Locked wheel extension protection in brake control systems

Patent metadata

Field	Value
Publication number	US-2017174331-A1
Application number	US-201514979198-A
Country	US
Kind code	A1
Filing date	Dec 22, 2015
Priority date	Dec 22, 2015
Publication date	Jun 22, 2017
Grant date	—

Abstract

A method for controlling brakes is provided. The method may include the steps of detecting an aircraft speed, determining the aircraft speed is within a range from an antiskid-dropout speed to a locked-wheel-protection-engagement speed, and determining an input of a pressure controller has a value less than a pressure maximum threshold. A current command that is output from the pressure controller may be detected at or above a threshold value. The states of the pressure controller and pressure controller input may be reset in response to the current command being at or above the threshold value for a predetermined duration.

First claim

What is claimed is:

1 . A method for controlling brakes, comprising:
detecting, by a brake control unit (BCU), an aircraft speed; determining, by the BCU, the aircraft speed is within a range from an antiskid-dropout speed to a locked-wheel-protection-engagement speed; determining, by the BCU, an input of a pressure controller has a value less than a pressure maximum threshold; determining, by the BCU, a current command that is output from the pressure controller is at least one of at or above a threshold value; and resetting, by the BCU, a state of the pressure controller and the input of the pressure controller in response to the current command being at least one of at or above the threshold value for a predetermined duration.

2 . The method of claim 1 , further comprising determining, by the BCU, that the predetermined duration has elapsed while the current command has been maintained in at least one of at or above the threshold value.

3 . The method of claim 1 , further comprising reducing, by the BCU, a brake pressure in response to the current command being at least one of at or above the threshold value for the predetermined duration.

4 . The method of claim 1 , wherein the antiskid-dropout speed is 10 knots and the locked-wheel-protection-engagement speed is 30 knots.

5 . The method of claim 1 , wherein the threshold value is a maximum current command value.

6 . The method of claim 1 , further comprising generating, by the BCU, the current command that is output by the pressure controller based on a relationship between the input of the pressure controller and the current command.

7 . The method of claim 1 , further comprising switching, by the BCU, to an open-loop control in response to a pressure sensor failure.

8 . The method of claim 1 , wherein the current command ranges from 2 mA to 30 mA.

9 . The method of claim 1 , wherein the input of the pressure controller comprises a pressure command ranging from 0 psi to 3000 psi.

10 . The method of claim 1 , further comprising setting, by the BCU, the input of the pressure controller to a minimum value selected from a pilot desired pressure or an antiskid control unit desired pressure.

11 . A brake control system, comprising:
a brake control unit (BCU) comprising a pressure control unit (PK), wherein the PK is configured to receive a pressure command and output a current command in response to the pressure command, wherein the BCU is configured to reset a state of the PK and the pressure command in response to detecting the current command being at least one of at or above a threshold value for a predetermined duration; an aircraft brake having a brake control device configured to apply a force in response to the current command.

12 . The brake control system of claim 11 , wherein the BCU comprises a brake control executive (BKX) configured to set the pressure command to a minimum value selected from a pilot desired pressure and an antiskid control unit desired pressure.

13 . The brake control system of claim 11 , wherein BCU is configured to switch to an open-loop control in response to a signal from a failed pressure sensor.

14 . The brake control system of claim 13 , wherein the signal from the failed pressure sensor is within an expected range.

15 . A brake control system, comprising:
a processor; a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause a brake control unit (BCU) to perform operations comprising: determining, by the BCU, an aircraft speed is within a range from an antiskid-dropout speed to a locked-wheel-protection-engagement speed; determining, by the BCU, an input of a pressure controller has a value less than a pressure maximum threshold; determining, by the BCU, a current command that is output from the pressure controller is at or above a threshold value for a predetermined duration; and resetting, by the BCU, a state of the pressure controller and the input of the pressure controller in response to the current command being at least one of at or above the threshold value for the predetermined duration.

16 . The brake control system of claim 15 , wherein the threshold value is a maximum current command value.

17 . The brake control system of claim 15 , wherein the antiskid-dropout speed is 10 knots and the locked-wheel-protection-engagement speed is 30 knots.

18 . The brake control system of claim 15 , further comprising generating, by the BCU, the current command that is output by the pressure controller based on a relationship between the input of the pressure controller and the current command.

19 . The brake control system of claim 15 , further comprising switching, by the BCU, to an open-loop control in response to a pressure sensor failure.

20 . The brake control system of claim 15 , further comprising setting, by the BCU, the input of the pressure controller to a minimum value selected from at least one of a pilot desired pressure or an antiskid control unit desired pressure.

Assignees

• Goodrich Corp

Inventors

• Georgin Mark
• Metzger Jr Richard Paul

Classifications

• B60T8/17616

  Microprocessor-based systems · CPC title

• B60T8/1703 Primary

  for aircrafts · CPC title

• B64C25/42 Primary

  Arrangement or adaptation of brakes · CPC title

• B60T8/171

  Detecting parameters used in the regulation; Measuring values used in the regulation · CPC title

• B64C25/34

  wheeled type, e.g. multi-wheeled bogies · CPC title