Antiskid brake control system with axle-mounted inertial sensor

Patent metadata

Field	Value
Publication number	US-10525945-B2
Application number	US-201715490577-A
Country	US
Kind code	B2
Filing date	Apr 18, 2017
Priority date	Apr 18, 2017
Publication date	Jan 7, 2020
Grant date	Jan 7, 2020

Abstract

A brake control system may comprise an inertial sensor coupled to an axle and configured to measure a linear acceleration of the axle and an antiskid control (ASK) in electronic communication with the inertial sensor, wherein at least one of the inertial sensor or the ASK calculate a linear velocity of the axle based on the linear acceleration, and the ASK uses the linear velocity to calculate a wheel slip speed.

First claim

What is claimed is:

1. A brake control system, comprising:
an inertial sensor coupled to an axle and configured to measure a linear acceleration of the axle; and
an antiskid control (ASK) in electronic communication with the inertial sensor,
wherein at least one of the inertial sensor or the ASK calculate a linear velocity of the axle based on the linear acceleration, and
the ASK uses the linear velocity to calculate a wheel slip speed.

2. The brake control system of claim 1 , wherein the inertial sensor measures the linear acceleration of the axle in a forward direction.

3. The brake control system of claim 1 , wherein the inertial sensor comprises at least one of an accelerometer, a magnetometer, and a gyroscope.

4. The brake control system of claim 3 , wherein the inertial sensor comprises a microelectromechanical system (MEMS).

5. The brake control system of claim 1 , further comprising a wheel speed sensor configured to measure a rotational velocity of the axle.

6. The brake control system of claim 5 , wherein the rotational velocity and the linear velocity are used to calculate the wheel slip speed.

7. The brake control system of claim 6 , wherein the ASK calculates the wheel slip speed using equation V slip −V ac −r drag ·ω, where V ac equals the linear velocity, ω equals the rotational velocity, and r drag equals a distance between an axis of rotation of the axle and a ground surface.

8. The brake control system of claim 1 , wherein the ASK comprises a controller and instructions stored in a memory configured to be executed by the controller, the ASK being mounted to the axle, the ASK configured to send the wheel slip speed to an airframe mounted controller via at least one of an analog signal or a digital signal.

9. The brake control system of claim 1 , wherein the ASK comprises a controller and instructions stored in a memory configured to be executed by the controller, the ASK being mounted to an airframe, the inertial sensor configured to send at least one of a raw signal or a processed signal to the ASK via at least one of an analog signal or a digital signal.

10. The brake control system of claim 1 , further comprising a load balance control (LBK).

11. The brake control system of claim 10 , wherein the inertial sensor is configured to measure an additional linear acceleration of the axle, the additional linear acceleration measured in a vertical direction.

12. The brake control system of claim 11 , wherein the LBK calculates a load balance deceleration command using the additional linear acceleration.

13. A method for controlling brakes, comprising:
measuring, by an inertial sensor, a linear acceleration of an aircraft;
receiving, by an antiskid control (ASK), the linear acceleration;
calculating, by the ASK, an aircraft speed based on the linear acceleration;
calculating, by the ASK, a wheel slip speed using the aircraft speed based on the linear acceleration; and
calculating, by the ASK, a pressure command based on the wheel slip speed.

14. The method of claim 13 , further comprising:
receiving, by a brake control unit (BCU), the pressure command from the ASK; and
sending, by the BCU, a current to a brake control device.

15. The method of claim 13 , wherein the aircraft speed is measured in a forward direction.

16. A method for controlling brakes, comprising:
measuring, by an inertial sensor, a linear acceleration of an aircraft in a vertical direction;
receiving, by a load balance control (LBK), the linear acceleration;
calculating, by the LBK, a drag radius using the linear acceleration; and
calculating, by the LBK, at least one of a load balance deceleration command and a desired pressure adjustor using the linear acceleration.

17. The method of claim 16 , further comprising receiving, by an antiskid control (ASK), the load balance deceleration command.

18. The method of claim 17 , further comprising:
receiving, by a brake control unit (BCU), a pressure command from the ASK, the pressure command generated using the load balance deceleration command; and
sending, by the BCU, a current to a brake control device.

Assignees

• Goodrich Corp

Inventors

• Ayichew Efrem E
• Kordik Michael
• Georgin Marc
• Summers Paul L

Classifications

• B60T8/325

  Systems specially adapted for aircraft · CPC title

• B60T8/1875

  comprising sensors of the type providing an electrical output signal representing the load on the vehicle suspension · CPC title

• B60T8/172

  Determining control parameters used in the regulation, e.g. by calculations involving measured or detected parameters {(B60T8/17551 takes precedence)} · CPC title

• B64C25/46

  Brake regulators for preventing skidding or aircraft somersaulting · CPC title

• B60T8/1761

  responsive to wheel or brake dynamics, e.g. wheel slip, wheel acceleration or rate of change of brake fluid pressure · CPC title