Gas turbine fuel injector with metering cavity
A technology of fuel injectors and gas turbines, which is applied in the direction of gas turbine devices, fuel valves of turbine/propulsion devices, turbine/propulsion fuel delivery systems, etc., and can solve problems that are not conducive to GTE current limitation
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[0012] figure 1 An exemplary gas turbine engine (GTE) 10 is shown. GTE 10 may have compressor system 12 , combustor system 14 , turbine system 16 , and exhaust system 18 disposed along engine shaft 98 , among other systems. Compressor system 12 compresses air to high pressure and temperature (approximately 200 psi and 800°F (426.7°C) respectively) and delivers the compressed air to casing 20 of combustor system 14 . The compressed air is then directed from the housing 20 into one or more fuel injectors 50 located therein. The compressed air is mixed with fuel in fuel injector 50 and the mixture is introduced into combustion chamber 22 . The fuel-air mixture ignites and combusts in combustion chamber 22 to produce combustion gases. These combustion gases are directed to a turbine system 16 . A turbine system 16 extracts energy from the combustion gases and discharges the exhaust into the atmosphere through an exhaust system 18 . As mentioned above, figure 1 The configurat...
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