FR3142277B1 - Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique - Google Patents

Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique Download PDF

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Publication number
FR3142277B1
FR3142277B1 FR2212089A FR2212089A FR3142277B1 FR 3142277 B1 FR3142277 B1 FR 3142277B1 FR 2212089 A FR2212089 A FR 2212089A FR 2212089 A FR2212089 A FR 2212089A FR 3142277 B1 FR3142277 B1 FR 3142277B1
Authority
FR
France
Prior art keywords
authorizing
flight
aircraft
electric motor
power plant
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
FR2212089A
Other languages
English (en)
Other versions
FR3142277A1 (fr
Inventor
Jérôme Camus
Julien Laurent
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
Airbus Defence and Space SAS
Original Assignee
Airbus Helicopters SAS
Airbus Defence and Space 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, Airbus Defence and Space SAS filed Critical Airbus Helicopters SAS
Priority to FR2212089A priority Critical patent/FR3142277B1/fr
Priority to EP23197103.7A priority patent/EP4371883B1/fr
Priority to US18/380,252 priority patent/US12142149B2/en
Publication of FR3142277A1 publication Critical patent/FR3142277A1/fr
Application granted granted Critical
Publication of FR3142277B1 publication Critical patent/FR3142277B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L3/00—Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
    • B60L3/0023—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train
    • B60L3/0046—Detecting, eliminating, remedying or compensating for drive train abnormalities, e.g. failures within the drive train relating to electric energy storage systems, e.g. batteries or capacitors
    • G—PHYSICS
    • G08—SIGNALLING
    • G08G—TRAFFIC CONTROL SYSTEMS
    • G08G5/00—Traffic control systems for aircraft
    • G08G5/20—Arrangements for acquiring, generating, sharing or displaying traffic information
    • G08G5/22—Arrangements for acquiring, generating, sharing or displaying traffic information located on the ground
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L50/00—Electric propulsion with power supplied within the vehicle
    • B60L50/50—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells
    • B60L50/60—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries
    • B60L50/61—Electric propulsion with power supplied within the vehicle using propulsion power supplied by batteries or fuel cells using power supplied by batteries by batteries charged by engine-driven generators, e.g. series hybrid electric vehicles
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R19/00—Arrangements for measuring currents or voltages or for indicating presence or sign thereof
    • G01R19/165—Indicating that current or voltage is either above or below a predetermined value or within or outside a predetermined range of values
    • G01R19/16533—Indicating that current or voltage is either above or below a predetermined value or within or outside a predetermined range of values characterised by the application
    • G01R19/16538—Indicating that current or voltage is either above or below a predetermined value or within or outside a predetermined range of values characterised by the application in AC or DC supplies
    • G01R19/16542—Indicating that current or voltage is either above or below a predetermined value or within or outside a predetermined range of values characterised by the application in AC or DC supplies for batteries
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
    • G01R31/3644—Constructional arrangements
    • G01R31/3647—Constructional arrangements for determining the ability of a battery to perform a critical function, e.g. cranking
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01M—PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY
    • H01M10/00—Secondary cells; Manufacture thereof
    • H01M10/42—Methods or arrangements for servicing or maintenance of secondary cells or secondary half-cells
    • H01M10/48—Accumulators combined with arrangements for measuring, testing or indicating the condition of cells, e.g. the level or density of the electrolyte
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
    • B60L2200/00—Type of vehicles
    • B60L2200/10—Air crafts
    • 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
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/005—Testing of electric installations on transport means
    • G01R31/008—Testing of electric installations on transport means on air- or spacecraft, railway rolling stock or sea-going vessels
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
    • G01R31/385—Arrangements for measuring battery or accumulator variables
    • G01R31/386—Arrangements for measuring battery or accumulator variables using test-loads
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R31/00—Arrangements for testing electric properties; Arrangements for locating electric faults; Arrangements for electrical testing characterised by what is being tested not provided for elsewhere
    • G01R31/36—Arrangements for testing, measuring or monitoring the electrical condition of accumulators or electric batteries, e.g. capacity or state of charge [SoC]
    • G01R31/396—Acquisition or processing of data for testing or for monitoring individual cells or groups of cells within a battery

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Transportation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Chemical & Material Sciences (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Electrochemistry (AREA)
  • General Chemical & Material Sciences (AREA)
  • Control Of Electric Motors In General (AREA)
  • Hybrid Electric Vehicles (AREA)

Abstract

La présente invention concerne un procédé d’autorisation de vol d’un aéronef (1) muni d’une installation motrice hybride (10) ayant au moins un moteur thermique (15) et au moins un moteur électrique (20) relié électriquement à une source d’énergie électrique (30) comprenant plusieurs accumulateurs électriques (31). Le procédé comporte un prélèvement (STP1) au sol d’une énergie électrique ou d’une puissance électrique à prélever à partir de la source d’énergie électrique (30) pendant une durée prédéterminée et une détermination (STP2) pour les accumulateurs électriques (31) de valeurs initiales respectives d’un paramètre de fonctionnement, un calcul (STP3) d’une valeur moyenne à partir des valeurs initiales, une détermination (STP4) d’une valeur minimale parmi les valeurs initiales mesurées, une autorisation de lorsqu’une différence entre la valeur moyenne et la valeur minimale est inférieure à un seuil et une interdiction lorsque ladite différence entre la valeur moyenne et la valeur minimale est supérieure ou égale au seuil. Figure d’abrégé : figure 2
FR2212089A 2022-11-21 2022-11-21 Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique Active FR3142277B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR2212089A FR3142277B1 (fr) 2022-11-21 2022-11-21 Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique
EP23197103.7A EP4371883B1 (fr) 2022-11-21 2023-09-13 Procede d'autorisation de vol d'un aeronef ayant une installation motrice hybride munie d'au moins un moteur electrique et d'au moins un moteur thermique
US18/380,252 US12142149B2 (en) 2022-11-21 2023-10-16 Method for authorizing the flight of an aircraft having a hybrid power plant provided with at least one electric motor and at least one heat engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2212089 2022-11-21
FR2212089A FR3142277B1 (fr) 2022-11-21 2022-11-21 Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique

Publications (2)

Publication Number Publication Date
FR3142277A1 FR3142277A1 (fr) 2024-05-24
FR3142277B1 true FR3142277B1 (fr) 2024-10-18

Family

ID=85221747

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2212089A Active FR3142277B1 (fr) 2022-11-21 2022-11-21 Procédé d’autorisation de vol d’un aéronef ayant une installation motrice hybride munie d’au moins un moteur électrique et d’au moins un moteur thermique

Country Status (3)

Country Link
US (1) US12142149B2 (fr)
EP (1) EP4371883B1 (fr)
FR (1) FR3142277B1 (fr)

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8789791B2 (en) * 2008-06-10 2014-07-29 Lockheed Martin Corporation Electrical system and electrical accumulator for electrical actuation and related methods
US20180118364A1 (en) * 2016-11-03 2018-05-03 The Boeing Company System and method for augmenting a primary powerplant
CN107452989A (zh) 2017-03-20 2017-12-08 亿航智能设备（广州）有限公司 电池管理系统及具有其的飞行控制系统和飞行器
WO2020011380A1 (fr) * 2018-07-13 2020-01-16 Aerospace Holdings Inc. Système de propulsion pour aéronef à rotors multiples
FR3090576B1 (fr) * 2018-12-20 2021-09-10 Airbus Helicopters Procédé d’assistance pour aéronef monomoteur à voilure tournante lors d’une panne moteur.
CN109739253B (zh) 2019-01-28 2021-11-26 深圳市道通智能航空技术股份有限公司 一种飞行器电池监控方法、装置、电池及飞行器
US11138868B2 (en) * 2019-07-01 2021-10-05 The Boeing Company Monitor circuit for summarizing sensor data
GB2593417A (en) * 2019-10-02 2021-09-29 Advanced Mobility Res And Development Ltd Systems and methods for aircraft
US20230211886A1 (en) * 2019-11-29 2023-07-06 Vladimir Petrovich Sevastyanov Nuclear aircraft system "karavan", aircraft thrust nuclear power plant, its hybrid thermal power cycle, its maintenance system and emergency response system
US11443569B1 (en) * 2021-10-30 2022-09-13 Beta Air, Llc Systems and methods for battery management for a vehicle

Also Published As

Publication number Publication date
EP4371883A1 (fr) 2024-05-22
EP4371883C0 (fr) 2025-01-15
US20240169845A1 (en) 2024-05-23
EP4371883B1 (fr) 2025-01-15
US12142149B2 (en) 2024-11-12
FR3142277A1 (fr) 2024-05-24

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