Methods and apparatus for controlling landing gear retract braking

Patent metadata

Field	Value
Publication number	US-10933982-B2
Application number	US-201815905392-A
Country	US
Kind code	B2
Filing date	Feb 26, 2018
Priority date	Feb 26, 2018
Publication date	Mar 2, 2021
Grant date	Mar 2, 2021

Abstract

Methods and apparatus for controlling landing gear retract braking are described. A controller determines wheel speed data corresponding to a speed of a wheel of a landing gear. The controller determines wheel deceleration data corresponding to a rate of change of the wheel speed data. The controller generates a first control signal in response to the wheel deceleration data being greater than a wheel deceleration threshold. The first control signal initiates a wheel deceleration regulation process, the wheel deceleration regulation process to cycle an antiskid valve between a first valve position to release brake pressure from the wheel and a second valve position to cease releasing the brake pressure from the wheel. The controller generates a second control signal in response to the wheel speed data being less than a wheel speed threshold. The second control signal terminates the wheel deceleration regulation process.

First claim

What is claimed is:

1. An apparatus comprising:
a controller configured to:
initiate a retract braking process in response to determining that a landing gear lever has moved from a first lever position to a second lever position, the retract braking process to decelerate a wheel of a shrinkable landing gear as the shrinkable landing gear moves from a deployed position to a retracted position, the deceleration of the wheel to generate an applied moment transferable to a lower strut of the shrinkable landing gear;
determine wheel speed data corresponding to a speed of the wheel;
determine wheel deceleration data corresponding to a rate of change of the wheel speed data;
generate a first control signal in response to the wheel deceleration data being greater than a wheel deceleration threshold, the first control signal to modulate the deceleration of the wheel during the retract braking process by cycling an antiskid valve between a first valve position to release brake pressure from the wheel and a second valve position to cease releasing the brake pressure from the wheel, the cycling of the antiskid valve to reduce an extent of the applied moment; and
generate a second control signal in response to the wheel speed data becoming less than a wheel speed threshold during the modulation of the deceleration of the wheel, the second control signal to terminate the modulation of the deceleration of the wheel.

2. The apparatus of claim 1 , wherein the wheel speed data is summed wheel speed data corresponding to a sum of a speed of a first wheel of the shrinkable landing gear and a speed of a second wheel of the shrinkable landing gear.

3. The apparatus of claim 1 , wherein the controller is configured to obtain the wheel speed data from a wheel speed sensor operatively coupled to the wheel of the shrinkable landing gear.

4. The apparatus of claim 1 , wherein the controller includes an anti skid inhibit switch configured to control the cycling of the antiskid valve between the first valve position and the second valve position.

5. The apparatus of claim 4 , wherein the antiskid inhibit switch is configured to operate between a first switch position corresponding to the first valve position and a second switch position corresponding to the second valve position.

6. The apparatus of claim 5 , wherein the antiskid inhibit switch is configured to operate between the first switch position and the second switch position based on a duty cycle.

7. The apparatus of claim 1 , wherein the controller is configured to terminate the retract braking process in response to determining that the landing gear lever has moved from the second lever position to the first lever position, or in response to determining that a timer associated with a duration of the retract braking process has expired.

8. A method comprising:
initiating, by executing one or more instructions via a controller, a retract braking process in response to determining that a landing gear lever has moved from a first lever position to a second lever position, the retract braking process decelerating a wheel of a shrinkable landing gear as the shrinkable landing gear moves from a deployed position to a retracted position, the deceleration of the wheel generating an applied moment transferable to a lower strut of the shrinkable landing gear;
determining, by executing one or more instructions via the controller, wheel speed data corresponding to a speed of the wheel;
determining, by executing one or more instructions via the controller, wheel deceleration data corresponding to a rate of change of the wheel speed data;
generating, by executing one or more instructions via the controller, a first control signal in response to the wheel deceleration data being greater than a wheel deceleration threshold, the first control signal modulating the deceleration of the wheel during the retract braking process by cycling an antiskid valve between a first valve position that releases brake pressure from the wheel and a second valve position that ceases releasing the brake pressure from the wheel, the cycling of the antiskid valve reducing an extent of the applied moment; and
generating, by executing one or more instructions via the controller, a second control signal in response to the wheel speed data becoming less than a wheel speed threshold during the modulation of the deceleration of the wheel, the second control signal terminating the modulation of the deceleration of the wheel.

9. The method of claim 8 , wherein the wheel speed data is summed wheel speed data corresponding to a sum of a speed of a first wheel of the shrinkable landing gear and a speed of a second wheel of the shrinkable landing gear.

10. The method of claim 8 , further comprising obtaining the wheel speed data from a wheel speed sensor operatively coupled to the wheel of the shrinkable landing gear.

11. The method of claim 8 , wherein the cycling of the antiskid valve between the first valve position and the second valve position is controlled via an antiskid inhibit switch.

12. The method of claim 11 , wherein the antiskid inhibit switch operates between a first switch position corresponding to the first valve position and a second switch position corresponding to the second valve position.

13. The method of claim 12 , wherein the antiskid inhibit switch operates between the first switch position and the second switch position based on a duty cycle.

14. The method of claim 8 , further comprising terminating the retract braking process in response to determining that the landing gear lever has moved from the second lever position to the first lever position, or in response to determining that a timer associated with a duration of the retract braking process has expired.

15. A non-transitory machine-readable storage medium comprising instructions that, when executed, cause a controller to at least:
initiate a retract braking process in response to determining that a landing gear lever has moved from a first lever position to a second lever position, the retract braking process to decelerate a wheel of a shrinkable landing gear as the shrinkable landing gear moves from a deployed position to a retracted position, the deceleration of the wheel to generate an applied moment transferable to a lower strut of the shrinkable landing gear;
determine wheel speed data corresponding to a speed of the wheel;
determine wheel deceleration data corresponding to a rate of change of the wheel speed data;
generate a first control signal in response to the wheel deceleration data being greater than a wheel deceleration threshold, the first control signal to modulate the deceleration of the wheel during the retract braking process by cycling an antiskid valve between a first valve position to release brake pressure from the wheel and a second valve position to cease releasing the brake pressure from the wheel, the cycling of the antiskid valve to reduce an extent of the applied moment; and
generate a second control signal in response to the wheel speed data becoming less than a wheel speed threshold during the modulation of the deceleration of the wheel, the second control signal to terminate the modulation of the deceleration of the wheel.

16. The non-transitory machine-readable storage medium of claim 15 , wherein the wheel speed data is summed wheel speed data corresponding to a sum of a speed of a first wheel of the shrinkable landing gear and a speed of a second wheel of the shrinkable landing gear.

17. The non-transitory machine-readable storage medium of claim 15 , wherein the instruct

Assignees

• Boeing Co

Inventors

• Hubbard Taylor R
• Neale Isaac
• Plude Leo W
• Douglass Daniel B

Classifications

• B64C25/426

  Braking devices providing an automatic sequence of braking · CPC title

• B64C25/46 Primary

  Brake regulators for preventing skidding or aircraft somersaulting · CPC title

• B60T8/1703

  for aircrafts · CPC title

• B60T8/325

  Systems specially adapted for aircraft · CPC title

• B64C25/12

  sideways · CPC title