Invention Grant
- Patent Title: Gas turbine engine component
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Application No.: US17866855Application Date: 2022-07-18
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Publication No.: US11661865B2Publication Date: 2023-05-30
- Inventor: Thomas E. Clark , Ken F. Blaney
- Applicant: Raytheon Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: Raytheon Technologies Corporation
- Current Assignee: Raytheon Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Carlson, Gaskey & Olds, P.C.
- The original application number of the division: US16019972 2018.06.27
- Main IPC: F01D11/08
- IPC: F01D11/08 ; F01D25/28

Abstract:
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.
Public/Granted literature
- US20220364483A1 GAS TURBINE ENGINE COMPONENT Public/Granted day:2022-11-17
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