A design outline is given of the actuator that rotates the engine and rotor nacelles on the V-22 aircraft. The actuator comprises a two-stage telescopic ballscrew that is driven either hydraulically from one end or electrically from the other. Requirements for structural redundancy, least weight, operation after any single failure and performance at low temperatures are shown to influence the choice of actuator configuration and the design of assemblies.


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    Title :

    V-22 Nacelle Conversion Actuator


    Contributors:
    White, G (author)


    Publication date :

    1993-01-01


    Size :

    12 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    V-22 nacelle conversion actuator

    White, G. | Tema Archive | 1993


    V-22 nacelle conversion actuator

    White, G. | Online Contents | 1993


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