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Accession Number:
AD0623111
Title:
EVALUATION OF A MECHANICAL SERVOACTUATOR FOR FLIGHT CONTROL SYSTEMS
Corporate Author:
LOCKHEED-CALIFORNIA CO BURBANK
Report Date:
1965-10-01
Abstract:
A prototype mechanical servo-actuator was tested under simulated loads to determine its suitability for use in powering flight control systems for helicopters. Tests included frequency response, step response, threshold, hysteresis, endurance, and emergency operation, and were compared with similar tests of a typical hydraulic servo. Recommendations are made regarding design changes for further investigation.
Descriptive Note:
Technical rept. for Jul 1964-Feb 1965
Supplementary Note:
Prepared in cooperation with Curtiss Div., Curtiss-Wright Corp. DOI: 10.21236/AD0623111
Pages:
0095
Distribution Statement:
Approved for public release; distribution is unlimited.
Contract Number:
DA-44-177-AMC-232(T)
File Size:
8.95MB
