Method of operating a gas turbine and a process and apparatus for fuel control for gas turbines
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United States of America Patent
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Apr 18, 1995
Issued Date -
N/A
app pub date -
Nov 23, 1993
filing date -
Jul 3, 1992
priority date (Note) -
Expired
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Abstract
A process and apparatus for controlling flow of fuel in a gas turbine has a fuel control unit which comprises piston pumps which have at least two piston elements working in opposite phase to one another, and which can be operated in opposite phase, so that the flow of fuel to the injector nozzle is sufficiently constant. This constancy of the fuel flow is thereby a function of the delivery frequency and the number of pump piston elements operating in parallel.
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