Test and Development of Flight Control Actuation System Components for Military Aircraft.

摘要

Test and development activities were conducted in the following nine areas: (1) Evaluation of a breadboard multiplexing system driving a fly-by-wire actuator; (2) Evaluate actuation system of six-degree of freedom motion base; (3) Evaluation of general purpose actuator test stand;; (4) Various design concepts were explored for the improvement of branch isolation techniques; (5) Evaluation of a Vickers Inc. integrated servopump actuator package; (6) Investigation of limit cycle characteristics of a General Electric 666A actuator; (7) Literature search and recommendation for a laboratory contamination measurement system choice; (8) Fabrication of a portable flow measurement stand and (9) Design and fabrication of a transducer range and balance panel.