FR3039614B1 - HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WING - Google Patents
HYBRID POWER SUPPLY FOR AN AIRCRAFT WITH A ROTARY REVOLVING WINGInfo
- 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
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)
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)
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)
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. |
-
2015
- 2015-07-31 FR FR1501642A patent/FR3039614B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3039614A1 (en) | 2017-02-03 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20170203 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |