Invention Grant
- Patent Title: Combustor liner attachment assembly for gas turbine engine
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Application No.: US16160321Application Date: 2018-10-15
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Publication No.: US11255547B2Publication Date: 2022-02-22
- Inventor: Kevin W. White , Stephen K. Kramer
- Applicant: United Technologies Corporation
- Applicant Address: US CT Farmington
- Assignee: United Technologies Corporation
- Current Assignee: United Technologies Corporation
- Current Assignee Address: US CT Farmington
- Agency: Cantor Colburn LLP
- Main IPC: F23R3/60
- IPC: F23R3/60 ; F02C3/14 ; F16B5/02 ; F23R3/00 ; F02C7/20

Abstract:
A combustor liner panel attachment assembly includes a liner extending from a first end to a second end, and circumferentially to partially define a combustion zone. The assembly also includes a spring element located adjacent to a portion of the liner and operatively coupled to a stationary structure, the spring element having a recessed segment. The assembly further includes a protrusion feature extending radially outwardly from the liner, the protrusion feature disposed within the recessed segment of the spring element to axially retain the liner.
Public/Granted literature
- US11199329B2 Combustor liner attachment assembly for gas turbine engine Public/Granted day:2021-12-14
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