The following research tasks were conducted: Determine methods and procedures for measuring aircraft flight control actuator performance characteristics; design and development of an electromechanical hydraulic branch isolation device that may be applied to any flight control actuator; investigate performance characteristics of aircraft hydraulic oil filters in an induced vibration environment; develop new visual techniques to investigate hydraulic fluid contamination and filter performance evaluations; improve the test capability of a general purpose actuator test rig by developing a new load actuator and associated instrumentation; design and preliminary analysis of an improved actuator test rig reaction frame; and evaluate an F-4 Stabilator actuator, the Vickers, Inc. Integrated Servo Pump actuator, and the Bendix Dynavector Pneumatic Rotary actuator.


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    Title :

    Series of Development and Test Tasks for Flight Control Design Techniques


    Contributors:

    Publication date :

    1973


    Size :

    224 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English






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