Turbine assembly and method for reducing fluid flow between turbine components
A turbine component and fluid technology, applied in the field of turbines, can solve problems such as reducing efficiency and reducing turbine power output
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[0012] FIG. 1 is a schematic diagram of an embodiment of a gas turbine system 100 . System 100 includes compressor 102 , combustor 104 , turbine 106 , shaft 108 , and fuel nozzles 110 . In one embodiment, system 100 may include a plurality of compressors 102 , combustors 104 , turbines 106 , shafts 108 , and fuel nozzles 110 . Compressor 102 and turbine 106 are coupled by shaft 108 . The shaft 108 may be a single shaft, or multiple shaft segments coupled together to form the shaft 108 .
[0013] In one aspect, combustor 104 operates the engine using liquid fuel and / or gaseous fuel, such as natural gas or hydrogen-rich syngas. For example, fuel nozzles 110 are in fluid communication with an air supply and a fuel supply 112 . Fuel nozzles 110 generate an air-fuel mixture and discharge the air-fuel mixture into combustor 104 , causing combustion of the heated pressurized gas. Combustor 104 directs hot pressurized exhaust gas through a transition piece into a turbine nozzle (o...
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