Invention Grant
- Patent Title: Turbine component assembly
-
Application No.: US15624070Application Date: 2017-06-15
-
Publication No.: US10808575B2Publication Date: 2020-10-20
- 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 ; F01D9/04 ; F23R3/00 ; F23R3/60 ; F01D25/00

Abstract:
A turbine component assembly is disclosed, including a first component, a second component, and a circumferentially oriented flat 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 circumferentially oriented flat spring is disposed on and directly contacting the second component and directly contacting and supporting the first component as a compliant contact interface between the first component and the second component. The circumferentially oriented flat spring provides a radial spring compliance between the first component and the second component.
Public/Granted literature
- US20180363509A1 TURBINE COMPONENT ASSEMBLY Public/Granted day:2018-12-20
Information query