Basic difference of systems is that in Skid Warning brakes are controlled by pilot, while Automatic Anti-Skid releases brake pressure automatically by means of hydraulic valve; with either system, d-c generator, driven by wheel, senses changes in wheel rotation; by connecting generator through electrical circuitry, deviation of wheel from normal deceleration is sensed; sequence of operations; detailed circuitry of systems using same sensing, power, and locked wheel prevention circuits.
Two methods of aircraft skid control
Soc Automotive Engrs -- Paper
Society of Automotive Engineers -- Meeting ; 1958 Landing
1958
10 pages
Conference paper
English
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TWO METHODS OF AIRCRAFT SKID CONTROL
SAE Technical Papers | 1958
|Anti-Skid Aircraft Braking Systems
NTIS | 1977
|