GAS TURBINE ENGINE WALL ASSEMBLY WITH ENHANCED FLOW ARCHITECTURE

• 收藏
• 分享

专利权人:

United Technologies Corporation

发明人:

Cunha Frank J.,Kostka Stanislav

申请号：

US201415039108

公开号：

US2017159936(A1)

申请日:

2014.12.31

申请国别(地区):

美国

年份:

2017

代理人:

摘要：

A liner panel is provided for use in a gas turbine engine. The liner panel includes an intermediate rail that extends from a cold side of a liner panel. The liner panel also includes a multiple of heat transfer augmentors, which generally decrease in height with respect to a distance from the intermediate rail.

来源网站：

中国工程科技知识中心

来源网址：

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