Series of Development & Test Tasks for Flight Control Design Techniques

摘要

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.