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.
Series of Development and Test Tasks for Flight Control Design Techniques
1973
224 pages
Report
No indication
English
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