All classes of airplane actuation systems have unique system level characteristics. This paper discusses key systems aspects of electric T/R actuation such as safety, power, controls, and maintainability, from an large airplane perspective, principally by comparing electric T/R actuation systems to equivalent hydraulic and pneumatic actuation. Enabling technology with which to implement system level requirements are discussed. The system issues are presented for a typical large airplane cascade T/R.


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    Title :

    Electric Thrust Reverser Actuation Systems


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    World Aviation Congress & Exposition ; 2002



    Publication date :

    2002-11-05




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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