Combustion liner having turbulators
A turbulator, turbulent flow technology, applied in the combustion chamber, combustion method, combustion equipment and other directions, can solve the problem of shortening the life of the liner
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[0058] see figure 1 with figure 2 , a typical gas turbine includes a transition piece 10 through which hot combustion gases pass from an upstream combustor (as represented by a combustion liner 12 ) to a first stage of the turbine, indicated at 14 . Flow from the gas turbine compressor exits the axial diffuser 16 and enters into the compressor discharge casing 18 . Approximately 50% of the compressor discharge air passes through the orifices 20 formed along and around the transition piece impingement sleeve 22 to flow between the transition piece 10 and the radially outer transition piece impingement sleeve 22 within the annular region or annulus 24 (or second flow annulus). The remaining approximately 50% of the compressor discharge flow passes into the flow sleeve bore 34 of the upstream combustion liner cooling sleeve (not shown) and into the annulus between the cooling sleeve and the liner and ultimately in the annulus 24 mixed with air. This combined air is ultimatel...
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