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US4039804A Expired / Lapsed US ⏱️ 0.0 years remaining

System and method for monitoring industrial gas turbine operating parameters and for providing gas turbine power plant control system inputs representative thereof

Assignee: Westinghouse Electric Corp
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Filing: 1973-10-04
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Granted: 1977-08-02
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Expires: 1993-10-04
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Abstract

Abstract A hybrid digital computer gas turbine power plant control system which may operate in a multiple-control loop arrangement is provided with selected process variable monitoring means. Control system inputs representative of current values of such variables are continuously available to provide positive highly responsive control over a broad range of gas turbine operating conditions. Predictable process sensor errors are effectively eliminated by means of programmed computer operations to thereby insure highly accurate control variable derivation essential to maintaining gas turbine operation at or near design limits.

Inventors

  • 👤 Terry J. Reed
  • 👤 Robert A. Yannone

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 09:13
CPC Classifications
F; F02; F02C; F02C9/00; F02C9/26; F02C9/32; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 3
Claim 1
Independent Claim 199 words
A machine implemented method for operating industrial gas turbine apparatus including a gas turbine having compressor, combustion and turbine elements, a fuel system for supplying fuel to the combustion element, and a process sensor for monitoring a selected process parameter of gas turbine operation by generating a signal representative thereof utilizable for scheduling fuel flow from said fuel system to said combustion element and means for storing signals of the type generated by said sensor, the steps of said method comprising a. generating a signal representative of the value of said parameter at a time when said value is known, b. comparing the actual value of the signal generated at said time to the known value of said parameters, c. storing the difference between the known value of said parameters and the actual value of the signal generated, d. determining, from said stored difference value, a calibration value for said process sensor, e. utilizing said calibration value in correctively adjusting the value of successive parameter generated signals representative of the value of said parameter, and f. scheduling fuel flow from said fuel system to said combustion element at least in part as a function of said adjusted signal values.
Claim 2
Dependent Claim 199 words
A machine implemented method for operating industrial gas turbine apparatus including a gas turbine having compressor, combustion and turbine elements, a fuel system for supplying fuel to the combustion element, and a process sensor for monitoring a selected process parameter of gas turbine operation by generating a signal representative thereof utilizable for scheduling fuel flow from said fuel system to said combustion element and means for storing signals of the type generated by said sensor, the steps of said method comprising a. generating a signal representative of the value of said parameter at a time when said value is known, b. comparing the actual value of the signal generated at said time to the known value of said parameters, c. storing the difference between the known value of said parameters and the actual value of the signal generated, d. determining, from said stored difference value, a calibration value for said process sensor, e. utilizing said calibration value in correctively adjusting the value of successive parameter generated signals representative of the value of said parameter, and f. scheduling fuel flow from said fuel system to said combustion element at least in part as a function of said adjusted signal values.
Claim 3
Dependent Claim 27 words
The method recited in claim 1 and further comprising the step of limiting compressor surge at least in part as a function of said adjusted parameter values.

References Cited (Backward Citations)

US3400374A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1980-08-01 1981-01-31 1981-08-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1984-08-01 1985-01-31 1985-08-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1988-08-01 1989-01-31 1989-08-02 $7700.00 Window Closed / Lapsed

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