Aircraft brake system testing methods

Patent metadata

Field	Value
Publication number	US-9714019-B2
Application number	US-201514929031-A
Country	US
Kind code	B2
Filing date	Oct 30, 2015
Priority date	May 29, 2014
Publication date	Jul 25, 2017
Grant date	Jul 25, 2017

Abstract

Methods for testing the operation of an aircraft braking system utilize the steps of applying a predetermined electrical energy level to an electromechanical actuator attached to a brake assembly, followed by discontinuing electrical energy to the electromechanical actuator. In some test methods, an actuation level of the electromechanical actuator is determined and used to evaluate braking performance. In other tests, a voltage generated by an electric motor in an actuator is measured and used to evaluate braking performance.

First claim

What is claimed is:

1. A method for testing the operation of an aircraft braking system comprising:
applying a predetermined electrical energy level to an electromechanical actuator attached to a brake assembly, wherein the brake assembly comprises a brake stack;
discontinuing electrical energy to the electromechanical actuator;
after discontinuing electrical energy to the electromechanical actuator, measuring a voltage from a motor of the electromechanical actuator; and
evaluating braking performance by comparing the voltage from the motor of the electromechanical actuator after discontinuing electrical energy to the electromechanical actuator to a predetermined desired voltage;
wherein the measuring the voltage from the motor of the electromechanical actuator comprises receiving a voltage signal from the motor of the electromechanical actuator operating as a generator, wherein the a difference between the voltage produced by the motor and the predetermined value between about 1 volts and 1000 volts indicates a braking performance issue.

2. The testing method of claim 1 , wherein the braking system comprises four electromechanical actuators.

3. The testing method of claim 2 , wherein each of the electromechanical actuators are tested independently from one another.

4. The testing method of claim 2 , wherein two or more of the electromechanical actuator are tested simultaneously.

5. The testing method of claim 4 , wherein the evaluating the braking performance comprises comparing the voltage produced by the motor of the electromechanical actuator to a predetermined value.

6. The testing method of claim 1 , wherein the testing method is performed on an aircraft as it is taxiing or parked.

Assignees

• Goodrich Corp

Inventors

• Cahill Eric
• Georgin Marc

Classifications

• B60T2270/406

  Test-mode; Self-diagnosis · CPC title

• B64C25/44

  Actuating mechanisms · CPC title

• B60T8/885

  using electrical circuitry · CPC title

• B60T8/1703 Primary

  for aircrafts · CPC title

• B64C25/42

  Arrangement or adaptation of brakes · CPC title