Methods and apparatus for controlling landing gear retract braking
Methods and apparatus for controlling landing gear retract braking are described. A controller is to determine an on-ground status of a wheel of a landing gear. The controller is to generate a control signal based on the on-ground status of the wheel. The control signal is to initiate a retract braking process for the wheel. The retract braking process is to decelerate the wheel from a first rate of rotation to a second rate of rotation less than the first rate of rotation.
1. An apparatus comprising:
a controller to:
determine an on-ground status of a wheel of a landing gear; and
generate a control signal in response to the on-ground status of the wheel indicating that the wheel is not contacting a ground surface, the control signal to automatically initiate a retract braking process for the wheel prior to a landing gear lever being manually actuated into a gear up position, the retract braking process to decelerate the wheel from a first rate of rotation to a second rate of rotation less than the first rate of rotation.
2. The apparatus of claim 1 , wherein the controller is to:
determine an engine speed of at least one of a left engine or a right engine; and
generate the control signal based further on the engine speed of the at least one of the left engine or the right engine.
3. The apparatus of claim 2 , wherein the controller is to generate the control signal in response to determining that the engine speed of the at least one of the left engine or the right engine exceeds an engine speed threshold.
4. The apparatus of claim 1 , wherein the controller is to:
determine a throttle parameter of at least one of a left throttle or a right throttle; and
generate the control signal based further on the throttle parameter of the at least one of the left throttle or the right throttle.
5. The apparatus of claim 4 , wherein the controller is to generate the control signal in response to determining that the throttle parameter of the at least one of the left throttle or the right throttle exceeds a throttle parameter threshold.
6. The apparatus of claim 1 , wherein the controller is to:
determine a landing gear position of the landing gear; and
generate the control signal based further on the landing gear position of the landing gear.
7. The apparatus of claim 6 , wherein the controller is to generate the control signal in response to the landing gear position of the landing gear indicating that the landing gear is not retracted or not locked.
8. The apparatus of claim 1 , wherein the controller is to:
determine a flap position of a flap; and
generate the control signal based further on the flap position of the flap.
9. The apparatus of claim 8 , wherein the controller is to generate the control signal in response to determining that the flap position of the flap corresponds to a takeoff position.
10. A method comprising:
determining, by executing one or more instructions via a controller, an on-ground status of a wheel of a landing gear; and
generating, by executing one or more instructions via the controller, a control signal in response to the on-ground status of the wheel indicating that the wheel is not contacting a ground surface, the control signal to automatically initiate a retract braking process for the wheel prior to a landing gear lever being manually actuated into a gear up position, the retract braking process to decelerate the wheel from a first rate of rotation to a second rate of rotation less than the first rate of rotation.
11. The method of claim 10 , further comprising:
determining, by executing one or more instructions via the controller, an engine speed of at least one of a left engine or a right engine; and
generating the control signal based further on the engine speed of the at least one of the left engine or the right engine.
12. The method of claim 10 , further comprising:
determining, by executing one or more instructions via the controller, a throttle parameter of at least one of a left throttle or a right throttle; and
generating the control signal based further on the throttle parameter of the at least one of the left throttle or the right throttle.
13. The method of claim 10 , further comprising:
determining, by executing one or more instructions via the controller, a landing gear position of the landing gear; and
generating the control signal based further on the landing gear position of the landing gear.
14. A non-transitory machine-readable storage medium comprising instructions that, when executed, cause a controller to at least:
determine an on-ground status of a wheel of a landing gear; and
generate a control signal in response to the on-ground status of the wheel indicating that the wheel is not contacting a ground surface, the control signal to automatically initiate a retract braking process for the wheel prior to a landing gear lever being manually actuated into a gear up position, the retract braking process to decelerate the wheel from a first rate of rotation to a second rate of rotation less than the first rate of rotation.
15. The non-transitory machine-readable storage medium of claim 14 , wherein the instructions, when executed, cause the controller to:
determine an engine speed of at least one of a left engine or a right engine; and
generate the control signal based further on the engine speed of the at least one of the left engine or the right engine.
16. The non-transitory machine-readable storage medium of claim 14 , wherein the instructions, when executed, cause the controller to:
determine a throttle parameter of at least one of a left throttle or a right throttle; and
generate the control signal based further on the throttle parameter of the at least one of the left throttle or the right throttle.
17. The non-transitory machine-readable storage medium of claim 14 , wherein the instructions, when executed, cause the controller to:
determine a landing gear position of the landing gear; and
generate the control signal based further on the landing gear position of the landing gear.
18. The method of claim 11 , wherein generating the control signal based further on the engine speed of the at least one of the left engine or the right engine includes generating the control signal in response to determining that the engine speed of the at least one of the left engine or the right engine exceeds an engine speed threshold.
19. The method of claim 12 , wherein generating the control signal based further on the throttle parameter of the at least one of the left throttle or the right throttle includes generating the control signal in response to determining that the throttle parameter of the at least one of the left throttle or the right throttle exceeds a throttle parameter threshold.
20. The method of claim 13 , wherein generating the control signal based further on the landing gear position of the landing gear includes generating the control signal in response to the landing gear position of the landing gear indicating that the landing gear is not retracted or not locked.