FR2961767B1 - METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD - Google Patents

METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD

Info

Publication number
FR2961767B1
FR2961767B1 FR1055068A FR1055068A FR2961767B1 FR 2961767 B1 FR2961767 B1 FR 2961767B1 FR 1055068 A FR1055068 A FR 1055068A FR 1055068 A FR1055068 A FR 1055068A FR 2961767 B1 FR2961767 B1 FR 2961767B1
Authority
FR
France
Prior art keywords
vehicle
carrying
increase
electrical energy
electric circuit
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
FR1055068A
Other languages
French (fr)
Other versions
FR2961767A1 (en
Inventor
Jean-Michel Prou
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 Electronics and Defense SAS
Original Assignee
Sagem Defense Securite 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 Sagem Defense Securite SA filed Critical Sagem Defense Securite SA
Priority to FR1055068A priority Critical patent/FR2961767B1/en
Publication of FR2961767A1 publication Critical patent/FR2961767A1/en
Application granted granted Critical
Publication of FR2961767B1 publication Critical patent/FR2961767B1/en
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
    • B60—VEHICLES IN GENERAL
    • B60W—CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION; CONTROL SYSTEMS SPECIALLY ADAPTED FOR HYBRID VEHICLES; ROAD VEHICLE DRIVE CONTROL SYSTEMS FOR PURPOSES NOT RELATED TO THE CONTROL OF A PARTICULAR SUB-UNIT
    • B60W20/00—Control systems specially adapted for hybrid vehicles
    • B60W20/10—Controlling the power contribution of each of the prime movers to meet required power demand
    • B60W20/15—Control strategies specially adapted for achieving a particular effect
    • B60W20/19—Control strategies specially adapted for achieving a particular effect for achieving enhanced acceleration
    • 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
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60W—CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION; CONTROL SYSTEMS SPECIALLY ADAPTED FOR HYBRID VEHICLES; ROAD VEHICLE DRIVE CONTROL SYSTEMS FOR PURPOSES NOT RELATED TO THE CONTROL OF A PARTICULAR SUB-UNIT
    • B60W2510/00—Input parameters relating to a particular sub-units
    • B60W2510/24—Energy storage means
    • B60W2510/242—Energy storage means for electrical energy
    • B60W2510/244—Charge state
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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)
  • Automation & Control Theory (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Electric Propulsion And Braking For Vehicles (AREA)
  • Charge And Discharge Circuits For Batteries Or The Like (AREA)
FR1055068A 2010-06-24 2010-06-24 METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD Active FR2961767B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1055068A FR2961767B1 (en) 2010-06-24 2010-06-24 METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1055068A FR2961767B1 (en) 2010-06-24 2010-06-24 METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD

Publications (2)

Publication Number Publication Date
FR2961767A1 FR2961767A1 (en) 2011-12-30
FR2961767B1 true FR2961767B1 (en) 2013-02-08

Family

ID=43466962

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1055068A Active FR2961767B1 (en) 2010-06-24 2010-06-24 METHOD FOR MANAGING ELECTRICAL ENERGY IN A VEHICLE TO INCREASE ITS OPERATING SAFETY, ELECTRIC CIRCUIT AND VEHICLE FOR CARRYING OUT SAID METHOD

Country Status (1)

Country Link
FR (1) FR2961767B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR2997382B1 (en) 2012-10-29 2014-11-21 Eurocopter France METHOD FOR MANAGING AN ENGINE FAILURE ON A MULTI-ENGINE AIRCRAFT PROVIDED WITH A HYBRID POWER PLANT
FR3023989B1 (en) 2014-07-17 2016-08-26 Airbus Helicopters ELECTRIC ARCHITECTURE OF AN AIRCRAFT, AIRCRAFT AND METHOD USED
FR3056558B1 (en) * 2016-09-26 2021-06-04 Safran PROCESS FOR OPTIMIZING THE OPERABILITY OF THE MOTORIZATION OF AN AIRCRAFT
FR3084318B1 (en) * 2018-07-25 2020-06-26 Airbus Helicopters METHOD AND DEVICE FOR MANAGING THE ENERGY OF A HYBRID POWER PLANT OF A MULTIROTOR AIRCRAFT

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6583599B1 (en) * 2000-11-03 2003-06-24 Ford Global Technologies, Inc. Method and apparatus for controlling battery charging in a hybrid electric vehicle
DE10318882A1 (en) * 2003-04-17 2004-11-04 Volkswagen Ag Device and method for energy management in a motor vehicle
US20080184906A1 (en) * 2007-02-07 2008-08-07 Kejha Joseph B Long range hybrid electric airplane
DE102007017332A1 (en) * 2007-04-11 2008-10-16 Flight - Design - GmbH Flugsportgeräte aircraft
FR2931456B1 (en) * 2008-05-26 2010-06-11 Snecma AIRCRAFT WITH HYBRID POWER SUPPLY.
FR2933910B1 (en) * 2008-07-18 2010-12-17 Eurocopter France HYBRID POWER PLANT AND METHOD FOR CONTROLLING SUCH A MOTOR INSTALLATION
FR2936207B1 (en) * 2008-09-23 2011-07-29 Peugeot Citroen Automobiles Sa METHOD AND DEVICE FOR CONTROLLING AN ENERGY STORER FOR A HYBRID VEHICLE
US8128019B2 (en) * 2008-12-12 2012-03-06 Honeywell International Inc. Hybrid power for ducted fan unmanned aerial systems

Also Published As

Publication number Publication date
FR2961767A1 (en) 2011-12-30

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