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METHOD FOR COOLING A TURBO-ENGINE COMPONENT AND TURBO-ENGINE COMPONENT
专利权人:
ANSALDO ENERGIA IP UK LIMITED
发明人:
KRÜCKELS Joerg,BRANDL Herbert
申请号:
US201615223242
公开号:
US2017030198(A1)
申请日:
2016.07.29
申请国别(地区):
美国
年份:
2017
代理人:
摘要:
Disclosed is a turbo-engine component and a method for cooling a turbo-engine component. The method includes guiding a working fluid flow along a hot gas side surface of a wall of the component and in a main working fluid flow direction, discharging a coolant discharge flow at the hot gas side surface from a coolant discharge duct provided in the wall, and supplying a coolant supply flow to the coolant discharge duct and through a coolant supply path. The method also includes discharging the coolant supply flow into the coolant discharge duct as a free jet oriented across a cross section of the coolant discharge duct, and directing the free jet onto an inner surface section of the coolant discharge duct, thus effecting impingement cooling of the inner surface section.
来源网站:
中国工程科技知识中心
来源网址:
http://www.ckcest.cn/home/

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