Integrated health management approach to propulsion control system protection limiting

• US 9,435,267 B2
• Filed: 03/11/2014
• Issued: 09/06/2016
• Est. Priority Date: 03/15/2013
• Status: Active Grant

• Current Assignee: Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Original Assignee: Rolls-Royce Corporation (Rolls-Royce Holdings Plc), Rolls-Royce North American Technologies, Inc. (Rolls-Royce Holdings Plc)
• Inventors: Myer, Joseph D., Skertic, Richard J., Calhoun, Keith A.
• Primary Examiner(s): Black, Thomas G
• Assistant Examiner(s): LOUIE, WAE LENNY
• Application Number:
  US14/204,619
• Publication Number:
  US 20140277992A1
• Time in Patent Office: 910 Days
• Field of Search: 701/100, 701/102
• US Class Current: 1/1
• CPC Class Codes: B60C 11/24 Wear-indicating arrangements
• CPC Class Codes: F02C 9/00 Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants controlling air intakes F02C7/057; controlling turbines F01D; controlling compressors F04D27/00; controlling in general G05
• CPC Class Codes: F02D 41/2422 Selective use of one or more tables
• CPC Class Codes: G05B 23/0291 Switching into safety or degraded mode, e.g. protection and supervision after failure
• CPC Class Codes: H04B 1/7163 using impulse radio
• CPC Class Codes: H05B 45/48 having LEDs organised in strings and incorporating parallel shunting devices

Abstract

A real-time engine management system having a controller system configured to control demand on a first component of an engine. The controller system is also configured to access a first set of prognostic data about the first component, where the first set of prognostic data includes a remaining lifespan approximation of the first component operating at a present operating condition. The controller system is also configured to identify a temporal length of an engine procedure operating at the present operating condition, alter a current limit constant associated with the first component to increase the remaining lifespan approximation of the first component beyond the temporal length, and implement the current limit constant associated with the first component so that the first component does not fault during the engine procedure.

Claims

1. An engine system comprising:

a controller system that controls demand on a first component of an engine, wherein the controller system includes at least one controller and is configured to;

access a first set of prognostic data about the first component, wherein the first set of prognostic data includes a remaining lifespan approximation of the first component operating at a present operating condition;

identify a temporal length of an engine procedure operating at the present operating condition;

decrease a maximum hard current limit of the first component to increase the remaining lifespan approximation of the first component beyond the temporal length; and

implement the current limit constant associated with the first component so that the first component does not fault during engine operation.

2. The system as claimed in claim 1, wherein the engine provides propulsive power in a transportation vehicle.

3. The system as claim in claim 1, the controller system further generates the first set of prognostic data.

4. The system as claimed in claim 1, the controller system further receives a user input to override the implementation of the current limit constant associated with the first component.

5. The system as claimed in claim 1, wherein the first component is a fuel pump metering unit.

6. The system as claimed in claim 1, the system further alters an additional current limit constant associated with the first component to increase the remaining lifespan approximation of a second component beyond the temporal length.

7. The system as claimed in claim 1, wherein the system further:

accesses a second set of prognostic data associated with a second component of the engine, wherein the second set of prognostic data associated with the second component includes a remaining lifespan approximation of the second component operating at the present operating condition;

alters a current limit constant associated with the second component to increase the remaining lifespan approximation of the second component beyond the temporal length; and

implements the current limit constant associated with the second component so that the second component does not fault during engine operation.

8. A system comprising:

an engine having a plurality of components each respectively configured to carry out a plurality of engine tasks;

a controller that manipulates operating conditions of each the plurality of components; and

a computer with a processor that;

identifies a first component predicted to fail during an active engine operation from the plurality of components;

determines at least one new operating condition for the first component such that when implemented by the controller the first component will no longer be predicted to fail, where the at least one new operating condition includes a new maximum hard limit constant that is lower than a present maximum hard current limit; and

causes the controller to implement the at least one new operating condition so that the first component is no longer predicted to fail during the active operation.

9. The system claimed in claim 8, wherein the at least one new operating condition is a new current limit constant.

10. The system claimed in claim 8, wherein the processor indicates that the first component will fail during the active engine operation.

11. The system claimed in claim 8, wherein the at least one new operating condition saturates current passed through the first component.

12. The system claimed in claim 8, wherein the at least one new operating condition is a new first and second current limit constant.

13. A method comprising:

identifying, by way of a processor, a first engine component that is predicted to fail during an active on-station operation, wherein identifying the first engine component occurs during the active on-station procedure;

decreasing, by way of the processor, a first maximum hard current limit constant during the active on-station procedure to provide a new first engine component limit protection to the first engine component, wherein decreasing the first maximum hard current limit constant alters the active on-station procedure to an altered active on-station procedure; and

determining, by way of the processor, that the first engine component working under the new first engine component limit protection is predicted to successfully perform during the altered active on-station procedure.

14. The method of claim 13, further comprising generating a set of prognostic data about the first component.

15. The method of claim 14, wherein the identifying the first engine component that is predicted to fail is based on generating the set of prognostic data about the first component.

16. The method claimed in claim 13 further comprising;

identifying a second engine component that is predicted to fail during the active on-station procedure, wherein identifying the second engine component occurs during the active on-station procedure;

adjusting a second current limit constant during the active on-station procedure to provide a new second engine component limit protection to the second engine component, wherein adjusting the second current limit constant alters the altered active on-station procedure to a second altered active on-station procedure; and

determining that the second engine component is predicted to successfully perform during the second altered active on-station procedure.

17. The method of claim 16 further comprising generating a set of prognostic data associated with the second component.

18. The method of claim 13, wherein the first engine component is a fuel pump metering unit.

19. The method of claim 13, wherein decreasing the first maximum hard current limit constant employs a least wins logic scheme.

20. The method as claimed in claim 13, further comprising receiving a user input to override the new first engine component limit protection.