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Title: Flexible metallic seal for transition duct in turbine system

Patent ·
OSTI ID:1129400
; ; ; ;

A turbine system is disclosed. In one embodiment, the turbine system includes a transition duct. The transition duct includes an inlet, an outlet, and a passage extending between the inlet and the outlet and defining a longitudinal axis, a radial axis, and a tangential axis. The outlet of the transition duct is offset from the inlet along the longitudinal axis and the tangential axis. The transition duct further includes an interface member for interfacing with a turbine section. The turbine system further includes a flexible metallic seal contacting the interface member to provide a seal between the interface member and the turbine section.

Research Organization:
General Electric Co., Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
8,701,415
Application Number:
13/292,389
OSTI ID:
1129400
Resource Relation:
Patent File Date: 2011 Nov 09
Country of Publication:
United States
Language:
English

References (39)

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Cited By (1)

Adjustable transition support and method of using the same patent July 2017

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