发明申请
- 专利标题： SPLAYED TIP FEATURES FOR GAS TURBINE ENGINE AIRFOIL
- 专利标题（中）： 气体涡轮发动机气翼的特点
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申请号： US14630814申请日： 2015-02-25
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公开(公告)号： US20160069189A1公开(公告)日： 2016-03-10
- 发明人: San Quach , Tracy A Propheter-Hinckley , Dominic J Mongillo, JR. , Steven Bruce Gautschi
- 申请人： UNITED TECHNOLOGIES CORPORATION
- 主分类号： F01D5/14
- IPC分类号： F01D5/14 ; F01D5/28
摘要：
A component for a gas turbine engine includes a trailing edge tip corner that at least partially defines a trailing edge cavity and a multiple of corner features within the trailing edge cavity, the multiple of corner features splayed along the trailing edge tip corner.
公开/授权文献
- US10329916B2 Splayed tip features for gas turbine engine airfoil 公开/授权日：2019-06-25
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