turbine fuel nozzle
A technology of fuel nozzles and turbines, which is applied in the direction of turbine/propulsion fuel delivery system, fuel control of turbine/propulsion device, gas fuel burner, etc., and can solve problems such as reduction
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[0068] see figure 1 , a turbine constructed in accordance with an exemplary embodiment is shown generally at 2 . The turbine 2 includes a compressor 4 and a plurality of circumferentially spaced combustors, one of which is shown at 6 . Combustor 6 includes a combustor 8 that directs hot gases to a turbine 10 operatively coupled to compressor 4 via a common compressor / turbine shaft or rotor 12 .
[0069] In operation, air flows through the compressor 4 such that the compressed air is supplied to the combustor 6 . Fuel is directed to the combustion chamber 8, mixed with air, and ignited to form combustion gases. The combustion gases are channeled to a turbine 10 where the thermal energy of the gas flow is converted into mechanical rotational energy. Turbine 10 is rotatably coupled to and drives shaft 12 . It should be appreciated that, as used herein, the term "fluid" includes any medium or material that flows and is not limited to gas and / or air. Furthermore, the term "fuel"...
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