发明名称 TAPERED THERMAL COATING FOR AIRFOIL
摘要 An airfoil comprises pressure and suction surfaces extending axially from a leading edge to a trailing edge and radially from a root section to a tip section, the root section and the tip section defining a span therebetween. A thermal coating extends from the root section of the airfoil toward the tip section of the airfoil. A relative coating thickness of the thermal coating decreases by at least thirty percent at full span in the tip section, as compared to minimum span in the root section.
申请公布号 WO2013172903(A3) 申请公布日期 2014.01.09
申请号 WO2013US27232 申请日期 2013.02.22
申请人 UNITED TECHNOLOGIES CORPORATION 发明人 LEVINE, JEFFREY R.;GREGG, SHAWN J.
分类号 F01D5/28;F01D5/14;F02C7/00;F02K3/00 主分类号 F01D5/28
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