Electromechanical actuation of primary flight control surfaces has been demonstrated by the development of an integrated rotary hinge-line dual-redundant actuation unit. The controller power level of 30 amp at 270 vdc was demonstrated. Thermal characteristics of the motor and actuator were evaluated at ambient temperatures ranging from -65 F to 250 F. (Author)


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    Electromechanical flight control actuation

    Bird, D.K. | Tema Archive | 1977


    Electromechanical Flight Control Actuation

    Bird, Daniel K. | SAE Technical Papers | 1977



    Electromechanical actuation brake device

    ZHANG MINGJUN / CHEN TONGHUI / XU FUJIAN et al. | European Patent Office | 2020

    Free access

    The Development of Electromechanical Actuation for Aircraft Systems

    White, J.A.P. | Emerald Group Publishing | 1987