OIL DEBRIS MONITORING (ODM) USING ACTIVE VALVE CONFIGURATION CONTROL

• US 20180073970A1
• Filed: 09/14/2016
• Published: 03/15/2018
• Est. Priority Date: 09/14/2016
• Status: Active Grant

• Current Assignee: Rtx Corporation
• Original Assignee: United Technologies Corporation (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Hagen, Gregory S.
• Granted Patent: US 10,302,541 B2
• Time in Patent Office: Days
• CPC Class Codes: F01D 21/003 Arrangements for testing or measuring for measuring vibrations G01H
• CPC Class Codes: F01D 21/10 responsive to unwanted deposits on blades, in working-fluid conduits or the like
• CPC Class Codes: F01D 25/18 Lubricating arrangements of machines or engines in general F01M
• CPC Class Codes: F02C 7/06 Arrangements of bearings bearings F16C; Lubricating of turbo machines F01D25/18; of machines or engines in general F01M
• CPC Class Codes: F05D 2220/32 in gas turbines
• CPC Class Codes: F05D 2260/607 Preventing clogging or obstruction of flow paths by dirt, dust, or foreign particles
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F05D 2260/98 Lubrication
• CPC Class Codes: G01N 15/02 Investigating particle size or size distribution by measuring osmotic pressure G01N7/10; investigating sedimentation of particle suspensions G01N15/04; investigating individual particles G01N15/10
• CPC Class Codes: G01N 15/0606 by collecting particles on a support
• CPC Class Codes: G01N 27/74 of fluids G01N24/00 takes precedence
• CPC Class Codes: G01N 33/2858 metal particles
• CPC Class Codes: G01N 33/2888 Lubricating oil characteristics, e.g. deterioration lubricating properties G01N33/30
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

A gas turbine engine, a method, and a system for detecting oil debris are provided. The gas turbine engine includes an oil debris monitor sensor configured to detects oil debris in an oil flow, and generate a sensor signal based on the detected oil debris, a controller configured to control the oil flow through the oil debris monitor sensor using a plurality of valves, and a signal processor configured to receive the sensor signal from the oil debris monitor and to receive a valve system configuration from the controller, the signal processor further configured to generates a health indicator based on the sensor signal and valve configuration.

Claims

1. A gas turbine engine with oil debris monitoring comprising:

an oil debris monitor sensor configured to detect oil debris in an oil flow, and generate a sensor signal based on the detected oil debris;

a controller configured to control the oil flow through the oil debris monitor sensor using a plurality of valves; and

a signal processor configured to receive the sensor signal from the oil debris monitor and to receive a valve system configuration from the controller, the signal processor further configured to generates a health indicator based on the sensor signal and valve configuration.

2. The gas turbine engine with oil debris monitoring of claim 1,

wherein the health indicator includes at least one of an estimated value of debris in the oil flow, a type of debris, a calculated size of debris particulate, and a calculated amount of debris in the oil over time.

3. The gas turbine engine with oil debris monitoring of claim 1,

wherein the signal processer receives health indicators over time, and detects and anomaly in the oil debris based on the health indicators over time.

4. The gas turbine engine with oil debris monitoring of claim 3,

wherein the signal processor receives information characterizing the valve system configurations history over time and detects the anomaly in the oil debris based on the valve system configurations over time and the health indicators over time.

5. The gas turbine engine with oil debris monitoring of claim 1,

wherein the oil debris monitor sensor is configured to detect oil debris by detecting one or more of at least a magnetic field and a disturbance to an expected magnetic field through the oil flow and to calculate an oil debris amount that corresponds to the magnetic field detected.

6. The gas turbine engine with oil debris monitoring of claim 1, wherein the plurality of valves further comprises:

an oil flow bypass valve connected in parallel with the oil debris monitor sensor; and

an oil flow regulator valve connected in series with the oil debris monitor sensor.

7. The gas turbine engine with oil debris monitoring of claim 6,

wherein the oil flow bypass valve is configured to adjust the oil flow through an oil flow bypass to control the flow of the oil flow through the oil debris monitor sensor, and

wherein the oil flow regulator valve is configured to adjust the oil flow through an oil flow bypass to control the flow of the oil flow through the oil debris monitor sensor.

8. The gas turbine engine with oil debris monitoring of claim 6,

wherein the oil flow bypass valve is further configured to adjust flow through the bypass valve based on at least one of a temperature of oil, pressure of oil, quantity of oil, opening and closing of other valves from the plurality of valves, oil flow through the oil debris monitor sensor, mechanical load, mode of operation, and shaft speeds.

9. The gas turbine engine with oil debris monitoring of claim 1,

wherein the plurality of valves are configured to determine the oil flow through the oil debris monitor sensor, and

wherein the controller is configured to adjust the valve system configuration using the control signals to control the plurality of valves to control the oil flow through the oil debris monitor sensor.

10. The gas turbine engine with oil debris monitoring of claim 1,

wherein the plurality of valves includes at least an actively controlled valve and a passively controlled valve.

11. The gas turbine engine with oil debris monitoring of claim 10,

wherein the actively controlled valve is driven by the controller in order to provide lubrication system performance to meet the needs of a current state of operation of the mechanical system.

12. The gas turbine engine with oil debris monitoring of claim 10,

wherein the passively controlled valve is configured to respond directly to the mechanical properties of the mechanical system.

13. The gas turbine engine with oil debris monitoring of claim 12,

wherein the passively controller valve is a pressure-driven bypass valves.

14. A computer implemented method for oil debris monitoring in a gas turbine engine, the method comprising:

generating control signals to control an oil flow using a plurality of valves in response to a sensor signal indicating oil debris in the oil flow;

receiving a valve system configuration; and

generating, using a signal processor, a health indicator based on the sensor signal and the valve configuration.

15. The computer implemented method of claim 14,

wherein the health indicator includes at least one of an estimated value of debris in the oil flow, a type of debris, a calculated size of debris particulate, and a calculated amount of debris in the oil over time.

16. The computer implemented method of claim 14, further comprising:

detecting, using an oil debris monitor sensor, oil debris by detecting one or more of at least a magnetic field and a disturbance to an expected magnetic field through the oil flow and calculating an oil debris amount that corresponds to the magnetic field detected.

17. The computer implemented method of claim 14, further comprising:

adjusting, using at least one of an oil flow bypass valve and regulator valve, the oil flow through at least one of the oil flow bypass valve and regulator valve to control the flow of the oil flow through an oil debris monitor sensor.

18. The computer implemented method of claim 14, further comprising:

adjusting, using an oil flow bypass valve, flow through the bypass valve based on at least one of a temperature of oil, pressure of oil, quantity of oil, opening and closing of other valves from the plurality of valves, oil flow through the oil debris monitor sensor, mechanical load, mode of operation, and shaft speeds.

19. The computer implemented method of claim 14,

wherein the plurality of valves determine the oil flow through an oil debris monitor sensor, and

wherein a controller adjusts the valve system configuration using the control signals to control the plurality of valves to control the oil flow through the oil debris monitor sensor.

20. A computer program product for oil debris monitoring in a gas turbine engine, the computer program product comprising a computer readable storage medium having program instructions embodied therewith, the program instructions executable by a processor to cause the processor to:

generate control signals to control an oil flow using a plurality of valves in response to a sensor signal indicating oil debris in the oil flow;

receive a valve system configuration; and

generate a health indicator based on the sensor signal and the valve configuration.