System and method for turbine engine startup profile characterization

• US 7,506,517 B2
• Filed: 09/30/2005
• Issued: 03/24/2009
• Est. Priority Date: 11/23/2004
• Status: Active Grant

• Current Assignee: Honeywell International Inc.
• Original Assignee: Honeywell International Inc.
• Inventors: Kim, Kyusung, Uluyol, Onder, Ball, Charles M.
• Primary Examiner(s): BARNES-BULLOCK, CRYSTAL JOY
• Application Number:
  US11/239,882
• Publication Number:
  US 20070234734A1
• Time in Patent Office: 1,271 Days
• Field of Search: 607/76, 607/78, 607/86, 607/87, 607/90, 608/00, 602/84, 602/86, 701/29, 701/34, 701/99, 701/100, 702/130, 702/182, 702/183, 702/185, 123/179.17, 123/305, 123/491, 123/641, 324/115, 340/945, 340/973
• US Class Current: 60/786
• CPC Class Codes: F02C 7/26 Starting; Ignition
• CPC Class Codes: F05D 2260/80 Diagnostics
• CPC Class Codes: F05D 2270/303 Temperature
• CPC Class Codes: F05D 2270/304 Spool rotational speed
• CPC Class Codes: G05B 23/0232 based on qualitative trend analysis, e.g. system evolution

Abstract

A system and method is provided for startup characterization in a turbine engine that provides the ability to accurately characterize engine startup. The startup characterization system and method uses engine temperature sensor data and engine speed sensor data to accurately characterize the startup of the turbine engine by determining when several key engine startup conditions are reached. By storing and analyzing engine sensor data taken during these key conditions of engine startup, the system and method is able to accurately characterize the performance of the engine during startup. This information can be used as part of a trending system to determine when faults in the start transient regime are occurring or likely to occur. Additionally, this information can be used in real time by control systems to better control the startup and operation of the turbine engine.

Claims

1. A method of characterizing startup in a turbine engine, the method comprising the steps of:

receiving engine temperature sensor data and engine speed sensor data for the turbine engine during startup;

determining an engine speed peak gradient time of the engine speed sensor data during startup;

determining an engine temperature peak gradient time of the engine temperature sensor data;

determining a lightoff time of the turbine engine during startup;

determining a 3rd phase time of the turbine engine during startup;

determining a peak temperature time of the turbine engine sensor data; and

capturing engine data corresponding to the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.

2. The method of claim 1 further comprising the step of providing the captured engine data comprises to a fault detection system or an engine control system.

3. The method of claim 1 wherein the step of capturing engine data comprises capturing at least one of time data, a snapshot of engine temperature data and a snapshot of engine speed data corresponding to each of the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.

4. The method of claim 1 wherein the step of capturing engine data comprises capturing engine temperature gradient data and engine speed gradient data.

5. The method of claim 1 wherein the step of capturing engine data comprises capturing hot section temperature data or exhaust gas temperature data.

6. The method of claim 1 wherein the step of capturing engine data comprises capturing rotational fan speed data or rotational core speed data.

7. The method of claim 1 wherein the step of capturing engine data comprises capturing power lever angle data.

8. A system for characterizing startup in a turbine engine, the system comprising:

an engine temperature analyzer, the engine temperature analyzer receiving engine temperature sensor data from the turbine engine to determine an engine temperature peak gradient time of the engine temperature sensor data and a peak temperature time of the turbine engine sensor data;

an engine speed analyzer, the engine speed analyzer receiving engine speed sensor data from the turbine engine to determine an engine speed peak gradient time of the engine speed sensor data; and

a condition estimator, the condition estimator determining a lightoff time of the turbine engine during startup and a 3rd phase time of the engine during startup, the condition estimator capturing engine data corresponding to the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.

9. The system of claim 8 wherein the condition estimator further provides the engine temperature data and engine speed data to a fault detection system or an engine control system.

10. The system of claim 8 wherein the engine data comprises hot section temperature data or exhaust gas temperature data.

11. The system of claim 8 wherein the engine data comprises rotational fan speed data or rotational core speed data.

12. The system of claim 8 wherein the engine data comprises power lever angle data.

13. The system of claim 8 wherein the engine data comprises capturing engine temperature gradient data and engine speed gradient data.

14. The system of claim 8 wherein the engine data comprises at least one of time data, a snapshot of engine temperature data and a snapshot of engine speed data corresponding to each of the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.

15. A computer readable medium encoding a computer program product, the program product comprising:

a turbine engine startup characterization program, the turbine engine startup characterization program including;

an engine temperature analyzer, the engine temperature analyzer receiving engine temperature sensor data from the turbine engine to determine an engine temperature peak gradient time of the engine temperature sensor data and a peak temperature time of the turbine engine sensor data;

an engine speed analyzer, the engine speed analyzer receiving engine speed sensor data from the turbine engine to determine an engine speed peak gradient time of the engine speed sensor data; and

a condition estimator, the condition estimator determining a lightoff time of the turbine engine during startup and a 3rd phase time of the engine during startup, the condition estimator capturing engine data corresponding to the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.

16. The program product of claim 15 wherein the condition estimator further provides the captured engine data to a fault detection system or to an engine control system.

17. The program product of claim 15 wherein the engine data comprises hot section temperature data or exhaust gas temperature data.

18. The program product of claim 15 wherein the engine data comprises rotational fan speed data or rotational core speed data.

19. The program product of claim 15 wherein the engine data comprises power lever angle data.

20. The program product of claim 15 wherein the engine data comprises at least one of time data, a snapshot of engine temperature data and a snapshot of engine speed data corresponding to each of the engine speed peak gradient time, the engine temperature peak gradient time, the engine lightoff time, the 3rd phase time, and the peak temperature time to characterize the turbine engine during startup.