System for determining the stack closure pressure of a brake stack

Patent metadata

Field	Value
Publication number	US-2020362979-A1
Application number	US-201916410720-A
Country	US
Kind code	A1
Filing date	May 13, 2019
Priority date	May 13, 2019
Publication date	Nov 19, 2020
Grant date	—

Abstract

A brake system is disclosed. The brake system includes a brake stack having a stack closure pressure, a force member positioned within a cylinder, a valve configured to control the fluid pressure of the brake system, and one or more pressure transducers that generate a proportional electrical signal representative of fluid pressure within the cylinder. The brake system also includes one or more processors in electronic communication with the valve, the one or more pressure transducers, and a memory coupled to the one or more processors. The memory stores data comprising a database and program code that, when executed by the one or more processors, causes the brake system to determine the stack closure pressure of the brake stack.

First claim

What is claimed is:

1 . A brake system having a brake stack with a stack closure pressure, a force member positioned within a cylinder, a valve configured to adjust fluid pressure in the brake system, and one or more pressure transducers that generate a proportional electrical signal representative of the fluid pressure within the cylinder, the brake system comprising:
one or more processors in electronic communication with the valve and the one or more pressure transducers; and a memory coupled to the one or more processors, the memory storing data comprising a database and program code that, when executed by the one or more processors, causes the brake system to:
generate a valve command instructing the valve to increase the fluid pressure in the brake system, which results in increasing an amount of brake fluid supplied to the cylinder at a fixed rate;
monitor an output of the proportional electrical signal generated by the one or more pressure transducers;
determine a derivative value of the output of the proportional electrical signal as the amount of brake fluid supplied to the cylinder is increased at the fixed rate;
determine a transition point of the derivative value, wherein the transition point represents when the derivative value exceeds about zero and increases to a positive value; and
select the fluid pressure at the transition point as the stack closure pressure of the brake system.

2 . The brake system of claim 1 , wherein the one or more processors execute instructions to:
save the fluid pressure at the transition point in the memory, wherein the memory includes a plurality of previously recorded values at the transition point.

3 . The brake system of claim 2 , wherein the one or more processors execute instructions to:
determine the stack closure pressure of the brake system is an average of the fluid pressure at the transition point and the plurality of previously recorded values at the transition point.

4 . The brake system of claim 1 , wherein autobrake instructions are saved in the memory, and wherein the one or more processors execute instructions to:
generate, by the autobrake instructions, an input command, wherein input command represents an amount of braking requested by the brake system; and determine the valve command based on at least the input command.

5 . The brake system of claim 1 , wherein the one or more processors execute instructions to:
determine the derivative value of the output of the proportional electrical signal is below a threshold pressure value; and in response to determining the derivative value of the output of the proportional electrical signal is below the threshold pressure value, set the derivative value to about zero.

6 . The brake system of claim 1 , wherein the brake fluid is one of a liquid and a gas.

7 . The brake system of claim 1 , wherein the brake system includes a dead band space.

8 . The brake system of claim 1 , wherein the proportional electrical signal is selected from the group comprising of: a current value, a capacitance value, and a voltage value.

9 . An aircraft having a brake system, the aircraft comprising:
a brake stack including one or more rotors interleaved with one or more stators; a force member positioned within a cylinder; a valve configured to adjust fluid pressure in the brake system; one or more pressure transducers that generate a proportional electrical signal representative of the fluid pressure within the cylinder; one or more processors in electronic communication with the valve and the one or more pressure transducers; and a memory coupled to the one or more processors, the memory storing data comprising a database and program code that, when executed by the one or more processors, causes the brake system to:
generate a valve command instructing the valve to increase the fluid pressure in the brake system, which results in increasing of an amount of hydraulic brake fluid supplied to the cylinder at a fixed rate;
monitor an output of the proportional electrical signal generated by the one or more pressure transducers;
determine a derivative value of the output of the proportional electrical signal as the amount of hydraulic brake fluid supplied to the cylinder is increased at the fixed rate;
determine a transition point of the derivative value, wherein the transition point represents when the derivative value exceeds about zero and increases to a positive value; and
select the fluid pressure at the transition point as a stack closure pressure of the brake system, wherein the stack closure pressure represents a minimum amount brake pressure required to generate brake torque by the brake stack.

10 . The aircraft of claim 9 , wherein the one or more processors executes instructions to:
save the fluid pressure at the transition point in the memory, wherein the memory includes a plurality of previously recorded values at the transition point.

11 . The aircraft of claim 10 , wherein the one or more processors execute instructions to:
determine the stack closure pressure of the brake system is an average of the fluid pressure at the transition point and the plurality of previously recorded values at the transition point.

12 . The aircraft of claim 9 , wherein autobrake instructions are saved in the memory, and wherein the one or more processors execute instructions to:
generate, by the autobrake instructions, an input command, wherein input command represents an amount of braking requested by the brake system; and determine the valve command based on at least the input command.

13 . The aircraft of claim 9 , wherein the one or more processors execute instructions to:
determine the derivative value of the output of the proportional electrical signal is below a threshold pressure value; and in response to determining the derivative value of the output of the proportional electrical signal is below the threshold pressure value, set the derivative value to about zero.

14 . The aircraft of claim 9 , wherein the brake system includes a dead band space.

15 . The aircraft of claim 9 , wherein the proportional electrical signal is selected from the group comprising of: a current value, a capacitance value, and a voltage value.

16 . A method for determining a stack closure pressure for a brake stack of a brake system, the method comprising:
generating, by a computer, a valve command instructing a valve to increase fluid pressure of the brake system, which results in an amount of brake fluid supplied to a cylinder at a fixed rate, wherein a force member is positioned within the cylinder and the valve is configured to control the amount of brake fluid supplied to the cylinder; monitoring, by the computer, an output of a proportional electrical signal generated by one or more pressure transducers, wherein the proportional electrical signal is representative of the fluid pressure within the cylinder; determining a derivative value of the output of the proportional electrical signal as the amount of brake fluid supplied to the cylinder is increased at the fixed rate; determining a transition point of the derivative value, wherein the transition point represents when the derivative value exceeds about zero and increases to a positive value; and selecting the fluid pressure at the transition point as the stack closure pressure of the brake system.

17 . The method of claim 16 , further comprising:
saving the fluid pressure at the transition point in a memory of the computer, wherein the memory includes a plurality of previousl

Assignees

• Boeing Co

Inventors

• Yamamoto David T
• Smith Steven Elliot
• Forghani Nima

Classifications

• B60T8/1703

  for aircrafts · CPC title

• F16D66/00

  Arrangements for monitoring working conditions, e.g. wear, temperature · CPC title

• F16D2121/16

  for releasing a normally applied brake · CPC title

• F16D2066/005

  Force, torque, stress or strain · CPC title

• F16D2121/04

  acting on a piston-type actuator, e.g. for liquid pressure · CPC title