Rapid power response turbine
AssigneeGeneral Electric Company
InventorKenneth O. Johnson
Life of this patent
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Abstract
In one form of the invention, means are provided for sensing changes in electrical power demanded from an electrical generator driven by a gas turbine engine. In response, other means change the rate of fuel and air delivery to the engine in proportion to the demand changes and keep the combustor fuel-air ratio substantially constant.
Claims3
Apparatus for controlling a gas turbine engine having a gas generator stage for supplying exhaust gases to a power turbine stage which drives an electrical generator, the gas generator stage having variable stators, comprising:
- (a) sensing means for sensing the frequency of the power produced by the electrical generator and for producing a frequency signal indicative thereof;
- (b) control means which receives the frequency signal and which, in response, modulates both the fuel supplied to the engine and the variable stators in the engine to maintain combustor fuel-air ratio substantially constant for
- (i) maintaining gas generator speed substantially constant, and
- (ii) maintaining electrical generator speed substantially constant.
Apparatus for controlling a gas turbine engine having a gas generation stage for supplying exhaust gases sequentially to a power turbine stage which drives an electrical generator and then to a heat exchanger stage, comprising:
- (a) sensing means for sensing the frequency of the power produced by the electrical generator and for producing a frequency signal indicative thereof;
- (b) control means which receives the frequency signal and which, in response, modulates the fuel supplied to the engine while maintaining combustor fuel-air ratio substantially constant for
- (i) maintaining gas generator speed substantially constant,
- (ii) maintaining electrical generator speed substantially constant, and
- (iii) maintaining exhaust gas temperature substantially constant.
A method of controlling a gas turbine engine which has a gas generation stage containing variable stators and supplying exhaust gases to a power turbine stage which drives an electrical generator, comprising the following steps:
- (a) sensing the speed of the electrical generator;
- (b) ascertaining a deviation of the speed of (a) from a predetermined speed;
- (c) in response to the deviation of (b), modulating the variable stators and the fuel supplied to the engine so that
- (i) the combustor fuel-air ratio remains substantially constant,
- (ii) the speed of the gas generator stage remains substantially constant, and
- (iii) the deviation of (b) is reduced.
Dependencies are inferred from the claim text.