FR3080608B1 - Systeme de propulsion hybride pour un aeronef - Google Patents

Systeme de propulsion hybride pour un aeronef Download PDF

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Publication number
FR3080608B1
FR3080608B1 FR1853678A FR1853678A FR3080608B1 FR 3080608 B1 FR3080608 B1 FR 3080608B1 FR 1853678 A FR1853678 A FR 1853678A FR 1853678 A FR1853678 A FR 1853678A FR 3080608 B1 FR3080608 B1 FR 3080608B1
Authority
FR
France
Prior art keywords
aircraft
propulsion system
hybrid propulsion
hybrid
propulsion
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
FR1853678A
Other languages
English (en)
Other versions
FR3080608A1 (fr
Inventor
Gaetan Chesneau
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran SA
Original Assignee
Safran SA
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 SA filed Critical Safran SA
Priority to FR1853678A priority Critical patent/FR3080608B1/fr
Priority to PCT/FR2019/050977 priority patent/WO2019207256A1/fr
Publication of FR3080608A1 publication Critical patent/FR3080608A1/fr
Application granted granted Critical
Publication of FR3080608B1 publication Critical patent/FR3080608B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • 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
    • B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
    • B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01K—STEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K23/00—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids
    • F01K23/02—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled
    • F01K23/06—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle
    • F01K23/065—Plants characterised by more than one engine delivering power external to the plant, the engines being driven by different fluids the engine cycles being thermally coupled combustion heat from one cycle heating the fluid in another cycle the combustion taking place in an internal combustion piston engine, e.g. a diesel engine
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Hybrid Electric Vehicles (AREA)
FR1853678A 2018-04-26 2018-04-26 Systeme de propulsion hybride pour un aeronef Active FR3080608B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1853678A FR3080608B1 (fr) 2018-04-26 2018-04-26 Systeme de propulsion hybride pour un aeronef
PCT/FR2019/050977 WO2019207256A1 (fr) 2018-04-26 2019-04-25 Systeme de propulsion hybride pour un aeronef

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1853678 2018-04-26
FR1853678A FR3080608B1 (fr) 2018-04-26 2018-04-26 Systeme de propulsion hybride pour un aeronef

Publications (2)

Publication Number Publication Date
FR3080608A1 FR3080608A1 (fr) 2019-11-01
FR3080608B1 true FR3080608B1 (fr) 2022-12-23

Family

ID=63036092

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1853678A Active FR3080608B1 (fr) 2018-04-26 2018-04-26 Systeme de propulsion hybride pour un aeronef

Country Status (2)

Country Link
FR (1) FR3080608B1 (fr)
WO (1) WO2019207256A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115432190B (zh) * 2022-09-22 2023-06-02 中国商用飞机有限责任公司 电动飞机综合电推进系统

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040155468A1 (en) * 2003-02-12 2004-08-12 Tai-Her Yang Series and parallel combined dual power drive system
JP4407679B2 (ja) * 2006-08-25 2010-02-03 マツダ株式会社 ハイブリッド車両の制御装置
WO2008041891A1 (fr) * 2006-10-06 2008-04-10 Volvo Construction Equipment Ab Procédé permettant de faire fonctionner un engin de chantier et engin de chantier doté d'une ligne de transmission améliorée
DE102007017332A1 (de) 2007-04-11 2008-10-16 Flight - Design - GmbH Flugsportgeräte Luftfahrzeug
FR2962404B1 (fr) * 2010-07-08 2012-07-20 Eurocopter France Architecture electrique pour aeronef a voilure tournante a motorisation hybride
FR2978728B1 (fr) * 2011-08-03 2014-07-04 Eads Europ Aeronautic Defence Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
ES2500015B1 (es) 2013-02-28 2015-06-23 Axter Aerospace S.L. Sistema de potencia auxiliar eléctrico para aeronaves de motor de pistón
FR3023989B1 (fr) * 2014-07-17 2016-08-26 Airbus Helicopters Architecture electrique d'un aeronef, aeronef et procede mis en oeuvre

Also Published As

Publication number Publication date
WO2019207256A1 (fr) 2019-10-31
FR3080608A1 (fr) 2019-11-01

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