Patent ID: 8312973

Claim:
A system for controlling electric carbon brakes of an aircraft when the aircraft is taxiing, the aircraft having left and right landing gear with a plurality of wheels, and a corresponding plurality of wheel brakes configured to be actuated by commanded initiation of braking by low and high brake clamping force commands, the system comprising: a first portion of a plurality of electric brake actuators of each wheel brake with a first range of low brake clamping force responsive to low brake clamping force commands; a second portion of the plurality of electric brake actuators of each brake with a second range of high brake clamping force responsive to high brake clamping force commands, said second range of high brake clamping force being greater than said first range of low brake clamping force; a plurality of wheel speed monitors configured to monitor a wheel speed of each of the wheels of the left and right landing gear, respectively; a brake actuation controller configured to monitor commanded initiation of braking of any of the plurality of wheel brakes of the aircraft and to apply a predetermined minimum residual brake clamping force with said first portion of a plurality of electric brake actuators for the plurality of wheel brakes in response to the commanded initiation of braking of any of the plurality of wheel brakes, said brake actuation controller being configured to determine a left side average wheel speed of the wheels of the left landing gear and a right side average wheel speed of the wheels of the right landing gear independently of the left side average wheel speed, responsive to said plurality of wheel speed monitors, to compare said left side average wheel speed with a first predetermined wheel speed threshold, to compare said right side average wheel speed with said first predetermined wheel speed threshold, to discontinue applying said predetermined minimum residual brake clamping force of said first portion of a plurality of electric brake actuators when either of said left side average wheel speed and right side average wheel speed is less than said first predetermined wheel speed threshold, to apply said second range of high brake clamping force only when the commanded braking force is in the second high range of brake clamping force, and to discontinue applying said predetermined minimum residual brake clamping force of said first portion of a plurality of electric brake actuators when the commanded braking force is less than the second high range of brake clamping force.