A thrust reverser device for an aircraft includes at least two thrust reversers, and each of them includes a movable cowl movably actuated by an actuator driven by an electric motor. The electric motor is powered by a single power-conversion module including at least one autotransformer which is supplied with an alternating electric voltage and connected to at least one rectifier stage converting the alternating electric voltage into a direct voltage. The rectifier stage is connected to a current balancing stage and a current smoothing stage, supplying with the direct voltage the electric motor of the electric actuator of the movable cowl.


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    Title :

    Thrust-reversal device for an aircraft including at least two thrust reversers


    Contributors:

    Publication date :

    2017-03-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Thrust-reversal device for an aircraft including at least two thrust reversers

    MAALIOUNE HAKIM / NOURRISSON ALAIN | European Patent Office | 2015

    Free access

    THRUST REVERSERS FOR JET AIRCRAFT

    STIMLER, F. J. / McDERMOTT, J. F. | SAE Technical Papers | 1957


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    Stimler, F.J. / McDermott, J.F. | Engineering Index Backfile | 1957


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