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    Electrical harness

    Freier Zugriff
    FREY OLIVIER | Europäisches Patentamt | 2020

    An electrical harness including at least one upstream connector arranged to be electrically connected to a computer, at least one

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    ELECTRICAL HARNESS

    Freier Zugriff
    FREY OLIVIER | Europäisches Patentamt | 2019

    An electrical harness including at least one upstream connector arranged to be electrically connected to a computer, at least one

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    ELECTRICAL APPARATUS

    Freier Zugriff
    DUDLEY NEIL | Europäisches Patentamt | 2020

    An aircraft electrical apparatus comprises an engine starter motor control unit (1) configured to provide an AC input voltage to a

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    Electrical circuit for control of an electrical device with high integrity

    Freier Zugriff
    KARNIEWICZ ERIC / MONTOYA MICHAEL / CHARRIER NICOLAS et al. | Europäisches Patentamt | 2020

    The invention relates to: Control circuit (1) for an electrical device (2), said control circuit (1) receiving as input a discrete

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    Electrical architecture for aircraft

    Freier Zugriff
    NANEIX PHILIPPE | Europäisches Patentamt | 2024

    The invention relates to an electrical architecture (2) for an aircraft, comprising:-a first propulsion power distribution system (16

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    ELECTRICAL CIRCUIT FOR CONTROL OF AN ELECTRICAL DEVICE WITH HIGH INTEGRITY

    Freier Zugriff
    KARNIEWICZ ERIC / MONTOYA MICHAEL / CHARRIER NICOLAS et al. | Europäisches Patentamt | 2017

    The invention relates to: Control circuit (1) for an electrical device (2), said control circuit (1) receiving as input a discrete

     ...

    Control method for an electrical braking system and electrical braking system for aircraft

    Freier Zugriff
    FREY OLIVIER | Europäisches Patentamt | 2022

    A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a

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    CONTROL METHOD FOR AN ELECTRICAL BRAKING SYSTEM AND ELECTRICAL BRAKING SYSTEM FOR AIRCRAFT

    Freier Zugriff
    FREY OLIVIER | Europäisches Patentamt | 2020

    A control method of an electrical braking system for aircraft includes a plurality of electromechanical actuators capable of applying a

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    AIRCRAFT ELECTRICAL ENERGY SUPPLY NETWORK

    Freier Zugriff
    BARRACO THOMAS / KLONOWSKI THOMAS / POUMAREDE VINCENT | Europäisches Patentamt | 2022

    An electrical energy supply network of an aircraft equipped with a plurality of electrical loads to be supplied includes at least two

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    PROTECTION DEVICE FOR ELECTRICAL CABINET

    Freier Zugriff
    BOISNIER BENJAMIN / LEMASSON LOÎC / AVIGNON PHILIPPE PIERRE | Europäisches Patentamt | 2022

    A protection device for an electrical cabinet is divided into a plurality of compartments, the protection device including a rain guard

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    Electrical harness for a turbomachine

    Freier Zugriff
    MARMET ERIC MAURICE DANIEL / AUDOUX CLÉMENT PIERRE BERNARD / MACHADO VICTORIN et al. | Europäisches Patentamt | 2022

    The present invention relates to an electrical harness (1) comprising at least one first cable strand (2) and at least one second cable

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    AIRCRAFT ELECTRICAL ENERGY SUPPLY NETWORK

    Freier Zugriff
    BARRACO THOMAS / KLONOWSKI / POUMAREDE VINCENT | Europäisches Patentamt | 2021

    The invention concerns an electrical energy supply network (1) of an aircraft equipped with a plurality of electrical loads (C1, C2) to

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    APPARATUS FOR PROVIDING AN ELECTRICAL CONNECTION

    Freier Zugriff
    MARQUIS JAMES / GONIDEC PATRICK / HARDYMAN STUART et al. | Europäisches Patentamt | 2021
    comprising: a first guide provided on or in the stationary part of the structure or the movable part of the structure; a first electrical connector ...

    STATOR WINDING FOR AN ELECTRICAL MACHINE

    Freier Zugriff
    FLOWER PAUL DAVID | Europäisches Patentamt | 2020

    A novel method of manufacture and an improved construction of windings of a stator of an electrical machine are provided, which minimise

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    Protection device for electrical cabinet in aircraft

    Freier Zugriff
    BOISNIER BENJAMIN / LEMASSON LOÎC / AVIGNON PHILIPPE PIERRE | Europäisches Patentamt | 2024

    A protection device for an electrical cabinet is divided into a plurality of compartments, the protection device including a rain guard

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    SYSTEM FOR CONTROLLING AN AIRCRAFT ELECTRICAL NETWORK

    Freier Zugriff
    CARRE NICOLAS / DELBOSC PHILIPPE | Europäisches Patentamt | 2022
    -generator and a second propulsion assembly having at least one right-hand starter-generator as well as other electrical motors, the system including ...

    SYSTEM FOR CONTROLLING AN AIRCRAFT ELECTRICAL NETWORK

    Freier Zugriff
    CARRE NICOLAS / DELBOSC PHILIPPE | Europäisches Patentamt | 2021

    System for controlling an aircraft electrical network comprising at least a first propulsion assembly having at least one left-hand

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    Unit for generating non-propulsive electrical power

    Freier Zugriff
    VAILLANT STEPHANE RICHARD DOMINIQUE / FAUCHER MICKAEL / TURPIN CHRISTOPHE | Europäisches Patentamt | 2021

    A unit (1′, 10′, 100′) for generating non-propulsive electrical power for use on board an aircraft, the unit (1′, 10′, 100′) comprising

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    Electrical power distribution assembly for an aircraft

    Freier Zugriff
    ROQUES SERGE THIERRY / AVIGNON PHILIPPE PIERRE / BLINEAU JEAN-MARC | Europäisches Patentamt | 2021

    An electrical power distribution assembly for an airplane, the assembly including an electric switch device for placing in a Karman

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    Method of controlling an electrical taxiing system

    Freier Zugriff
    GORCE CLÉMENT | Europäisches Patentamt | 2019

    A control method for controlling an electrical taxiing system adapted to moving an aircraft while it is taxiing, the method comprising

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