (1) FR3029172B1 (pl)
PL (1) PL3224141T3 (pl)
RU (1) RU2707488C2 (pl)
WO (1) WO2016083720A1 (pl)

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FR3047974B1 (fr) * 2016-02-18 2018-01-19 Airbus Helicopters Dispositif et methode de commande d'un embrayage entre le moteur et la boite de transmission principale de puissance d'un aeronef
FR3057120B1 (fr) 2016-10-03 2023-03-17 Safran Helicopter Engines Machine electrique pour turbopropulseur d'aeronef
US10618667B2 (en) * 2016-10-31 2020-04-14 Rolls-Royce Corporation Fan module with adjustable pitch blades and power system
US10826343B2 (en) * 2016-11-17 2020-11-03 General Electric Company High speed electric machine with radially supported rotor magnets
US10683900B2 (en) * 2017-03-29 2020-06-16 Pratt & Whitney Canada Corp. Clutch device for gas turbine engines
FR3077804B1 (fr) * 2018-02-09 2022-03-18 Safran Propulsion hybride pour un aeronef
US20190256202A1 (en) * 2018-02-19 2019-08-22 Parallel Flight Technologies, Inc. Method and apparatus for lifting a payload
FR3079498B1 (fr) * 2018-03-30 2020-06-19 Airbus Operations Unite de propulsion a helice comprenant un moteur thermique et un moteur electrique et aeronef comportant une telle unite de propulsion a helice
US11623757B2 (en) * 2018-06-08 2023-04-11 Embraer S.A. Hybrid electric taxi system (HETS) or full electric taxi system (FETS)
CH715122A1 (de) * 2018-06-25 2019-12-30 kopter group ag Drehflügler mit einem elektrischen Antrieb zum Antreiben eines Haupt- und/oder Heckrotors des Drehflüglers.
FR3087421B1 (fr) * 2018-10-17 2022-03-04 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
CN109733621B (zh) * 2018-12-17 2022-01-18 南京航空航天大学 一种多推进模式的混合动力无人机
US11939074B2 (en) 2018-12-27 2024-03-26 Honda Motor Co., Ltd. Flying body with a control section having a plurality of operational modes
US11732639B2 (en) * 2019-03-01 2023-08-22 Pratt & Whitney Canada Corp. Mechanical disconnects for parallel power lanes in hybrid electric propulsion systems
US11098655B2 (en) * 2019-04-10 2021-08-24 United Technologies Corporation Variable multiple-drive gas turbine engine
US11781476B2 (en) 2019-06-25 2023-10-10 Pratt & Whitney Canada Corp. System and method for operating a multi-engine rotorcraft
FR3099319B1 (fr) * 2019-07-26 2021-06-25 Safran Aircraft Engines Turbomachine comprenant une machine électrique ayant une fonction de démarreur-générateur et procédé de régulation de la vitesse d’une telle machine électrique
CN110486165B (zh) * 2019-07-31 2021-05-07 中国航发南方工业有限公司 涡桨发动机及无人机
US11668245B2 (en) 2020-01-28 2023-06-06 Pratt & Whitney Canada Corp. Gas turbine engine with clutch system between low-pressure compressor and low-pressure turbine
WO2021222776A1 (en) * 2020-04-30 2021-11-04 Volansi, Inc. Hybrid fixed vtol aircraft powered by heavy fuel engine
WO2022094205A1 (en) * 2020-10-29 2022-05-05 Hybrid Project Llc Dual drive hybrid electric power plant for aircraft
FR3116303B1 (fr) 2020-11-16 2022-10-14 Safran Helicopter Engines Turbomachine à propulsion hybride et aéronef comportant une telle turbomachine
WO2022146943A1 (en) 2020-12-28 2022-07-07 Parallel Flight Technologies, Inc. System defining a hybrid power unit for thrust generation in an aerial vehicle and method for controlling the same
FR3126016A1 (fr) 2021-08-04 2023-02-10 Safran Helicopter Engines Turbopropulseur apte à fournir une fonction d’éolienne de secours et aéronef comportant un tel turbopropulseur
EP4310309A1 (en) * 2022-07-19 2024-01-24 General Electric Company Hybrid-electric propulsion system equipped with a coupler for switching between modes of operation
US20240059422A1 (en) * 2022-08-22 2024-02-22 Pratt & Whitney Canada Corp. Multi-drive unit propulsion system for an aircraft
FR3142460A1 (fr) * 2022-11-28 2024-05-31 Safran Helicopter Engines Turbopropulseur hybride amélioré pour aéronef

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Also Published As

Publication number Publication date
FR3029172A1 (fr) 2016-06-03
US20170321601A1 (en) 2017-11-09
RU2017122326A (ru) 2018-12-27
JP2018502242A (ja) 2018-01-25
JP6745267B2 (ja) 2020-08-26
RU2707488C2 (ru) 2019-11-26
EP3224141B1 (fr) 2019-09-25
FR3029172B1 (fr) 2018-05-25
CN107000848A (zh) 2017-08-01
US10662875B2 (en) 2020-05-26
WO2016083720A1 (fr) 2016-06-02
CN107000848B (zh) 2020-06-19
CA2968476C (fr) 2023-04-11
CA2968476A1 (fr) 2016-06-02
RU2017122326A3 (pl) 2019-05-22
KR20170094161A (ko) 2017-08-17
KR102534791B1 (ko) 2023-05-19
EP3224141A1 (fr) 2017-10-04

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