Method for categorizing the operating mode of a gas turbine

• US 6,719,526 B2
• Filed: 08/23/2002
• Issued: 04/13/2004
• Est. Priority Date: 08/23/2002
• Status: Active Grant

• Current Assignee: General Electric Company
• Original Assignee: General Electric Company
• Inventors: Sanborn, Stephen Duane, Catharine, Douglas Ancona
• Primary Examiner(s): Look, Edward K.
• Assistant Examiner(s): MCALEENAN, JAMES M
• Application Number:
  US10/226,215
• Publication Number:
  US 20040037697A1
• Time in Patent Office: 599 Days
• Field of Search: 415/1, 415/28, 415/17, 415/119, 415/116, 415/26, 415/13, 415/29, 415/118, 415/123, 416/35, 416/42, 416/170.R, 416/61, 455/66
• US Class Current: 415/118
• 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: F05D 2270/44 active, predictive, or anticipative

Abstract

A method is disclosed for categorizing an operating mode of a gas turbine comprising: monitoring at least one operating condition of the gas turbine; using the operating condition to categorize an operating mode of the gas turbine into one of the plurality of predetermined operating modes, and assigning a value to the categorized operating mode where the value is a number that is a power of a predetermined base number.

Claims

1. A method for tracking an operating mode of a gas turbine comprising:

a. monitoring at least one operating condition of the gas turbine;

b. using the operating condition to categorize an operating mode of the gas turbine into one of the plurality of predetermined operating modes;

c. assigning a value to the categorized operating mode where the value is a number that is a power of a predetermined base number;

d. using the assigned value to select a normal range for an operational parameter for the gas turbine, and

e. determining whether an actual operational parameter for the gas turbine is within said normal range.

2. A method as in claim 1 wherein the base number is two.

3. A method as in claim 1 wherein the predetermined operating modes include a plurality of major modes and a plurality of sub-modes, wherein each of said sub-modes is associated with one of said plurality of major modes.

4. A method as in claim 3 wherein the plurality of major modes include an unknown mode, a startup or shutdown mode, a thermal transient mode, a steady-state mode, and a load transient mode.

5. A method as in claim 4 wherein said plurality of sub-modes includes:

a slow roll or cranking sub-mode, an accelerate high sub-mode, an accelerate low sub-mode, a decelerate high bus-mode, and a decelerate low sub-mode which are associated with the startup or shutdown mode.

6. A method as in claim 1 wherein statistical characteristics of multiple independent measurements of a given operating condition, such as the standard deviation calculated over time for each independent measurement, are used to reduce error in using the operating condition to categorize an operating mode of the gas turbine into one of the plurality of predetermined operating modes.