Concept and technique for solving problems associated with prediction and control of flight component failures which are attributed to contamination of power transmission fluid are presented; systems and applications considered are hydraulic type flight control servo actuators as used on B-58 Bomber, Century series type fighter aircraft, missiles, etc; technique assumes that these failures are probabilistic; mathematical models are established and comparisons made between calculated and measured values of contamination in system to determine degree of acceptability of fluid.
Criteria for contamination level in flight control systems
SAE -- Paper
SAE Meeting ; 1967 Hydraulic equipment
1967
18 pages
Aufsatz (Konferenz)
Englisch
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Criteria for Contamination Level in Flight Control Systems
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