基本信息:
- 专利标题： GAS TURBINE ENGINE COMPONENT WITH DISCHARGE SLOT HAVING OVAL GEOMETRY
- 专利标题（中）：燃气轮机发动机部件与带有卵形几何的排气槽
- 申请号：PCT/US2013/046733 申请日：2013-06-20
- 公开(公告)号：WO2014042735A2 公开(公告)日：2014-03-20
- 发明人： BOEKE, Mark A. , OTERO, Edwin , DEGRAY, Jeffrey J. , PROPHETER-HINCKLEY, Tracy A. , FERNANDEZ, Guillermo J. , RILEY, Sarah
- 申请人： UNITED TECHNOLOGIES CORPORATION
- 申请人地址： One Financial Plaza Hartford, Connecticut 06101 US
- 专利权人： UNITED TECHNOLOGIES CORPORATION
- 当前专利权人： UNITED TECHNOLOGIES CORPORATION
- 当前专利权人地址： One Financial Plaza Hartford, Connecticut 06101 US
- 代理机构： BARRETT, Todd W.
- 优先权： US61/665,499 20120628; US13/598,988 20120830
摘要：
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.
摘要（中）：
根据本公开的示例性方面的用于燃气涡轮发动机的部件尤其包括在前缘和后缘之间延伸的主体部分。 前缘和后缘中的至少一个包括至少一个排出槽，该排出槽具有包括椭圆形几何形状的第一部分。