FR3039614B1 - HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING - Google Patents

HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING

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
French (fr)
Other versions
FR3039614A1 (en
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/en
Publication of FR3039614A1 publication Critical patent/FR3039614A1/en
Application granted granted Critical
Publication of FR3039614B1 publication Critical patent/FR3039614B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/24Aircraft characterised by the type or position of power plants using steam or spring force
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/12Rotor drives
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02Aircraft characterised by the type or position of power plants
    • B64D27/026Aircraft 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
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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 HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING Active FR3039614B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1501642A FR3039614B1 (en) 2015-07-31 2015-07-31 HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1501642A FR3039614B1 (en) 2015-07-31 2015-07-31 HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING

Publications (2)

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

Family

ID=54608581

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1501642A Active FR3039614B1 (en) 2015-07-31 2015-07-31 HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING

Country Status (1)

Country Link
FR (1) FR3039614B1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3087421B1 (en) * 2018-10-17 2022-03-04 Voltaero MACHINE COMPRISING A HYBRID POWERTRAIN AND CORRESPONDING METHOD OF CONTROL
EP3670348A1 (en) * 2018-12-20 2020-06-24 Airbus Defence and Space GmbH Device for providing power or thrust to an aerospace vehicle and method for controlling a device for providing power to an aerospace vehicle
FR3092562B1 (en) 2019-02-12 2022-01-28 Airbus Helicopters Process for optimizing the noise generated on the ground by a rotorcraft
FR3094314B1 (en) 2019-03-29 2021-07-09 Airbus Helicopters Method for optimizing the noise generated in flight by a rotorcraft.
FR3096659B1 (en) * 2019-05-29 2021-05-07 Voltaero Machine comprising a hybrid powertrain and corresponding piloting method
FR3109407B1 (en) * 2020-04-17 2024-08-23 Safran Electric power generation system for aircraft
US12054274B2 (en) * 2021-03-19 2024-08-06 Pratt & Whitney Canada Corp. Hybrid electric systems for rotorcraft
FR3123324B1 (en) 2021-05-31 2023-04-21 Airbus Helicopters Method for assisting the piloting of a rotorcraft at high altitudes by providing mechanical power from an electric power plant
US11670942B2 (en) 2021-09-23 2023-06-06 General Electric Company Electrically driven distributed propulsion system
FR3133175B1 (en) * 2022-03-03 2024-03-01 Safran Helicopter Engines Improved propulsion assembly for multi-engine hybrid aircraft
FR3138414A1 (en) * 2022-07-29 2024-02-02 Safran Helicopter Engines MONITORING AN AIRCRAFT PROPULSIVE SYSTEM

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2914697B1 (en) * 2007-04-06 2012-11-30 Turbomeca DEVICE FOR ASSISTING THE TRANSIENT PHASES OF ACCELERATION AND DECELERATION
US8727271B2 (en) * 2008-01-11 2014-05-20 Ival O. Salyer Aircraft using turbo-electric hybrid propulsion system
FR2952907B1 (en) * 2009-11-26 2011-12-09 Eurocopter France MOTOR INSTALLATION, HELICOPTER COMPRISING SUCH A MOTOR INSTALLATION, AND METHOD IMPLEMENTED BY THIS MOTOR INSTALLATION
DE102010021026A1 (en) * 2010-05-19 2011-11-24 Eads Deutschland Gmbh Hybrid propulsion and power system for aircraft
FR2962404B1 (en) * 2010-07-08 2012-07-20 Eurocopter France ELECTRICAL ARCHITECTURE FOR AN AIRCRAFT WITH A HYBRID MOTORIZED TURNING SAIL
FR2993243B1 (en) * 2012-07-12 2014-07-11 Eurocopter France HYBRID POWER SUPPLY ARCHITECTURE MECHANICAL OF A ROTOR, MANAGED FROM THE FLIGHT NETWORK OF A GIRAVION
FR3003514B1 (en) * 2013-03-25 2016-11-18 Eurocopter France AIRCRAFT WITH REVOLVING SAIL WITH HYBRID MOTORIZATION.

Also Published As

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

Similar Documents

Publication Publication Date Title
FR3039614B1 (en) HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING
FR3003514B1 (en) AIRCRAFT WITH REVOLVING SAIL WITH HYBRID MOTORIZATION.
BR112017012232A2 (en) pesticide-active tetracyclic derivatives with sulfur-containing substituents
BR112017014061A2 (en) pesticide-active tetracyclic derivatives with sulfur-containing substituents
DK3212502T3 (en) Aircraft with several rotors
EP3201085A4 (en) Dual rotor, rotary wing aircraft
BR112017007510A2 (en) tetracyclic heterocyclic derivatives with pesticide-active sulfur-containing substituents
BR112017005122A2 (en) pesticide-active tetracyclic derivatives with sulfur-containing substituents.
LT3118080T (en) Tramcar motive power system
EP3201077A4 (en) Dual rotor, rotary wing aircraft
SG11201700607UA (en) Power over ethernet for 10gbase-t ethernet
FR2980771B1 (en) HYBRID AIRCRAFT WITH ROTATING WING
EP3198705A4 (en) Power dense motor with thermal management capability
DK3011170T3 (en) A THREE PART WINDMILL WING
GB2526941B (en) Centrifuge with automatically opening rotor cover
FR3008957B1 (en) REGULATED TRIMMER MOTOR INSTALLATION FOR AN AIRCRAFT WITH A ROTARY VESSEL
GB201406952D0 (en) Open rotor propulsion engine
GB2518934B (en) Rotary vane motor
GB201305461D0 (en) Lift-reducing apparatus for aircraft wings
GB2504369B (en) Aircraft wing
EP3038909A4 (en) Rotor hub for rotary wing aircraft
FR3004699B1 (en) AIRCRAFT COMPRISING A HYBRID ENGINE
EP3124769A4 (en) Package-storage-type engine power generator
IL277226B (en) Rotary engine rotor
HK1251275A1 (en) Drive for a rotatable wing

Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 2

PLSC Publication of the preliminary search report

Effective date: 20170203

PLFP Fee payment

Year of fee payment: 3

PLFP Fee payment

Year of fee payment: 4

PLFP Fee payment

Year of fee payment: 6

PLFP Fee payment

Year of fee payment: 7

PLFP Fee payment

Year of fee payment: 8

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10