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 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|