This turbine exhaust structure and gas turbine are configured with a turbine cylinder (26) being provided that configures a combustion gas pathway (A) by forming a tubular shape, and an exhaust diffuser (31) that configures an exhaust gas pathway (B) by forming a tubular shape being connected to the turbine cylinder (26). By providing a pressure loss body (61) to the exhaust diffuser (31), it is possible to increase performance by increasing turbine efficiency by performing efficient exhaust gas pressure recovery.
申请公布号
WO2012133123(A1)
申请公布日期
2012.10.04
申请号
WO2012JP57388
申请日期
2012.03.22
申请人
MITSUBISHI HEAVY INDUSTRIES, LTD.;KITAGAWA, HITOSHI;SAKAMOTO, YASURO;ITO, EISAKU