COOLING SYSTEMS FOR GAS TURBINE ENGINES

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专利权人:

UNITED TECHNOLOGIES CORPORATION

发明人:

Weiner Richard Alan

申请号：

US201415111997

公开号：

US2016333783(A1)

申请日:

2014.12.22

申请国别(地区):

美国

年份:

2016

代理人:

摘要：

An air-oil cooler for a gas turbine engine includes an air cooling structure and a lubricant channel. The lubricant channel extends between a lubricant inlet and a lubricant inlet and is bounded by the air cooling structure. The air cooling structure has an arcuate shape for circumferentially spanning a portion of a gas turbine engine core.

来源网站：

中国工程科技知识中心

来源网址：

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