Method and apparatus for assessing the impact of individual parts of a gas turbine component on the overall thermal performance of a gas turbine

• US 20030125906A1
• Filed: 12/28/2001
• Published: 07/03/2003
• Est. Priority Date: 12/28/2001
• Status: Abandoned Application

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Guaglardi, Paul A.
• Application Number:
  US10/028,936
• Publication Number:
  US 20030125906A1
• Time in Patent Office: Days
• US Class Current: 702/182
• CPC Class Codes: G05B 23/0251 Abstraction hierarchy, e.g. "complex systems", i.e. system is divided in subsystems, subsystems are monitored and results are combined to decide on status of whole system

Abstract

A method of determining performance impact of a gas turbine component on overall thermal performance of a gas turbine. The method includes obtaining measured physical condition data for a select gas turbine component part. The measured physical condition data is compared with a predetermined reference value for the select gas turbine component part to determine a deviation of the measured physical condition data with respect to the predetermined reference value. The impact of the deviation on the overall thermal performance of the gas turbine is subsequently determined.

Claims

1. A method of determining performance impact of a gas turbine component on overall thermal performance of a gas turbine, the method comprising:

(a) obtaining measured physical condition data for a select gas turbine component part;

(b) comparing the measured physical condition data with a predetermined reference value for the select gas turbine component part;

(c) determining a deviation of the measured physical condition data with respect to the predetermined reference value; and

(d) determining an impact of the deviation on the overall thermal performance of the gas turbine.

2. The method as in claim 1, wherein step (d) is determined by correlating a deviation value with a corresponding predetermined overall thermal performance effect factor.

3. The method as in claim 1, wherein step (a) further comprises:

measuring the physical condition of the select gas turbine component to obtain the measured physical condition data;

storing the measured physical condition data in a memory.

4. The method as in claim 1, wherein step (b) is performed using a processor.

5. The method as in claim 1, further comprising:

(e) displaying an indication of the impact on the overall thermal performance of the gas turbine.

6. An apparatus for determining performance impact of a gas turbine component part on overall thermal performance of the gas turbine, comprising:

means for obtaining measured physical condition data for a select gas turbine component part;

means for comparing the measured physical condition data of the select gas turbine component part with a corresponding predetermined reference value;

means for determining a deviation of the measured physical condition data with respect to the predetermined reference value; and

means for determining an impact of the deviation on the overall thermal performance of the gas turbine.

7. The apparatus as in claim 6, wherein an impact of the deviation is determined by correlating a deviation value with a corresponding predetermined performance effect factor.

8. The apparatus as in claim 6, further comprising:

a memory for storing the measured physical condition data of the select gas turbine component part.

9. The apparatus as in claim 6, further comprising:

means for displaying an indication of the impact on the overall performance of the gas turbine.

10. The apparatus as in claim 6, wherein the determining means uses empirically developed trade factors and theoretically derived relationships to determine the impact of deviation.

11. A computer program product comprising a computer useable medium having computer program logic stored thereon for enabling a processor in a computer system to process data, said computer program product when executed by the processor performing the steps of:

(a) comparing measured physical condition data of a select gas turbine component part with a corresponding predetermined reference value;

(b) determining a deviation of the measured physical condition data with respect to the predetermined reference value; and

(c) determining an impact of the deviation on the overall thermal performance of the gas turbine.

12. In a combined cycle power plant having a plurality of components, each component having a plurality of component parts, a method for determining performance impact of a component part on overall thermal performance of the power-plant, the method comprising:

(a) obtaining measured physical condition data for a select component part;

(b) comparing the measured physical condition data with a corresponding predetermined reference value;

(c) determining a deviation of the measured physical condition data with respect to the predetermined reference value; and

(d) determining an impact of the deviation on the overall thermal performance of the power plant.

13. The method as in claim 12, wherein step (d) is determined by correlating the deviation value with a corresponding predetermined overall thermal performance effect factor.

14. The method as in claim 12, further comprising:

(e) displaying an indication of the impact on the overall thermal performance of the power plant.

15. A computer-based method for providing assistance to a user of an application program for assessing performance impact of a gas turbine component part on overall thermal performance of a gas turbine, the method comprising:

obtaining measured physical condition data of a select gas turbine component part;

using an application program to determine a deviation of the measured physical data with respect to a corresponding reference value; and

determining an impact of the deviation on the overall thermal performance of the gas turbine by correlating the deviation with a corresponding predetermined thermal performance effect factor.