发明申请
US20160376901A1 TURBINE SHROUD SEGMENT WITH FLANGE-FACING PERIMETER SEAL
审中-公开
涡轮SHROUD分段与法兰边缘PERIMETER密封
- 专利标题： TURBINE SHROUD SEGMENT WITH FLANGE-FACING PERIMETER SEAL
- 专利标题（中）： 涡轮SHROUD分段与法兰边缘PERIMETER密封
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申请号： US15004442申请日： 2016-01-22
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公开(公告)号： US20160376901A1公开(公告)日： 2016-12-29
- 发明人: Mark O'Leary , Daniel K. Vetters , Matthew R. Brandt , Ted J. Freeman
- 申请人： Rolls-Royce North American Technologies, Inc. , Rolls-Royce Corporation
- 主分类号： F01D11/00
- IPC分类号： F01D11/00 ; F01D9/02 ; F01D25/12 ; F01D11/08 ; F01D25/00
摘要：
A turbine shroud adapted for use in a gas turbine engine includes a plurality of metallic carrier segments and a plurality of blade track segments mounted to corresponding metallic carrier segments. Cooling air is directed onto the blade track segments to cool the blade track segments when exposed to high temperatures in a gas turbine engine.
公开/授权文献
- US10047624B2 Turbine shroud segment with flange-facing perimeter seal 公开/授权日：2018-08-14
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