This is a report of design study on Dual-Mode Dynavector Actuator for use as control-surface actuator on aircraft. Actuator operates on pneumatic power and /or electric power. Operation within specifications continues despite loss of either electric or pneumatic power, providing survivability feature for aircraft. (Author)


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    Title :

    Advanced Flight Control Actuation System (AFCAS-E/P). Feasibility Investigation of an Electro/Pneumatic Dual Power Driven Concept


    Contributors:
    R. E. Feucht (author) / R. W. Presley (author) / P. Forman (author) / R. Krehely (author)

    Publication date :

    1978


    Size :

    118 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English