Patent ID: 9139292
Filing Date: 2015-09-22
Classification: B60T,B64C

Abstract:
1. A system comprising: a first electromechanical brake actuator controller; a second electromechanical brake actuator controller; a first communication channel in communication with the first electromechanical brake actuator controller and the second electromechanical brake actuator controller; a first electromechanical brake actuator in electrical communication with the first electromechanical brake actuator controller and configured to receive a first commanded braking force from the first electromechanical brake actuator controller; a second electromechanical brake actuator in electrical communication with the second electromechanical brake actuator controller; wherein the first electromechanical brake actuator and the second electromechanical brake actuator are associated with a plate; wherein the first electromechanical brake actuator controller is configured to receive observed aircraft deceleration information and determine whether additional braking force is needed; wherein the first electromechanical brake actuator controller transmits a command for increased braking force in response to a determination that additional braking force is needed to the second electromechanical brake actuator controller via the first communication channel; and wherein the second electromechanical brake actuator controller commands the second electromechanical brake actuator with a second commanded braking force responsive to the command from the first electromechanical brake actuator controller, wherein the first commanded braking force is different from the second commanded braking force.