发明申请
- 专利标题： BLADE PLATFORM WITH CHAMFER
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申请号： US15397501申请日： 2017-01-03
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公开(公告)号： US20180187558A1公开(公告)日： 2018-07-05
- 发明人: Charles Thistle , Mohamed Hassan
- 申请人： United Technologies Corporation
- 主分类号： F01D5/22
- IPC分类号： F01D5/22 ; F01D5/02 ; F01D5/30 ; F04D29/32 ; F04D29/66 ; F04D29/08 ; F01D11/00
摘要：
A blade for a gas turbine engine is provided. The blade having: a root; a platform located between the root and the blade, wherein the platform defines a cavity; and a chamfer located on opposing peripheral edges of the platform.
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