US 5,487,265 AGranted

Gas turbine coordinated fuel-air control method and apparatus therefor

AssigneeGeneral Electric Company

InventorsRavi Rajamani, Karl D. Minto, Benjamin E. Bulkley, Bruce G. Norman

Life of this patent

Estimating the term…

Loading patent…

Abstract

A method of minimizing undesirable emissions from and acoustic pressure oscillations in a gas turbine includes the step of coordinating modulation of turbine fuel and air supply signals to maintain the fuel air ration (FAR) within a selected range. Coordination of the modulation of fuel and air supply signals includes the steps of producing a turbine fuel supply control signal in correspondence with a turbine speed error signal, generating a coordinated turbine exhaust temperature error signal by modifying a preliminary turbine exhaust temperature error signal in correspondence with the speed error signal, and producing a turbine air supply control signal from the coordinated turbine exhaust temperature error signal; the coordinated turbine exhaust temperature error signal provides coordination between the turbine fuel supply signal and the turbine air supply signal so as to maintain the fuel-air ratio of the combustible mixture being fed to the turbine within the selected range.

Claims16

Dependent claims

A method for operating a gas turbine so as to reduce undesirable emissions and acoustic pressure oscillations, the method comprising the step of coordinating the modulation of respective turbine fuel supply and air supply signals so as to maintain the fuel-air ratio of the fuel air combustible mixture supplied to the turbine substantially constant over loaded operating conditions of said gas turbine in which both fuel and air supply to said turbine is modulated, coordinating the modulation of turbine fuel supply and air supply further comprising the steps of:

generating a turbine speed error signal by comparing actual turbine speed with a selected turbine reference speed;
generating a preliminary turbine exhaust temperature error signal by comparing actual turbine exhaust temperature with a selected turbine exhaust reference temperature;
producing a turbine fuel supply control signal in correspondence with said speed error signal;
generating a coordinated turbine exhaust temperature error signal by modifying said preliminary turbine exhaust temperature error signal in correspondence with a temperature error modification signal, said temperature error modification signal being processed from said turbine speed error signal with a time delay transfer function;
and
producing a turbine air supply signal from said coordinated turbine exhaust temperature error signal;
said coordinated turbine exhaust temperature error signal providing coordination between said turbine fuel supply signal and said turbine air supply signal so as to maintain the fuel-air mixture in said gas turbine substantially constant.

4 more elements

A gas turbine control system for providing reduction of undesirable emissions from and acoustic pressure oscillations in a gas turbine in which fuel and air supply is modulated to provide a combustible mixture of fuel and air, comprising:

a turbine control unit coupled to a gas turbine to receive a plurality of respective turbine operating parameter signals and further coupled to apply selected respective regulatory function control signals to said gas turbine;
said turbine control unit comprising a coordinating processor unit adapted for coordinating control of gas turbine fuel supply and gas turbine air supply such that the fuel-air ratio of the said combustible mixture entering the combustion chamber of said turbine is maintained substantially constant over loaded operating conditions of said gas turbine in which both fuel and air supply is modulated by said turbine controller;
said coordinating processor unit comprising:
a fuel supply controller;
an air supply controller
a first processing means for comparing a reference turbine speed signal and an actual turbine speed signal to generate a turbine speed error signal, said first processing means being coupled to said fuel supply controller;
a second processing means for comparing a reference turbine exhaust temperature signal and an actual turbine exhaust temperature signal to generate a preliminary turbine exhaust temperature error signal, said second processing means being coupled to said air supply controller;
and
a time delay cross channel controller coupled respectively to said fuel supply controller and said air supply controller and adapted for processing said turbine speed error signal in correspondence with a selected time delay transfer function to generate a temperature error modification signal.

6 more elements

Dependencies are inferred from the claim text.