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FR2978728B1 - Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie - Google Patents

Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie

Info

Publication number
FR2978728B1
FR2978728B1 FR1157122A FR1157122A FR2978728B1 FR 2978728 B1 FR2978728 B1 FR 2978728B1 FR 1157122 A FR1157122 A FR 1157122A FR 1157122 A FR1157122 A FR 1157122A FR 2978728 B1 FR2978728 B1 FR 2978728B1
Authority
FR
France
Prior art keywords
recovery system
energy recovery
aircraft propulsion
architecture integrating
propulsion architecture
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
FR1157122A
Other languages
English (en)
Other versions
FR2978728A1 (fr
Inventor
Bruno Rechain
Hichem Smaoui
Emmanuel Joubert
Gilles Bezes
Matthieu Sautreuil
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.)
Airbus Group SAS
Airbus Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
European Aeronautic Defence and Space Company EADS France
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 Eurocopter France SA, Eurocopter SA, European Aeronautic Defence and Space Company EADS France filed Critical Eurocopter France SA
Priority to FR1157122A priority Critical patent/FR2978728B1/fr
Priority to CA2843802A priority patent/CA2843802C/fr
Priority to PCT/EP2012/065221 priority patent/WO2013017680A1/fr
Priority to EP12753671.2A priority patent/EP2739530A1/fr
Priority to US14/236,621 priority patent/US9885289B2/en
Publication of FR2978728A1 publication Critical patent/FR2978728A1/fr
Application granted granted Critical
Publication of FR2978728B1 publication Critical patent/FR2978728B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • 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
    • B64D27/30—Aircraft characterised by electric power plants
    • B64D27/33—Hybrid electric aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/82—Rotorcraft; Rotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft
    • B64C2027/8209—Electrically driven tail rotors
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR1157122A 2011-08-03 2011-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie Active FR2978728B1 (fr)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR1157122A FR2978728B1 (fr) 2011-08-03 2011-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
CA2843802A CA2843802C (fr) 2011-08-03 2012-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
PCT/EP2012/065221 WO2013017680A1 (fr) 2011-08-03 2012-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
EP12753671.2A EP2739530A1 (fr) 2011-08-03 2012-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie
US14/236,621 US9885289B2 (en) 2011-08-03 2012-08-03 Aircraft propulsion architecture integrating an energy recovery system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1157122A FR2978728B1 (fr) 2011-08-03 2011-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie

Publications (2)

Publication Number Publication Date
FR2978728A1 FR2978728A1 (fr) 2013-02-08
FR2978728B1 true FR2978728B1 (fr) 2014-07-04

Family

ID=46785368

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1157122A Active FR2978728B1 (fr) 2011-08-03 2011-08-03 Architecture de propulsion d'aeronef integrant un systeme de recuperation d'energie

Country Status (5)

Country Link
US (1) US9885289B2 (fr)
EP (1) EP2739530A1 (fr)
CA (1) CA2843802C (fr)
FR (1) FR2978728B1 (fr)
WO (1) WO2013017680A1 (fr)

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US9637217B2 (en) 2015-09-21 2017-05-02 General Electric Company Aircraft having an aft engine
US9815560B2 (en) * 2015-09-21 2017-11-14 General Electric Company AFT engine nacelle shape for an aircraft
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US9821917B2 (en) 2015-09-21 2017-11-21 General Electric Company Aft engine for an aircraft
US9884687B2 (en) 2015-09-21 2018-02-06 General Electric Company Non-axis symmetric aft engine
US10017270B2 (en) 2015-10-09 2018-07-10 General Electric Company Aft engine for an aircraft
US9764848B1 (en) 2016-03-07 2017-09-19 General Electric Company Propulsion system for an aircraft
US20170292447A1 (en) * 2016-04-08 2017-10-12 Hamilton Sundstrand Corporation Hybrid electric aircraft with rankine cycle heat recovery system
US10392119B2 (en) 2016-04-11 2019-08-27 General Electric Company Electric propulsion engine for an aircraft
US10252810B2 (en) 2016-04-19 2019-04-09 General Electric Company Propulsion engine for an aircraft
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US10526085B2 (en) 2016-06-03 2020-01-07 Bell Textron Inc. Electric distributed propulsion anti-torque redundant power and control system
US10703471B2 (en) 2016-06-03 2020-07-07 Bell Helicopter Textron Inc. Anti-torque control using matrix of fixed blade pitch motor modules
US10377479B2 (en) 2016-06-03 2019-08-13 Bell Helicopter Textron Inc. Variable directional thrust for helicopter tail anti-torque system
US10800539B2 (en) * 2016-08-19 2020-10-13 General Electric Company Propulsion engine for an aircraft
US11105340B2 (en) 2016-08-19 2021-08-31 General Electric Company Thermal management system for an electric propulsion engine
US10676205B2 (en) 2016-08-19 2020-06-09 General Electric Company Propulsion engine for an aircraft
US10093428B2 (en) 2016-08-22 2018-10-09 General Electric Company Electric propulsion system
US10308366B2 (en) 2016-08-22 2019-06-04 General Electric Company Embedded electric machine
US10487839B2 (en) 2016-08-22 2019-11-26 General Electric Company Embedded electric machine
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DE102017201808A1 (de) * 2017-02-06 2018-08-09 Airbus Operations Gmbh Turbine mit einem thermoelektrischen Generator
US10808534B2 (en) 2017-02-08 2020-10-20 General Electric Company Reconfigurable maintenance apparatus
US10822103B2 (en) 2017-02-10 2020-11-03 General Electric Company Propulsor assembly for an aircraft
US10793281B2 (en) 2017-02-10 2020-10-06 General Electric Company Propulsion system for an aircraft
US11149578B2 (en) 2017-02-10 2021-10-19 General Electric Company Propulsion system for an aircraft
US10137981B2 (en) 2017-03-31 2018-11-27 General Electric Company Electric propulsion system for an aircraft
US11186185B2 (en) 2017-05-31 2021-11-30 Textron Innovations Inc. Rotor brake effect by using electric distributed anti-torque generators and opposing electric motor thrust to slow a main rotor
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
US10544705B2 (en) 2018-03-16 2020-01-28 Hamilton Sundstrand Corporation Rankine cycle powered by bleed heat
FR3080608B1 (fr) * 2018-04-26 2022-12-23 Safran Systeme de propulsion hybride pour un aeronef
FR3080607B1 (fr) * 2018-04-26 2020-10-02 Safran Systeme de propulsion hybride pour un aeronef
DE102018208026A1 (de) * 2018-05-22 2019-11-28 MTU Aero Engines AG Abgasbehandlungsvorrichtung, Flugzeugantriebssystem und Verfahren zum Behandeln eines Abgasstromes
DE102018005586A1 (de) 2018-07-17 2020-01-23 Manfred Koch Ein neuer integrierter Prozess für die Herstellung von Kathodenmaterial für Batterien
US11156128B2 (en) 2018-08-22 2021-10-26 General Electric Company Embedded electric machine
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine
US11359635B2 (en) 2019-04-14 2022-06-14 Hamilton Sundstrand Corporation Power modules with regenerative compressor wheels
US10876424B2 (en) 2019-04-14 2020-12-29 Hamilton Sunstrand Corporation Energy recovery modules, generator arrangements, and methods of recovering energy in generator arrangements
FR3095806B1 (fr) 2019-05-06 2021-08-20 Safran Helicopter Engines Système de propulsion hybride pour aéronef à décollage et atterrissage verticaux
US11095246B1 (en) 2020-02-13 2021-08-17 General Electric Company Redundant electric motor drive
US11820526B2 (en) * 2020-02-26 2023-11-21 Honda Motor Co., Ltd. Power supply apparatus for a flying body including a combustion gas and intake air heat exchanger
US12031479B2 (en) * 2020-08-31 2024-07-09 General Electric Company Hybrid electric propulsion system load share
CN112706913B (zh) * 2020-12-07 2022-03-11 沈阳飞机设计研究所扬州协同创新研究院有限公司 一种主动热控分布式电液伺服舵机
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Also Published As

Publication number Publication date
CA2843802A1 (fr) 2013-02-07
FR2978728A1 (fr) 2013-02-08
US20140290208A1 (en) 2014-10-02
CA2843802C (fr) 2019-08-27
US9885289B2 (en) 2018-02-06
WO2013017680A1 (fr) 2013-02-07
EP2739530A1 (fr) 2014-06-11

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