Method to reduce carbon brake wear through residual brake force

Fluid-pressure and analogous brake systems – Speed-controlled – Automatic braking including speed governor or hydraulic...

Reexamination Certificate

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Details

C303S020000

Reexamination Certificate

active

07735938

ABSTRACT:
The method for reducing aircraft carbon brake wear involves monitoring the commanded initiation of braking, and setting a residual brake clamping force to a predetermined minimum residual brake clamping force, which is maintained following the commanded initiation of braking to prevent release of braking during taxiing of the aircraft. The minimum residual brake clamping force is applied despite a commanded release of braking until at least one predetermined control logic condition occurs.

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