Gas turbine engine component with compound cusp cooling configuration

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专利权人:

United Technologies Corporation

发明人:

Xu JinQuan

申请号：

US201615243220

公开号：

US9869186(B2)

申请日:

2016.08.22

申请国别(地区):

美国

年份:

2018

代理人:

Kinney & Lange, P.A.

摘要：

A component for a gas turbine engine including a gas path wall having a first surface and a second surface. A cooling hole extends through the gas path wall from an inlet in the first surface through a transition to an outlet in the second surface. Cusps are formed on the transition.

来源网站：

中国工程科技知识中心

来源网址：

http://www.ckcest.cn/home/