Method and system to increase electric brake clamping force accuracy

1. In a method for controlling electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes when the aircraft is taxiing, the method including the step of providing a plurality of brake actuators of each wheel brake with brake clamping force commands, the improvement in the method comprising:

providing a first portion of the 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, and 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;

monitoring commanded initiation of braking of any of the plurality of wheel brakes of the aircraft;

setting a residual brake clamping force to a predetermined minimum residual brake clamping force for the plurality of wheel brakes in response to said commanded initiation of braking of any of the plurality of wheel brakes;

actuating said first portion of electric brake actuators to apply said predetermined minimum residual brake clamping force once wheel braking is commanded and maintaining said predetermined minimum residual brake clamping force despite a commanded release of braking of any of the plurality of wheel brakes;

discontinuing applying said predetermined minimum residual brake clamping force in response to at least one control logic condition;

determining an average wheel speed; and

comparing said average wheel speed with a predetermined wheel speed threshold, and wherein said at least one control logic condition comprises said average wheel speed being below said predetermined wheel speed threshold.

2. The method of claim 1 , further comprising the step of actuating said second portion of electric brake actuators only when the commanded braking force is in the second high range of brake clamping force.

3. The method of claim 1 , wherein said aircraft has left and right landing gear, and said step of determining an average wheel speed comprises determining an average wheel speed of the left landing gear and an average wheel speed of the right landing independently, comparing said average wheel speeds of the left and right landing gear, and comparing the lesser of the average wheel speeds of the left and right landing gear with said predetermined wheel speed threshold.

4. The method of claim 1 , further comprising the step of detecting wheel speed acceleration, and comparing said wheel speed acceleration with a predetermined acceleration threshold, and wherein said at least one control logic condition comprises said wheel speed acceleration exceeding said acceleration threshold.

5. The method of claim 1 , further comprising monitoring temperature of said plurality of wheel brakes, and comparing said temperature of said plurality of wheel brakes with a temperature threshold, and wherein said at least one control logic condition comprises said temperature of said plurality of wheel brakes exceeding said temperature threshold.

6. The method of claim 1 , further comprising determining distance rolled with said predetermined minimum residual brake clamping force applied, comparing said distance rolled with a predetermined distance threshold, and wherein said at least one control logic condition comprises said distance rolled exceeding said predetermined distance threshold.

7. In a method for controlling electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes when the aircraft is taxiing, and the aircraft having at least one engine thrust lever, the method including the step of providing a plurality of brake actuators of each wheel brake with brake clamping force commands, the improvement in the method comprising;

providing a first portion of the 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, and 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;

monitoring commanded initiation of braking of any of the plurality of wheel brakes of the aircraft;

setting a residual brake clamping force to a predetermined minimum residual brake clamping force for the plurality of wheel brakes in response to said commanded initiation of braking of any of the plurality of wheel brakes;

actuating said first portion of electric brake actuators to apply said predetermined minimum residual brake clamping force once wheel braking is commanded and maintaining said predetermined minimum residual brake clamping force despite a commanded release of braking of any of the plurality of wheel brakes;

monitoring engine thrust lever position; and

discontinuing applying said predetermined minimum residual brake clamping force in response to at least one control logic condition, and wherein said at least one control logic condition comprises said at least one engine thrust lever being in an advanced position.

8. The method of claim 7 , further comprising the step of detecting wheel speed acceleration, and comparing said wheel speed acceleration with a predetermined acceleration threshold, and wherein said at least one control logic condition comprises said wheel speed acceleration exceeding said acceleration threshold.

9. The method of claim 7 , further comprising monitoring temperature of said plurality of wheel brakes, and comparing said temperature of said plurality of wheel brakes with a temperature threshold, and wherein said at least one control logic condition comprises said temperature of said plurality of wheel brakes exceeding said temperature threshold.

10. The method of claim 7 , further comprising determining distance rolled with said predetermined minimum residual brake clamping force applied, and comparing said distance rolled with a predetermined distance threshold, and wherein said at least one control logic condition comprises said distance rolled exceeding said predetermined distance threshold.

11. In a system for increasing accuracy of clamping force of electric aircraft carbon brakes of an aircraft having a plurality of wheels and a corresponding plurality of wheel brakes for the plurality of wheels to reduce brake wear when the aircraft is taxiing, the system including a plurality of brake actuators of each wheel brake, the improvement in the system comprising:

a first portion of a plurality of electric brake actuators of each brake having a first range of low brake clamping force responsive to low brake clamping force commands;

a second portion of a plurality of electric brake actuators of each brake having a second range of high brake clamping force responsive to high brake clamping force commands;

means for monitoring commanded initiation of braking of any of the plurality of wheel brakes of the aircraft;

means for setting a residual brake clamping force to a predetermined minimum residual brake clamping force for the plurality of wheel brakes in response to said commanded initiation of braking of any of the plurality of wheel brakes; and

means for actuating said first portion of electric brake actuators to apply said predetermined minimum residual brake clamping force once wheel braking is commanded and maintaining said predetermined minimum residual brake clamping force despite a commanded release of braking of any of the plurality of wheel brakes;

means for discontinuing applying said predetermined minimum residual brake clamping force in response to at least one control logic condition; and

means for determining an average wheel speed and comparing said average wheel speed with a predetermined wheel speed threshold, and wherein said at least one control logic condition comprises said average wheel speed being below said predetermined wheel speed threshold.

12. The system of claim 11 , further comprising means for actuating said second portion of electric brake actuators only when the commanded braking force is in the second high range of brake clamping force.

13. The system of claim 11 , further comprising means for detecting wheel speed acceleration, and means for comparing said wheel speed acceleration with a predetermined acceleration threshold, and wherein said at least one control logic condition comprises said wheel speed acceleration exceeding said acceleration threshold.

14. The system of claim 11 , further comprising means for monitoring temperature of said plurality of wheel brakes, and means for comparing said temperature of said plurality of wheel brakes with a temperature threshold, and wherein said at least one control logic condition comprises said temperature of said plurality of wheel brakes exceeding said temperature threshold.

15. The system of claim 11 , further comprising means for determining distance rolled with said predetermined minimum residual brake clamping force applied, and means for comparing said distance rolled with a predetermined distance threshold, and wherein said at least one control logic condition comprises said distance rolled exceeding said predetermined distance threshold.