发明名称 |
MULTIPLE INJECTOR HOLES FOR GAS TURBINE ENGINE VANE |
摘要 |
A vane comprises an airfoil extending from a radially outer platform to a radially inner platform. A pair of legs extend radially inwardly from the radially inner platform, and an air flow passage extends through the radially outer platform, through the airfoil, and into a chamber defined between the pair of legs. One of the pair of legs includes a plurality of injector holes, configured to allow air from the radially outer platform to pass outwardly of the holes. A gas turbine engine is also disclosed. |
申请公布号 |
WO2015112227(A3) |
申请公布日期 |
2015.10.22 |
申请号 |
WO2014US64213 |
申请日期 |
2014.11.06 |
申请人 |
UNITED TECHNOLOGIES CORPORATION |
发明人 |
BERMAN, RUSSELL J.;WU, CHARLES C.;BARTLING, BRETT ALAN |
分类号 |
F02C7/18;F01D5/18;F01D9/02;F01D25/12 |
主分类号 |
F02C7/18 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|