Systems and methods for brake failure detection using retract braking

1. A system for detecting aircraft brake failure using retract braking, comprising:

a landing gear comprising:

a wheel;

a brake coupled to the wheel; and

a wheel sensor coupled to the wheel;

a brake controller coupled to the brake and the wheel sensor;

a tangible, non-transitory memory configured to communicate with the brake controller, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the brake controller, cause the brake controller to perform operations comprising:

receiving, by the brake controller, a begin retract braking signal;

commanding, by the brake controller, the brake to apply a braking force to the wheel;

receiving, by the brake controller, data from the wheel sensor;

calculating, by the brake controller, a wheel speed characteristic for the wheel based on the data from the wheel sensor; and

determining, by the brake controller, whether the wheel speed characteristic indicates a failure of the brake;

a landing gear controller coupled to the landing gear and the brake controller, wherein the landing gear controller is configured to send the begin retract braking signal to the brake controller;

a weight on wheels sensor coupled to the landing gear, wherein the weight on wheels sensor is configured to send a weight off wheels signal to the landing gear controller;

a pilot gear handle coupled to the landing gear controller, wherein the pilot gear handle is configured to send a gear handle up signal to the landing gear controller, the gear handle up signal indicating the pilot gear handle is in a landing gear up position; and

a landing gear lock coupled to the landing gear, wherein the landing gear lock is configured to send a gear unlocked signal to the landing gear controller, the gear unlocked signal indicating the landing gear is in an unlocked position, and wherein the landing gear controller is configured to send the begin retract braking signal to the brake controller in response to receiving the weight off wheels signal and at least one of the gear handle up signal or the gear unlocked signal.

2. The system of claim 1 , further comprising a brake sensor coupled to the brake, wherein the brake sensor is configured to output braking feedback data to the brake controller, and wherein determining whether the wheel speed characteristic indicates the failure of the brake comprises:

calculating, by the brake controller, an expected wheel speed characteristic based on the braking feedback data output from the brake sensor;

determining, by the brake controller, a difference between the wheel speed characteristic and the expected wheel speed characteristic; and

comparing, by the brake controller, the difference between the wheel speed characteristic and the expected wheel speed characteristic to a threshold difference.

3. The system of claim 1 , wherein the operations further comprise generating, by the brake controller, an alert if the wheel speed characteristic indicates the failure of the brake.

4. The system of claim 3 , wherein determining whether the wheel speed characteristic indicates the failure of the brake comprises comparing, by the brake controller, the wheel speed characteristic to a threshold wheel speed characteristic.

5. The system of claim 4 , wherein the wheel speed characteristic is at least one of an angular velocity of the wheel or a deceleration of the wheel.

6. A method of detecting aircraft brake failure using retract braking, comprising:

receiving, by a landing gear controller, a weight off wheels signal from a weight on wheels sensor;

receiving, by the landing gear controller, at least one of a gear handle up signal or a gear unlocked signal, wherein the gear handle up signal indicates a pilot landing gear handle is in a landing gear up position, and wherein the gear unlocked signal indicates a landing gear in an unlocked position;

sending, by the landing gear controller, a begin retract braking signal to a brake controller in response to receiving the weight off wheels signal and the at least one of the gear handle up signal or the gear unlocked signal;

receiving, by the brake controller, the begin retract braking signal;

commanding, by the brake controller, a brake to apply a braking force to a wheel of the landing gear;

calculating, by the brake controller, a wheel speed characteristic of the wheel; and

determining, by the brake controller, whether the wheel speed characteristic indicates a failure of the brake.

7. The method of claim 6 , further comprising generating, by the brake controller, an alert if the wheel speed characteristic indicates the failure of the brake.

8. The method of claim 7 , wherein determining whether the wheel speed characteristic indicates the failure of the brake comprises:

calculating, by the brake controller, an expected wheel speed characteristic based on a braking signal output from a brake sensor coupled to the brake;

determining, by the brake controller, a difference between the wheel speed characteristic and the expected wheel speed characteristic; and

comparing, by the brake controller, the difference between the wheel speed characteristic and the expected wheel speed characteristic to a threshold discrepancy value.

9. The method of claim 6 , further comprising receiving, by the brake controller, data from a wheel sensor coupled to the wheel, wherein the wheel speed characteristic of the wheel is calculated using the data from the wheel sensor.

10. The method of claim 9 , wherein the wheel speed characteristic is at least one of an angular velocity of the wheel or a deceleration of the wheel.

11. An article of manufacture including a non-transitory, tangible computer readable storage medium having instructions stored thereon that, in response to execution by a brake controller, cause the brake controller to perform operations comprising:

receiving, by the brake controller, a begin retract braking signal, the begin retract braking signal comprising a weight off wheel signal and at least one of a gear handle up signal or a gear unlocked signal, wherein the gear handle up signal indicates a pilot landing gear handle is in a landing gear up position, and wherein the gear unlocked signal indicates a landing gear is in an unlocked position;

commanding, by the brake controller, a brake to apply a braking force to a wheel of the landing gear;

receiving, by the brake controller, data from a wheel sensor coupled to the wheel;

calculating, by the brake controller, a wheel speed characteristic of the wheel based on the data; and

determining, by the brake controller, whether the wheel speed characteristic indicates a failure of the brake.

12. The article of manufacture of claim 11 , wherein the operations further comprise generating, by the brake controller, an alert if the wheel speed characteristic indicates the failure of the brake.

13. The article of manufacture of claim 12 , wherein determining whether the wheel speed characteristic indicates the failure of the brake comprises:

calculating, by the brake controller, an expected wheel speed characteristic based on the braking force applied to the wheel;

determining, by the brake controller, a difference between the wheel speed characteristic and the expected wheel speed characteristic; and

comparing, by the brake controller, the difference between the wheel speed characteristic and the expected wheel speed characteristic to a threshold discrepancy value.

14. The article of manufacture of claim 13 , wherein calculating the expected wheel speed characteristic comprises:

receiving, by the brake controller, braking feedback data from a brake sensor coupled to the brake; and

calculating, by the brake controller, the expected wheel speed characteristic using the braking feedback data.

15. The article of manufacture of claim 11 , wherein the begin retract braking signal is sent from a landing gear controller.