Advanced locked wheel protection functionality
A method for controlling brake assemblies of a vehicle is provided. Responsive to identifying a locked wheel protection event for a first wheel of a paired set of wheels on the vehicle, where the paired set of wheels is the first wheel on one side of the vehicle and a second wheel on an opposite side of the vehicle, a first brake pressure to a first brake assembly associated with the first wheel is released to zero pounds per square inch (PSI) and a second brake pressure to a second brake assembly associated with the second wheel of the paired set of wheels is reduced by a predetermined amount thereby reducing a yaw effect to the vehicle.
1. A method for controlling brake assemblies of a vehicle, the method comprising:
responsive to identifying a locked wheel protection event for a first wheel of a paired set of wheels on the vehicle, wherein the paired set of wheels is the first wheel on one side of the vehicle and a second wheel on an opposite side of the vehicle:
reducing a first brake pressure to a first brake assembly associated with the first wheel to zero pounds per square inch (PSI); and
reducing a second brake pressure to a second brake assembly associated with the second wheel of the paired set of wheels by a predetermined amount in order to reduce a yaw effect to the vehicle;
determining whether the first wheel has recovered from the locked wheel protection event; and
responsive to the first wheel recovering from the locked wheel protection event, returning the first brake pressure and the second brake pressure to a braking pressure being commanded by a brake pedal of the vehicle.
2. The method of claim 1 , wherein the predetermined amount is from 40% to 60% of a brake pressure being commanded by a brake pedal of the vehicle.
3. The method of claim 1 , further comprising:
further reducing the second brake pressure to the second brake assembly associated with the second wheel linearly over a predetermined time period.
4. The method of claim 3 , wherein the predetermined time period is from 1 to 6seconds.
5. The method of claim 1 , wherein the determining of whether the first wheel has recovered from the locked wheel protection event occurs over a predetermined time period.
6. The method of claim 5 , further comprising:
responsive to the predetermined time period expiring and the first wheel failing to recover from the locked wheel protection event, leaving the first brake pressure at zero PSI and returning the second brake pressure to the braking pressure being commanded by the brake pedal of the vehicle.
7. The method of claim 1 , wherein the locked wheel protection event is indicated by a wheel speed transducer indicating a reduced wheel speed.
8. A braking system for controlling brake assemblies of a vehicle, the braking system comprising:
a brake control unit, wherein the brake control unit is configured to:
responsive to identifying a locked wheel protection event for a first wheel of a paired set of wheels on the vehicle, wherein the paired set of wheels is the first wheel on one side of the vehicle and a second wheel on an opposite side of the vehicle:
reduce a first brake pressure to a first brake assembly associated with the first wheel to zero pounds per square inch (PSI); and
reduce a second brake pressure to a second brake assembly associated with the second wheel of the paired set of wheels by a predetermined amount in order to reduce a yaw effect to the vehicle;
determine whether the first wheel has recovered from the locked wheel protection event; and
responsive to the first wheel recovering from the locked wheel protection event, return the first brake pressure and the second brake pressure to a braking pressure being commanded by a brake pedal of the vehicle.
9. The braking system of claim 8 , wherein the predetermined amount is from 40% to 60% of a brake pressure being commanded by a brake pedal of the vehicle.
10. The braking system of claim 8 , wherein the brake control unit is further configured to:
further reduce the second brake pressure to the second brake assembly associated with the second wheel linearly over a predetermined time period.
11. The braking system of claim 10 , wherein the predetermined time period is from 1to 6 seconds.
12. The braking system of claim 8 , wherein the determining of whether the first wheel has recovered from the locked wheel protection event occurs over a predetermined time period.
13. The braking system of claim 12 , wherein the brake control unit is further configured to:
responsive to the predetermined time period expiring and the first wheel failing to recover from the locked wheel protection event, leave the first brake pressure at zero PSI and return the second brake pressure to the braking pressure being commanded by the brake pedal of the vehicle.
14. The braking system of claim 8 , wherein the locked wheel protection event is indicated by a wheel speed transducer indicating a reduced wheel speed.
15. An aircraft, the aircraft comprising:
a first wheel and a second wheel;
a first brake assembly associated with the first wheel;
a second brake assembly associated with the second wheel; and
a brake control unit, wherein the brake control unit is configured to:
responsive to identifying a locked wheel protection event for the first wheel:
reduce a first brake pressure to the first brake assembly to zero pounds per square inch (PSI); and
reduce a second brake pressure to the second brake assembly by a predetermined amount in order to reduce a yaw effect to the aircraft;
determine whether the first wheel has recovered from the locked wheel protection event; and
responsive to the first wheel recovering from the locked wheel protection event, return the first brake pressure and the second brake pressure to a braking pressure being commanded by a brake pedal of the aircraft.
16. The aircraft of claim 15 , wherein the brake control unit is further configured to:
further reduce the second brake pressure to the second brake assembly associated with the second wheel linearly over a predetermined time period.
17. The aircraft of claim 16 , wherein the determining of whether the first wheel has recovered from the locked wheel protection event occurs over the predetermined time period.
18. The aircraft of claim 17 , wherein the brake control unit is further configured to:
responsive to the predetermined time period expiring and the first wheel failing to recover from the locked wheel protection event, leave the first brake pressure at zero PSI and return the second brake pressure to the braking pressure being commanded by the brake pedal of the aircraft.