Harry K. Winters - South Bend IN Warren D. Chambers - South Bend IN
Assignee:
The Bendix Corporation - Southfield MI
International Classification:
B60T 812
US Classification:
188181T
Abstract:
In an aircraft multiple disc brake assembly, an excessive total brake torque can be experienced during favorable, dry, conditions. To limit the brake torque to a predetermined maximum, the plurality of conventional brake piston assemblies are modified to provide a pressure responsive surface area which is in an opposing relationship to the braking force. When a predetermined amount of braking torque is experienced, conventional electronics employing strain gauge sensors control a solenoid valve to vent pressurized brake fluid to the opposing surface area thereby reducing the braking force and limiting the total braking torque experienced by the brake assembly to a predetermined maximum amount. The brake pressure is not affected by this system.
Harry Winters (1940-1944), Twyla Finch (1980-1984), Mac Houlihan (1967-1971), Rachel White (1989-1993), Phillip England (1960-1964), Bill Turk (1980-1981)