发明名称 Tip clearance control apparatus and method.
摘要 In a gas turbine engine, conduit [90] delivers pressurized cooling air to a selected group of hollow [87,70,71] 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. <IMAGE>
申请公布号 EP0509802(A1) 申请公布日期 1992.10.21
申请号 EP19920303410 申请日期 1992.04.15
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 主分类号 F02C7/18
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