GAS TURBINE ENGINE COMPONENT WITH DISCHARGE SLOT HAVING OVAL GEOMETRY
摘要
<p>A component for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, an body portion that extends between a leading edge and a trailing edge. At least one of the leading edge and the trailing edge includes at least one discharge slot having a first portion that includes an oval geometry.</p>
申请公布号
EP2867479(A4)
申请公布日期
2015.05.06
申请号
EP20130836277
申请日期
2013.06.20
申请人
UNITED TECHNOLOGIES CORPORATION
发明人
BOEKE, MARK A.;OTERO, EDWIN;DEGRAY, JEFFREY J.;PROPHETER-HINCKLEY, TRACY A.;FERNANDEZ, GUILLERMO J.;RILEY, SARAH
