SYSTEM AND METHOD FOR MONITORING THERMAL STATE TO NORMALIZE ENGINE TRENDING DATA

• US 20020173897A1
• Filed: 05/18/2001
• Published: 11/21/2002
• Est. Priority Date: 05/18/2001
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Leamy, Kevin Richard, Maruscik, Ronald George
• Granted Patent: US 6,498,978 B2
• Time in Patent Office: Days
• US Class Current: 701/100
• CPC Class Codes: F02C 9/28 Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed F02C9/30 - F02C9/38, F02C9/44 take precedence
• CPC Class Codes: F05D 2220/50 for auxiliary power units (APU's)

Abstract

A method and system for monitoring engine performance in a gas turbine engine uses a plurality of sensors to sense data related to the operation and performance of the gas turbine engine. Selected data parameters from the sensed data are continuously sampled prior to completion of an engine start sequence. The selected data parameters are then evaluated to determine whether specific criteria have been met, and evaluation data are captured whenever the criteria are met. The evaluation data are used to normalize engine performance data to a particular thermal state of the engine. The normalized engine performance data are then trended by comparing it to a parametric baseline for the gas turbine engine.

Claims

1. A method of monitoring engine performance in a gas turbine engine, said method comprising:

sensing data related to the operation and performance of said gas turbine engine;

continuously sampling selected data parameters from said sensed data prior to completion of an engine start sequence;

evaluating said data parameters to determine whether specific criteria have been met;

capturing evaluation data when said specific criteria are met; and

using said evaluation data to normalize engine performance data to a particular thermal state of said gas turbine engine.

2. The method of claim 1 wherein said selected data parameters include one or more of core speed and fuel flow.

3. The method of claim 1 wherein said gas turbine engine includes a starter valve and said criteria include said starter valve being open.

4. The method of claim 1 wherein said criteria include core speed exceeding a predetermined value.

5. The method of claim 1 wherein said criteria include fuel flow being off.

6. The method of claim 1 wherein said evaluation data include one or more of oil temperature, high pressure turbine shroud temperature, ambient temperature, exhaust gas temperature and core speed.

7. The method of claim 1 further comprising trending said normalized engine performance data by comparing it to a parametric baseline for said gas turbine engine.

8. The method of claim 1 wherein normalizing engine performance data to a particular thermal state includes determining said gas turbine engine'"'"'s thermal state at engine start-up from said evaluation data.

9. A method of monitoring engine performance in a gas turbine engine, said method comprising:

using a plurality of sensors to sense data related to the operation and performance of said gas turbine engine;

initiating an engine start sequence for said gas turbine engine;

continuously sampling selected data parameters from said sensed data prior to completion of said engine start sequence;

continuously sampling engine performance data parameters from said sensed data;

evaluating said selected data parameters to determine whether specific criteria have been met;

capturing evaluation data when said specific criteria are met;

using said evaluation data to assess said gas turbine engine'"'"'s thermal state at engine start-up;

normalizing said engine performance data parameters for said thermal state; and

trending said normalized engine performance data parameters by comparing them to a parametric baseline for said gas turbine engine.

10. The method of claim 9 wherein said selected data parameters include one or more of core speed and fuel flow.

11. The method of claim 9 wherein said gas turbine engine includes a starter valve and said criteria include said starter valve being open.

12. The method of claim 9 wherein said criteria include core speed exceeding a predetermined value.

13. The method of claim 9 wherein said criteria include fuel flow being off.

14. The method of claim 9 wherein said evaluation data include one or more of oil temperature, high pressure turbine shroud temperature, ambient temperature, exhaust gas temperature and core speed.

15. The method of claim 9 further comprising trending said normalized engine performance data by comparing it to a parametric baseline for said gas turbine engine.

17. The system of claim 16 wherein said means for using said evaluation data to normalize engine performance data to a particular thermal state of said gas turbine engine includes means for determining said gas turbine engine'"'"'s thermal state.

16. A system for monitoring engine performance in a gas turbine engine, said system comprising:

a plurality of sensors for sensing data related to the operation and performance of said gas turbine engine;

means for continuously sampling selected data parameters from said sensors prior to completion of an engine start sequence;

means for evaluating said data parameters to determine whether specific criteria have been met;

means for capturing evaluation data when said specific criteria are met; and

means for using said evaluation data to normalize engine performance data to a particular thermal state of said gas turbine engine.

18. A computer-readable medium containing instructions for controlling a computer-based system having a plurality of sensors for sensing predetermined parameter values related to the operation and performance of a gas turbine engine to perform a method comprising the steps of:

continuously sampling selected data parameters from said sensors prior to completion of an engine start sequence;

evaluating said data parameters to determine whether specific criteria have been met;

capturing evaluation data when said specific criteria are met; and

using said evaluation data to normalize engine performance data to a particular thermal state of said gas turbine engine.