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Antiskid brake control for aircraft

  • US 4,327,948 A
  • Filed: 08/14/1978
  • Issued: 05/04/1982
  • Est. Priority Date: 08/14/1978
  • Status: Expired due to Term
First Claim
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1. An antiskid control circuit for aircraft having an antiskid valve for controlling the braking of the wheels thereof by regulating the application of brake pressure, and a transducer for each wheel producing wheel speed signals indicative of the instantaneous rotational speed of the associated wheel, comprising:

  • deceleration detection means connected to and receiving the wheel speed signals from the transducers for presenting an output signal when the rate of deceleration of a wheel exceeds a predetermined threshold;

    a valve driver interconnected between said deceleration detection means and the antiskid valve and responsive to said output signals to release brake pressure;

    a modulator interconnected between said deceleration detection means and said valve driver, responsive to said output signal to further release brake pressure and then increase brake pressure at a predetermined rate following said release; and

    wherein said valve driver includes gain control circuitry responsive to said deceleration detection means and said modulator to modify the effect of the modulator and deceleration detection means on the antiskid valve as a function of the amplitude and frequency of occurrence of said output signal.

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