发明名称 BLADE CLEARANCE CONTROL
摘要 A turbine engine has a circumferentially segmented shroud within a case structure. Each shroud segment is mounted for movement between an inboard position and an outboard position. One or more springs bias the shroud segments toward their inboard positions. One or more valves are positioned to vent one or more volumes so as to counter the spring bias to shift the shroud segments to their outboard positions.
申请公布号 CA2511635(A1) 申请公布日期 2006.01.09
申请号 CA20052511635 申请日期 2005.07.06
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 PENDA, ALLAN R.;BURGE, JOSEPH C.
分类号 F01D11/22;F01D11/16 主分类号 F01D11/22
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