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Accession Number:
AD0918237
Title:
Test and Development of Flight Control Actuation System Components for Military Aircraft
Corporate Author:
HYDRAULIC RESEARCH AND MFG CO VALENCIA CA
Report Date:
1972-02-01
Abstract:
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.
Descriptive Note:
Final rept. 8 Dec 1970-3 Nov 1971
Pages:
0232
Contract Number:
F33615-71-C-1124
File Size:
11.82MB
