An actuator has been developed and qualified with all loop-closure and redundancy management functions covered by an electronic package physically located on the actuator manifold assembly. The actuator meets or exceeds all Original Equipment Manufacturer (OEM) requirements of the F/A-18 aileron servocylinder design with the single restriction of 99 °C (210 °F) maximum oil temperature. While the actuator has performed well at temperatures in excess of 135 °C (275 °F), present MIL-SPEC derating for electronics limit the allowable operating range. The basic design offers potential advantages in the areas of weight, maintainability, self-diagnostics, and ease of integration.


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    Titel :

    Second Generation Smart Actuator


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Deller, R. W. (Autor:in)

    Kongress:

    Aerospace Technology Conference and Exposition ; 1993



    Erscheinungsdatum :

    01.09.1993




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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