By throttling the amount of fuel delivered to the combustion chamber
gas turbine generator
Dwight Osten Ness has written: 'Boundary layer control as a method of gas turbine blade cooling' -- subject(s): Aeronautics 'Boundary layer control as a method of gas turbine blade cooling' -- subject(s): Aeronautics
A gas turbine is one type of power plant. It produces power by burning gas to turn the turbine.
Gas Turbine Research Establishment was created in 1959.
The control stages are the stages at which steam is admitted to or extracted from the turbine. These "control" the output of the turbine.
The function of IGV in a gas turbine is to prevent surges and stall conditions.
The first gas turbine in the Gulf started working in the 1970s
Gas turbine power generators are used in two basic configurations. Simple Systems consisting of the gas turbine driving an electrical power generator. You fill them with gas carefully & turn them in.
A diagram of an impulse turbine is in related links.
It's actually fadec (full authority digital engine control)
Westinghouse Aviation Gas Turbine Division was created in 1945.
The gas (working fluid) having flown through the turbine does some work on the turbine, converting its thermal energy into mechanical work produced by the turbine and coming out as an expanding gas with lower temperature and pressure.