Invention Grant
- Patent Title: Turbine component assembly
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Application No.: US15624142Application Date: 2017-06-15
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Publication No.: US10697326B2Publication Date: 2020-06-30
- Inventor: Glenn Curtis Taxacher , John McConnell Delvaux , Matthew Troy Hafner
- Applicant: GENERAL ELECTRIC COMPANY
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: McNees Wallace & Nurick LLC
- Main IPC: F01D25/28
- IPC: F01D25/28 ; F23R3/00 ; F23R3/60 ; F01D9/04 ; F01D11/08

Abstract:
A turbine component assembly is disclosed, including a first component, a second component, and a cantilever spring. The first component is arranged to be disposed adjacent to a hot gas path, and includes a ceramic matrix composite composition. The second component is adjacent to the first component and arranged to be disposed distal from the hot gas path across the first component. The cantilever spring is attached directly to the second component as a compliant contact interface between the first component and the second component. The cantilever spring provides a radial spring compliance between the first component and the second component. During operation, the cantilever spring directly contacts and supports the first component.
Public/Granted literature
- US20180363510A1 TURBINE COMPONENT ASSEMBLY Public/Granted day:2018-12-20
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