Invention Application
- Patent Title: TURBINE SHROUD ASSEMBLY
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Application No.: US15623990Application Date: 2017-06-15
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Publication No.: US20180363498A1Publication Date: 2018-12-20
- Inventor: Glenn Curtis TAXACHER , John McConnell DELVAUX , Matthew Troy HAFNER
- Applicant: GENERAL ELECTRIC COMPANY
- Main IPC: F01D25/04
- IPC: F01D25/04 ; F01D9/04

Abstract:
A turbine shroud assembly is disclosed including an inner shroud, an outer shroud, a shroud dampening pin, and a biasing apparatus. The inner shroud is adjacent to a hot gas path. The outer shroud is adjacent to the inner shroud and distal from the hot gas path, and includes a channel extending from an aperture adjacent to the inner shroud. The shroud dampening pin is within the channel and contacts the inner shroud, and includes a shaft, a contact surface, and a cap. The shaft is within the channel. The contact surface extends through the aperture in contact with the inner shroud. The cap is distal across the shaft from the contact surface. The biasing apparatus contacts the cap, is driven by a pressurized fluid, and provides a biasing force away from the outer shroud along the shroud dampening pin to the inner shroud through the contact surface.
Public/Granted literature
- US10544701B2 Turbine shroud assembly Public/Granted day:2020-01-28
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