发明名称 TIP CLEARANCE CONTROL APPARATUS AND METHOD
摘要 In a gas turbine engine, conduit delivers pressurized cooling air to a selected group of hollow struts at a temperature sufficient to induce thermal contraction of the selected group of hollow struts, thereby opposing a downward shift in the rotor axis during high power engine operation, and maintaining a circumferentially uniform tip clearance. Air baffles disposed in the cooled struts ensure radially uniform thermal contraction and efficient heat transfer.
申请公布号 CA2062929(A1) 申请公布日期 1992.10.17
申请号 CA19922062929 申请日期 1992.03.12
申请人 GENERAL ELECTRIC COMPANY 发明人 GLOVER, JEFFREY
分类号 F02C7/18;F01D11/20;F01D11/24;F01D25/16;F02C7/28;F02C9/18;(IPC1-7):F01D7/00 主分类号 F02C7/18
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