Single valve braking system having anti-skid control
AssigneeGoodyear Aerospace Corporation
InventorEdgar J. Ruof
Life of this patent
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AssigneeGoodyear Aerospace Corporation
InventorEdgar J. Ruof
Estimating the term…
An anti-skid and brake control system for use on an aircraft wherein the output signals from standard anti-skid circuitry are combined with the signals from a brake pedal transducer to create braking signals. The braking signals are applied to current controlled hydraulic valves for regulation of the application and release of brake pressure. The brakes utilized are dual cavity brakes with corresponding cavities of all brakes being interconnected to the same hydraulic line. Shut-off valves are interposed in the hydraulic lines and are operative to enable the brake valves to regulate brake pressure when either brake pedal of the aircraft has been depressed a fixed amount. Biasing circuitry is presented to affect the brake signal in such a manner as to overcome a dead band within the response characteristics of the brake valves utilized.
An anti-skid system and brake control device for use on a vehicle having at least two wheels and having anti-skid circuitry connected to brakes on each of said wheels for producing anti-skid signals indicative of skidding activity and further having brake pedals connected to brake pedal transducers for producing pedal force signals indicative of the degree of brake pedal depression, comprising:
A brake control system for use on an aircraft having at least two wheels, one on each side of the aircraft, each wheel having an electrically controlled hydraulic valve connected to a brake for such wheel, all wheels on the same side of the aircraft being controllable by the same brake pedal and each wheel having anti-skid circuitry associated therewith to produce anti-skid signals indicative of skidding activity of the wheel comprising:
Dependencies are inferred from the claim text.