IP Library › Granted Patent US 11,078,935
Granted Patent B2
US 11,078,935 · App. 16/392,384 · Granted Aug 3, 2021

Prediction of hydraulic pump health and failure

Inventor: Dennis D. Chung (Arlington, WA)
Assignee: The Boeing Company
F15B19/005B64C13/504F04B51/00F15B2211/20515F15B2211/864F15B2211/8633F15B2211/8636G05B19/414G05B2219/41309
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 11,078,935
App. No.
16/392,384
Granted
Aug 3, 2021
Kind
B2
Abstract

In one or more embodiments, a system for predicting health of a hydraulic pump comprises a reservoir tank temperature sensor to measure a temperature of a reservoir tank. The system further comprises a hydraulic pump temperature sensor to measure a temperature of the hydraulic pump. Also, the system comprises a differential pressure sensor to measure a differential pressure across a filter associated with the hydraulic pump. Further, the system comprises a processor(s) to determine a differential temperature by subtracting the temperature of the reservoir tank from the temperature of the hydraulic pump, to compare the differential temperature to a differential temperature threshold, to compare the differential pressure to a differential pressure threshold, and to generate an alert signal indicating failure of the hydraulic pump, when the processor(s) determines that the differential temperature exceeds the differential temperature threshold and the differential pressure exceeds the differential pressure threshold.

Claims (31)

1. A method for predicting health of a hydraulic pump, the method comprising:

measuring, by a reservoir tank temperature sensor, a temperature of a reservoir tank;

measuring, by a hydraulic pump temperature sensor, a temperature of the hydraulic pump;

determining, by at least one processor, a differential temperature by subtracting the temperature of the reservoir tank from the temperature of the hydraulic pump;

measuring, by a differential pressure sensor, a differential pressure across a filter associated with the hydraulic pump;

comparing, by the at least one processor, the differential temperature to a differential temperature threshold;

comparing, by the at least one processor, the differential pressure to a differential pressure threshold; and

generating, by the at least one processor, an alert signal indicating failure of the hydraulic pump, when the at least one processor determines that the differential temperature exceeds the differential temperature threshold and the differential pressure exceeds the differential pressure threshold.

2. The method of claim 1 , wherein the filter is a case drain filter.

3. The method of claim 1 , wherein the hydraulic pump is one of an engine-driven pump (EDP) or an electric motor pump (EMP).

4. The method of claim 1 , wherein the method further comprises generating, by the at least one processor, an alert signal indicating that the differential temperature exceeds the differential temperature threshold, when the at least one processor determines that the differential temperature exceeds the differential temperature threshold and the differential pressure does not exceed the differential pressure threshold.

5. The method of claim 4 , wherein the alert signal indicating that the differential temperature exceeds the differential temperature threshold further indicates that the hydraulic pump should be monitored.

6. The method of claim 1 , wherein the method further comprises generating, by the at least one processor, an alert signal indicating that the differential pressure exceeds the differential pressure threshold, when the at least one processor determines that the differential pressure exceeds the differential pressure threshold and the differential temperature does not exceed the differential temperature threshold.

7. The method of claim 6 , wherein the alert signal indicating that the differential pressure exceeds the differential pressure threshold further indicates that the hydraulic pump should be one of replaced or monitored.

8. The method of claim 1 , wherein a vehicle comprises the hydraulic pump, the filter, and the reservoir tank.

9. The method of claim 8 , wherein the vehicle is one of an airborne vehicle, a terrestrial vehicle, or a marine vehicle.

10. The method of claim 9 , wherein when the vehicle is the airborne vehicle, the hydraulic pump provides hydraulic power to operate at least one of flight controls, landing gear actuation, nose landing gear steering, high lift devices, or thrust reversers.

11. A system for predicting health of a hydraulic pump, the system comprising:

a reservoir tank temperature sensor to measure a temperature of a reservoir tank;

a hydraulic pump temperature sensor to measure a temperature of the hydraulic pump;

a differential pressure sensor to measure a differential pressure across a filter associated with the hydraulic pump; and

at least one processor to determine a differential temperature by subtracting the temperature of the reservoir tank from the temperature of the hydraulic pump, to compare the differential temperature to a differential temperature threshold, to compare the differential pressure to a differential pressure threshold, and to generate an alert signal indicating failure of the hydraulic pump, when the at least one processor determines that the differential temperature exceeds the differential temperature threshold and the differential pressure exceeds the differential pressure threshold.

12. The system of claim 11 , wherein the filter is a case drain filter.

13. The system of claim 11 , wherein the hydraulic pump is one of an engine-driven pump (EDP) or an electric motor pump (EMP).

14. The system of claim 11 , wherein the at least one processor is further to generate an alert signal indicating that the differential temperature exceeds the differential temperature threshold, when the at least one processor determines that the differential temperature exceeds the differential temperature threshold and the differential pressure does not exceed the differential pressure threshold.

15. The system of claim 14 , wherein the alert signal indicating that the differential temperature exceeds the differential temperature threshold further indicates that the hydraulic pump should be monitored.

16. The system of claim 11 , wherein the at least one processor is further to generate an alert signal indicating that the differential pressure exceeds the differential pressure threshold, when the at least one processor determines that the differential pressure exceeds the differential pressure threshold and the differential temperature does not exceed the differential temperature threshold.

17. The system of claim 16 , wherein the alert signal indicating that the differential pressure exceeds the differential pressure threshold further indicates that the hydraulic pump should be one of replaced or monitored.

18. The system of claim 11 , wherein a vehicle comprises the system.

19. The system of claim 18 , wherein the vehicle is one of an airborne vehicle, a terrestrial vehicle, or a marine vehicle.

20. The system of claim 19 , wherein when the vehicle is the airborne vehicle, the system provides hydraulic power to operate at least one of flight controls, landing gear actuation, nose landing gear steering, high lift devices, or thrust reversers.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 23, 2019
From: CHUNG, DENNIS D.
To: THE BOEING COMPANY
Reel/Frame 048979/0831 →
Continuity (1)
Related Publication 20200340504A1 · Oct 29, 2020