System and method of determining accumulator status

Patent metadata

Field	Value
Publication number	US-9533667-B2
Application number	US-201414527930-A
Country	US
Kind code	B2
Filing date	Oct 30, 2014
Priority date	Feb 6, 2014
Publication date	Jan 3, 2017
Grant date	Jan 3, 2017

Abstract

A method of detecting an accumulator failure is provided. The method may comprise measuring a first pressure on a gas-side of an accumulator, measuring a second pressure on a fluid-side of the accumulator, finding a difference between the first pressure and the second pressure, and comparing the difference to a predetermined threshold. A system for detecting an accumulator failure is also provided. The system may comprise a non-transitory memory communicating with a processor, the non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations. The operations may include receiving a first pressure measurement, receiving a second pressure measurement, determining a difference between the first pressure measurement and the second pressure measurement, and detecting the accumulator failure based on the difference.

First claim

What is claimed is:

1. A method comprising:
receiving, by a processor, a first pressure measurement;
receiving, by the processor, a second pressure measurement;
determining, by the processor, a difference between the first pressure measurement and the second pressure measurement;
detecting, by the processor, the accumulator failure based on the difference; and
signaling, to at least one of a cockpit, a warning light, a monitor, or a maintenance device, that an accumulator is sticking in response to the accumulator failure.

2. The method of claim 1 , further comprising measuring a gas-side pressure of the accumulator using a first pressure sensor, wherein the first pressure sensor provides the first pressure measurement.

3. The method of claim 2 , further comprising measuring a fluid-side pressure of the accumulator using a second pressure sensor, wherein the second pressure sensor provides the second pressure measurement.

4. The method of claim 1 , wherein the detecting the accumulator failure based on the difference further comprises:
receiving, by the processor, a predetermined threshold; and
determining, by the processor, the difference exceeds the predetermined threshold.

5. The method of claim 4 , wherein the detecting the accumulator failure based on the difference further comprises:
receiving, by the processor, a failure duration; and
determining, by the processor, the difference has exceeded the predetermined threshold for the failure duration.

6. The method of claim 5 , wherein the failure duration is greater than or equal to 3 milliseconds.

7. The method of claim 5 , wherein the failure duration is less than or equal to 1 second.

8. The method of claim 4 , wherein the predetermined threshold is 150 psi.

9. The method of claim 1 , further comprising a piston accumulator.

10. The method of claim 9 , wherein the accumulator failure is a sticking piston of the piston accumulator.

11. A system comprising:
a processor;
an accumulator having a gas-side and a fluid-side;
a gas-side pressure sensor operatively coupled to the gas-side of the accumulator and the processor; and
a fluid-side pressure sensor operatively coupled to the fluid-side of the accumulator and the processor,
wherein the processor is configured to receive a first pressure measurement from the gas-side pressure sensor,
wherein the processor is configured to receive a second pressure measurement from the fluid-side pressure sensor;
wherein the processor is configured to determine a difference between the first pressure measurement and the second pressure measurement,
wherein the processor is configured to detect an accumulator failure based on the difference,
wherein the processor is configured to signal at least one of a cockpit, a warning light, a monitor, or a maintenance device, that the accumulator is sticking in response to the accumulator failure.

12. The system of claim 11 , wherein the processor is configured to receive a predetermined threshold and determine whether the difference exceeds the predetermined threshold.

13. The system of claim 12 , wherein the predetermined threshold is 150 psi.

Assignees

• Goodrich Corp

Inventors

• Cahill Eric D
• Burte Paul R

Classifications

• F15B2201/51

  Pressure detection · CPC title

• F15B2201/31

  having rigid separating means, e.g. pistons · CPC title

• F15B2201/205

  using gas · CPC title

• F15B1/24 Primary

  with rigid separating means, e.g. pistons · CPC title

• B60T17/221 Primary

  Procedure or apparatus for checking or keeping in a correct functioning condition of brake systems (hydraulic pressure systems in general F15B19/00, F15B21/04; testing structures or apparatus G01M) · CPC title