- 专利标题: Gas turbine engine component
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申请号: US17866855申请日: 2022-07-18
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公开(公告)号: US11661865B2公开(公告)日: 2023-05-30
- 发明人: Thomas E. Clark , Ken F. Blaney
- 申请人: Raytheon Technologies Corporation
- 申请人地址: US CT Farmington
- 专利权人: Raytheon Technologies Corporation
- 当前专利权人: Raytheon Technologies Corporation
- 当前专利权人地址: US CT Farmington
- 代理机构: Carlson, Gaskey & Olds, P.C.
- 分案原申请号: US16019972 2018.06.27
- 主分类号: F01D11/08
- IPC分类号: F01D11/08 ; F01D25/28
摘要:
A method of assembling a blade outer air seal assembly includes engaging a first blade outer air seal with a first attachment surface on a first attachment body. The first blade outer air seal includes a first attachment body passage for accepting the first attachment body. A second blade outer air seal is engaged with a second attachment surface on the first attachment body. The second blade outer air seal includes a second attachment body passage for accepting the first attachment body. Rotation is prevented of the first attachment body relative to the first blade outer air seal with a first post engaging the first blade outer air seal. Rotation is prevented of the first attachment body relative to the second blade outer air seal with a second post engaging the second blade outer air seal.
公开/授权文献
- US20220364483A1 GAS TURBINE ENGINE COMPONENT 公开/授权日:2022-11-17
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