FR3039614B1 - Installation motrice hybride pour aeronef a voilure tournante bimoteur - Google Patents

Installation motrice hybride pour aeronef a voilure tournante bimoteur

Info

Publication number
FR3039614B1
FR3039614B1 FR1501642A FR1501642A FR3039614B1 FR 3039614 B1 FR3039614 B1 FR 3039614B1 FR 1501642 A FR1501642 A FR 1501642A FR 1501642 A FR1501642 A FR 1501642A FR 3039614 B1 FR3039614 B1 FR 3039614B1
Authority
FR
France
Prior art keywords
aircraft
power supply
hybrid power
revolving wing
rotary revolving
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
FR1501642A
Other languages
English (en)
Other versions
FR3039614A1 (fr
Inventor
Hopdjanian Marie Laure Grojo
Damien Mariotto
Loic Meiffre
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 Helicopters SAS
Original Assignee
Airbus Helicopters SAS
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 Airbus Helicopters SAS filed Critical Airbus Helicopters SAS
Priority to FR1501642A priority Critical patent/FR3039614B1/fr
Publication of FR3039614A1 publication Critical patent/FR3039614A1/fr
Application granted granted Critical
Publication of FR3039614B1 publication Critical patent/FR3039614B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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
    • 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
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Control Of Eletrric Generators (AREA)
FR1501642A 2015-07-31 2015-07-31 Installation motrice hybride pour aeronef a voilure tournante bimoteur Active FR3039614B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1501642A FR3039614B1 (fr) 2015-07-31 2015-07-31 Installation motrice hybride pour aeronef a voilure tournante bimoteur

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1501642A FR3039614B1 (fr) 2015-07-31 2015-07-31 Installation motrice hybride pour aeronef a voilure tournante bimoteur

Publications (2)

Publication Number Publication Date
FR3039614A1 FR3039614A1 (fr) 2017-02-03
FR3039614B1 true FR3039614B1 (fr) 2018-05-04

Family

ID=54608581

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1501642A Active FR3039614B1 (fr) 2015-07-31 2015-07-31 Installation motrice hybride pour aeronef a voilure tournante bimoteur

Country Status (1)

Country Link
FR (1) FR3039614B1 (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3087421B1 (fr) * 2018-10-17 2022-03-04 Voltaero Engin comprenant un groupe motopropulseur hybride et procede de pilotage correspondant
EP3670348A1 (fr) * 2018-12-20 2020-06-24 Airbus Defence and Space GmbH Dispositif de fourniture de puissance ou de poussée à un véhicule aérospatial et procédé de commande d'un dispositif de fourniture de puissance à un véhicule aérospatial
FR3092562B1 (fr) 2019-02-12 2022-01-28 Airbus Helicopters Procédé d’optimisation du bruit généré au sol par un giravion
FR3094314B1 (fr) 2019-03-29 2021-07-09 Airbus Helicopters Procédé d’optimisation du bruit généré en vol par un giravion.
FR3096659B1 (fr) * 2019-05-29 2021-05-07 Voltaero Engin comprenant un groupe motopropulseur hybride et procédé de pilotage correspondant
FR3109407A1 (fr) * 2020-04-17 2021-10-22 Safran Système de génération de puissance électrique pour aéronef
US12054274B2 (en) * 2021-03-19 2024-08-06 Pratt & Whitney Canada Corp. Hybrid electric systems for rotorcraft
FR3123324B1 (fr) 2021-05-31 2023-04-21 Airbus Helicopters Procédé d’aide au pilotage d’un giravion en hautes altitudes grâce à l’apport d’une puissance mécanique provenant d’une installation motrice électrique
US11670942B2 (en) 2021-09-23 2023-06-06 General Electric Company Electrically driven distributed propulsion system
FR3133175B1 (fr) * 2022-03-03 2024-03-01 Safran Helicopter Engines Ensemble propulsif amélioré pour aéronef hybridé multi moteurs
FR3138414A1 (fr) * 2022-07-29 2024-02-02 Safran Helicopter Engines Surveillance d’un systeme propulsif d’un aeronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914697B1 (fr) * 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
US8727271B2 (en) * 2008-01-11 2014-05-20 Ival O. Salyer Aircraft using turbo-electric hybrid propulsion system
FR2952907B1 (fr) * 2009-11-26 2011-12-09 Eurocopter France Installation motrice, helicoptere comportant une telle installation motrice, et procede mis en oeuvre par cette installation motrice
DE102010021026A1 (de) * 2010-05-19 2011-11-24 Eads Deutschland Gmbh Hybrides Antriebs- und Energiesystem für Fluggeräte
FR2962404B1 (fr) * 2010-07-08 2012-07-20 Eurocopter France Architecture electrique pour aeronef a voilure tournante a motorisation hybride
FR2993243B1 (fr) * 2012-07-12 2014-07-11 Eurocopter France Architecture d'alimentation hybride en puissance mecanique d'un rotor, geree a partir du reseau de bord d'un giravion
FR3003514B1 (fr) * 2013-03-25 2016-11-18 Eurocopter France Aeronef a voilure tournante a motorisation hybride.

Also Published As

Publication number Publication date
FR3039614A1 (fr) 2017-02-03

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