发明名称 TURBINE EXHAUST STRUCTURE AND GAS TURBINE
摘要 This turbine exhaust structure and gas turbine are configured with a turbine cylinder (26) being provided that configures a combustion gas pathway (›) 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 KR20130135928(A) 申请公布日期 2013.12.11
申请号 KR20137025437 申请日期 2012.03.22
申请人 MITSUBISHI HEAVY INDUSTRIES, LTD. 发明人 KITAGAWA HITOSHI;SAKAMOTO YASURO;ITO EISAKU
分类号 F01D25/30;F02C7/00 主分类号 F01D25/30
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