A secondary flight control system is provided. The secondary flight control system comprising: a first flight control surface system (47); a second flight control surface system (57); and a power distribution unit (150a) operably connected to the first flight control surface system and the second flight control surface system, wherein the power distribution unit is configured to generate torque to actuate the first flight control surface system and the second flight control surface system.


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    Title :

    CONTROL OF MULTIPLE FLIGHT CONTROL SURFACE SYSTEMS USING SINGLE POWER DRIVE UNIT


    Additional title:

    STEUERUNG VON MEHREREN FLUGSTEUERUNGSFLÄCHENSYSTEMEN UNTER VERWENDUNG EINER EINZIGEN KRAFTANTRIEBSEINHEIT
    COMMANDE DE SYSTÈMES DE SURFACES DE COMMANDE DE VOL MULTIPLES UTILISANT UNE SEULE UNITÉ D'ENTRAÎNEMENT ÉLECTRIQUE


    Contributors:

    Publication date :

    2022-12-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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