Turboprop aircraft gas turbine. Gas turbines are being increasingly used for power generation, when they are used in combination with steam turbines to make a CCGT power plant. A schematic diagram of such a plant is shown in Fig. 17.5(a). This has been much simplified, and usually more ...
The function of the regenerator is to use gas generator exhaust vapors to preheat the air exiting the air compressor, thus reducing the amount of fuel required by the gas turbine. Figure 6.1.5 also shows the changes of gas temperature, pressure, energy, and the horsepower produced in the ...
1. A method for monitoring at a remote monitoring center a turbine driven by a supply of high temperature combustion gas generated by combustion in a combustor, the method comprising: a first step of receiving second data containing representative values within a predetermined period of time in a...
Gas turbine control device is disclosed to generate for the phasor power that gasifies. Gas turbine control device, because using burning gases by burner combustion, not only can remove the interference of evaporating method with gas turbine, and can prevent damage to gas turbine by including; ...
Because of the constant volume of gas turbine, the output power is decreased. Different from the TIT operating strategy, more high-temperature flue gas is produced resulting in more production of cooling and heating. Consequently, the flue energy saving ratio and over efficiency of the system is...
The engine model consists of 6 parts intake and exhaust manifold, the cylinder, the turbine, EGR valve system, and the compressor system. A schematic diagram of the engine is shown in Fig. 1. In this section, we briefly discuss the equation required for the present study and these are tak...
An apparatus for controlling a gas turbine engine. A control device is provided for controlling the energy conversion function of the engine. Adjustments of the control device are obtained by comparing an actual value of a condition of the engine with a
1.A gas turbine that supplies combustion gas generated by supplying fuel to a combustor where the fuel is combusted with compressed air compressed at a compressor to a turbine to acquire rotational power, the gas turbine comprising:pressurizing means connected to a branching channel branching from...
Gas turbine unit (GTV) provides compressed air and steam methane-hydrogen mixture to a combustion chamber to enrich combustion products and cooling by evaporation or superheating of
In a gas turbine combustor, mixing of a fuel and air is accelerated in a mixing chamber of a burner as well as in air introduction passages provided in a wall of the mixing chamber, whereby NOx emissi