PL4169142T3 - Instalacja elektromechaniczna statku powietrznego z turbogeneratorem, sposób wyłączania awaryjnego turbogeneratora statku powietrznego oraz odpowiadający mu program komputerowy - Google Patents

Instalacja elektromechaniczna statku powietrznego z turbogeneratorem, sposób wyłączania awaryjnego turbogeneratora statku powietrznego oraz odpowiadający mu program komputerowy

Info

Publication number
PL4169142T3
PL4169142T3 PL21737111.1T PL21737111T PL4169142T3 PL 4169142 T3 PL4169142 T3 PL 4169142T3 PL 21737111 T PL21737111 T PL 21737111T PL 4169142 T3 PL4169142 T3 PL 4169142T3
Authority
PL
Poland
Prior art keywords
turbogenerator
aicraft
aircraft
computer program
emergency stop
Prior art date
Application number
PL21737111.1T
Other languages
English (en)
Inventor
Romain Jean Gilbert THIRIET
David Bernard Martin LEMAY
Original Assignee
Safran Helicopter Engines
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 Safran Helicopter Engines filed Critical Safran Helicopter Engines
Publication of PL4169142T3 publication Critical patent/PL4169142T3/pl

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00—Circuit arrangements for mains or distribution networks not specified as AC or DC; Circuit arrangements for mains or distribution networks combining AC and DC sections or sub-networks
    • 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
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/16—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants
    • B64D31/18—Power plant control systems; Arrangement of power plant control systems in aircraft for electric power plants for hybrid-electric power plants
    • 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
    • B64D41/00—Power installations for auxiliary purposes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/14—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to other specific conditions
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02H—EMERGENCY PROTECTIVE CIRCUIT ARRANGEMENTS
    • H02H7/00—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions
    • H02H7/06—Emergency protective circuit arrangements specially adapted for specific types of electric machines or apparatus or for sectionalised protection of cable or line systems, and effecting automatic switching in the event of an undesired change from normal working conditions for dynamo-electric generators; for synchronous capacitors
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P9/00—Arrangements for controlling electric generators for the purpose of obtaining a desired output
    • H02P9/48—Arrangements for obtaining a constant output value at varying speed of the generator, e.g. on vehicle
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/10—Adaptations for driving, or combinations with, electric generators
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • F05D2220/768—Application in combination with an electrical generator equipped with permanent magnets
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—ELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00—Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32—Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2101/00—Special adaptation of control arrangements for generators
    • H02P2101/30—Special adaptation of control arrangements for generators for aircraft
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
    • H02P2103/00—Controlling arrangements characterised by the type of generator
    • H02P2103/20—Controlling arrangements characterised by the type of generator of the synchronous type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Eletrric Generators (AREA)
  • Control Of Turbines (AREA)
PL21737111.1T 2020-06-17 2021-06-14 Instalacja elektromechaniczna statku powietrznego z turbogeneratorem, sposób wyłączania awaryjnego turbogeneratora statku powietrznego oraz odpowiadający mu program komputerowy PL4169142T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2006328A FR3111751B1 (fr) 2020-06-17 2020-06-17 Installation electromecanique d’aeronef avec turbogenerateur, procede d’arret d’urgence d’un turbogenerateur d’aeronef et programme d’ordinateur correspondant
PCT/FR2021/051055 WO2021255371A1 (fr) 2020-06-17 2021-06-14 Installation electromecanique d'aeronef avec turbogenerateur, procede d'arret d'urgence d'un turbogenerateur d'aeronef et programme d'ordinateur correspondant

Publications (1)

Publication Number Publication Date
PL4169142T3 true PL4169142T3 (pl) 2024-05-06

Family

ID=72356192

Family Applications (1)

Application Number Title Priority Date Filing Date
PL21737111.1T PL4169142T3 (pl) 2020-06-17 2021-06-14 Instalacja elektromechaniczna statku powietrznego z turbogeneratorem, sposób wyłączania awaryjnego turbogeneratora statku powietrznego oraz odpowiadający mu program komputerowy

Country Status (7)

Country Link
US (1) US20230138626A1 (pl)
EP (1) EP4169142B1 (pl)
CN (1) CN115699499A (pl)
CA (1) CA3182186A1 (pl)
FR (1) FR3111751B1 (pl)
PL (1) PL4169142T3 (pl)
WO (1) WO2021255371A1 (pl)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3149042B1 (fr) * 2023-05-23 2025-10-10 Safran Helicopter Engines Procede d’arret d’une turbomachine d’aeronef en cas d’incendie dans le compartiment de la turbomachine

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7583063B2 (en) * 2003-05-27 2009-09-01 Pratt & Whitney Canada Corp. Architecture for electric machine
US7876542B2 (en) * 2007-08-16 2011-01-25 Hamilton Sundstrand Corporation Generator for gas turbine engine having DC bus fault short circuit control using a battery
US8237416B2 (en) * 2008-12-09 2012-08-07 Hamilton Sundstrand Corporation More electric engine with regulated permanent magnet machines
GB0921323D0 (en) * 2009-12-07 2010-01-20 Rolls Royce Plc An electrical machine
US9698593B2 (en) * 2012-11-20 2017-07-04 Vestas Wind Systems A/S Methods and systems for reducing the impact of a generator short circuit in a wind turbine
US10006375B1 (en) * 2017-07-11 2018-06-26 General Electric Company Propulsion system for an aircraft
DK3522362T3 (da) * 2018-02-01 2024-03-04 Siemens Gamesa Renewable Energy As Styring af en elektrisk permanentmagnetmaskine med multiviklingssæt
FR3084340B1 (fr) * 2018-07-27 2022-05-06 Safran Systeme de generation de puissance electrique pour aeronef

Also Published As

Publication number Publication date
EP4169142B1 (fr) 2024-02-21
EP4169142A1 (fr) 2023-04-26
CN115699499A (zh) 2023-02-03
FR3111751B1 (fr) 2022-06-03
WO2021255371A1 (fr) 2021-12-23
US20230138626A1 (en) 2023-05-04
FR3111751A1 (fr) 2021-12-24
CA3182186A1 (en) 2021-12-23

Similar Documents

Publication Publication Date Title
GB202003498D0 (en) Systems, arrangements, structures and methods for aircraft
PL3626627T3 (pl) Oparty na modelu układ sterowania i sposób dla silnika turbośmigłowego
GB201814777D0 (en) System and method for aircraft contaminant monitoring
BR112012029302A2 (pt) proteção de ferimento
MX345818B (es) Método para realizar pruebas a múltiples dispositivos de protección distribuidos espacialmente de una red de suministro de energía y sistema de prueba correspondiente.
SG10201807209VA (en) Method and system for designing aircraft
WO2012130244A3 (en) Wind turbine control system with decentralized voting
ZA201902169B (en) Simulation method and system for helicopter flight simulation
IL288179A (en) Aircraft retrieval system and method
GB202003970D0 (en) Aircraft fuel system monitoring
EP3866171A4 (en) PREDICT MANAGEMENT SYSTEM, PREDICT MANAGEMENT METHOD, DATA STRUCTURE, PREDICT MANAGEMENT DEVICE AND PREDICT EXECUTION DEVICE
GB201908097D0 (en) Interface arrangement, computer system and method for assembling an interface arrangement
WO2015015262A8 (en) Method for attachment of a pre-assembled powerplant and pylon assembly to an aircraft
GB202102720D0 (en) Magnetic braking system and method for downhole turbine assemblies
GB2571686B (en) System and method for analyzing and associating elements of a computer system by shared characteristics
EP4191076A4 (en) CYLINDER FAILURE PREDICTION SYSTEM AND METHOD, AND CYLINDER FAILURE INSPECTION SYSTEM AND METHOD
GB202106173D0 (en) Aircraft landing event system and method
EP3045228B8 (de) Mikroflotationsanlage mit einer Entspannungsventilanordnung und Verfahren zum Betreiben einer Mikroflotationsanlage
GB2564242B (en) A vehicle control system, method and computer program for a vehicle control multilayer architecture
GB2619896B (en) Actuator, method and system
GB202019178D0 (en) Environment information management system, environment information management method and environment information management program
EP3682104A4 (en) PRESSURIZED FUEL SYSTEM FOR AN ENGINE AND METHOD OF OPERATING A PRESSURIZED FUEL SYSTEM FOR AN ENGINE
GB201819989D0 (en) Fan assembly, corresponding turbofan engine and method of controlling a clearance gap
EP3779813A4 (en) FUTURE PREDICTION SIMULATION DEVICE, PROCESS AND COMPUTER PROGRAM
GB202106172D0 (en) Aircraft landing event system and method