PL3207223T3 - Konstrukcja układu napędowego śmigłowca zawierającego hybrydowy silnik turbinowy i układ ponownego uruchamiania takiego hybrydowego silnika turbinowego - Google Patents

Konstrukcja układu napędowego śmigłowca zawierającego hybrydowy silnik turbinowy i układ ponownego uruchamiania takiego hybrydowego silnika turbinowego

Info

Publication number
PL3207223T3
PL3207223T3 PL15791693T PL15791693T PL3207223T3 PL 3207223 T3 PL3207223 T3 PL 3207223T3 PL 15791693 T PL15791693 T PL 15791693T PL 15791693 T PL15791693 T PL 15791693T PL 3207223 T3 PL3207223 T3 PL 3207223T3
Authority
PL
Poland
Prior art keywords
turboshaft engine
hybrid turboshaft
reactivating
hybrid
helicopter including
Prior art date
Application number
PL15791693T
Other languages
English (en)
Inventor
Philippe VALLART
Jean-Michel Bazet
Loïc LE DUIGOU
Original Assignee
Safran Helicopter Engines
Safran Electrical & Power
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, Safran Electrical & Power filed Critical Safran Helicopter Engines
Publication of PL3207223T3 publication Critical patent/PL3207223T3/pl

Links

Classifications

    • 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
    • F01D13/00—Combinations of two or more machines or engines
    • 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
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • B64C27/14—Direct drive between power plant and rotor hub
    • 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 
    • 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
    • F01D13/00—Combinations of two or more machines or engines
    • F01D13/003—Combinations of two or more machines or engines with at least two independent shafts, i.e. cross-compound
    • 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
    • F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • 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
    • 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
    • B64D27/026—Aircraft characterised by the type or position of power plants comprising different types of power plants, e.g. combination of a piston engine and a gas-turbine
    • 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
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
  • Plasma Technology (AREA)
PL15791693T 2014-10-13 2015-10-06 Konstrukcja układu napędowego śmigłowca zawierającego hybrydowy silnik turbinowy i układ ponownego uruchamiania takiego hybrydowego silnika turbinowego PL3207223T3 (pl)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1459777A FR3027058B1 (fr) 2014-10-13 2014-10-13 Architecture d'un systeme propulsif d'un helicoptere comprenant un turbomoteur hybride et un systeme de reactivation de ce turbomoteur hybride
EP15791693.3A EP3207223B1 (fr) 2014-10-13 2015-10-06 Architecture d'un systeme propulsif d'un helicoptere comprenant un turbomoteur hybride et un systeme de reactivation de ce turbomoteur hybride
PCT/FR2015/052683 WO2016059320A1 (fr) 2014-10-13 2015-10-06 Architecture d'un systeme propulsif d'un helicoptere comprenant un turbomoteur hybride et un systeme de reactivation de ce turbomoteur hybride

Publications (1)

Publication Number Publication Date
PL3207223T3 true PL3207223T3 (pl) 2018-09-28

Family

ID=51987386

Family Applications (1)

Application Number Title Priority Date Filing Date
PL15791693T PL3207223T3 (pl) 2014-10-13 2015-10-06 Konstrukcja układu napędowego śmigłowca zawierającego hybrydowy silnik turbinowy i układ ponownego uruchamiania takiego hybrydowego silnika turbinowego

Country Status (11)

Country Link
US (2) US11161603B2 (pl)
EP (1) EP3207223B1 (pl)
JP (1) JP6639510B2 (pl)
KR (1) KR102447272B1 (pl)
CN (1) CN106795774B (pl)
CA (1) CA2963694C (pl)
ES (1) ES2676275T3 (pl)
FR (1) FR3027058B1 (pl)
PL (1) PL3207223T3 (pl)
RU (1) RU2689223C2 (pl)
WO (1) WO2016059320A1 (pl)

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US11994722B2 (en) 2020-11-30 2024-05-28 Corning Research & Development Corporation Fiber optic adapter assemblies including an adapter housing and a locking housing
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Also Published As

Publication number Publication date
CN106795774A (zh) 2017-05-31
WO2016059320A1 (fr) 2016-04-21
EP3207223B1 (fr) 2018-05-16
JP6639510B2 (ja) 2020-02-05
US11597504B2 (en) 2023-03-07
US20220024568A1 (en) 2022-01-27
CA2963694C (fr) 2023-03-14
US20170305541A1 (en) 2017-10-26
FR3027058B1 (fr) 2016-11-04
EP3207223A1 (fr) 2017-08-23
US11161603B2 (en) 2021-11-02
RU2017113510A (ru) 2018-11-15
CN106795774B (zh) 2020-01-10
CA2963694A1 (fr) 2016-04-21
KR20170070063A (ko) 2017-06-21
RU2689223C2 (ru) 2019-05-24
JP2017537268A (ja) 2017-12-14
FR3027058A1 (fr) 2016-04-15
RU2017113510A3 (pl) 2019-04-02
KR102447272B1 (ko) 2022-09-29
ES2676275T3 (es) 2018-07-18

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