发明名称 Blade tip clearance control of a gas turbine
摘要 The gas turbine has a number of guide vanes (12) arranged in rows on a turbine shaft (8) and a number of guide vanes (14) arranged in rows and joined to a turbine housing. The rows or each row in the inner region of the turbine housing are or is enclosed by a guide ring (21) subjected to a control medium for influencing its thermal expansion.
申请公布号 EP1329594(A1) 申请公布日期 2003.07.23
申请号 EP20020001264 申请日期 2002.01.17
申请人 SIEMENS AKTIENGESELLSCHAFT 发明人 TIEMANN, PETER
分类号 F01D11/02;F01D11/14;F01D11/20;F01D11/24;(IPC1-7):F01D11/02 主分类号 F01D11/02
代理机构 代理人
主权项
地址