A high-lift actuation system for differentially actuating a plurality of high-lift surfaces of an aircraft is disclosed. An exemplary high-lift actuation system includes a plurality of independent drive devices for individually actuating the plurality of high-lift surfaces. The independent drive devices may include a power drive unit (PDU) arranged between an inboard actuator and an outboard actuator of a respective high-lift surface and an interconnecting driveline. The PDU of at least one independent drive device may include two motors having a respective motor output coupled together in a torque summing arrangement. A controller may be implemented with two independent control channels respectively coupled to one of the two motors.


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    Titel :

    HIGH-LIFT ACTUATION SYSTEM HAVING INDEPENDENT ACTUATION CONTROL


    Weitere Titelangaben:

    HOCHAUFTRIEBSBETÄTIGUNGSSYSTEM MIT UNABHÄNGIGER BETÄTIGUNGSSTEUERUNG
    SYSTÈME D'ACTIONNEMENT HYPERSUSTENTATEUR À COMMANDE D'ACTIONNEMENT INDÉPENDANTE


    Beteiligte:
    TZABARI EHUD (Autor:in)

    Erscheinungsdatum :

    2020-05-20


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    High-lift actuation system having independent actuation control

    TZABARI EHUD | Europäisches Patentamt | 2020

    Freier Zugriff

    HIGH-LIFT ACTUATION SYSTEM HAVING INDEPENDENT ACTUATION CONTROL

    TZABARI EHUD | Europäisches Patentamt | 2020

    Freier Zugriff

    HIGH-LIFT ACTUATION SYSTEM HAVING INDEPENDENT ACTUATION CONTROL

    TZABARI EHUD | Europäisches Patentamt | 2020

    Freier Zugriff