Method and apparatus for injecting steam in a gas turbine
A gas turbine and steam technology, applied in the direction of gas turbine devices, mechanical equipment, machines/engines, etc., can solve the problems of reducing flame stability, lack of power increase of steam injection technology, etc.
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[0014] First refer to figure 1 , shows a gas turbine combustor, generally designated 10, comprising an outer cladding or shell 12, a flow sleeve 14, and a combustor liner 16 disposed substantially centrally within the flow sleeve 14 and defining a combustion chamber 18 . A transition piece or duct 20 is coupled to the aft or downstream end of combustor liner 16 and supplies hot combustion gases to a first turbine section or stage represented by first stator vanes or nozzles 22 . At the forward end of the combustor 10 , an end cover 24 supports a plurality of fuel nozzles 26 that project into the combustion chamber 18 . End cover 24 includes the head or forward end of the combustor and supplies purge air and fuel to fuel nozzles 26 while supplying compressor exhaust air into the forward end of liner 16 to communicate with the Fuel mix supplied. As is well known, in certain gas turbine engines a plurality of combustors 10 are arranged in an annular array about the turbine rot...
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