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Title: Flexible metallic seal for transition duct in turbine system

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.
Inventors:
; ; ; ;
Issue Date:
OSTI Identifier:
1129400
Assignee:
General Electric Company (Schenectady, NY) NETL
Patent Number(s):
8,701,415
Application Number:
13/292,389
Contract Number:
FC26-05NT42643
Resource Relation:
Patent File Date: 2011 Nov 09
Research Org:
General Electric Company, Schenectady, NY (United States)
Sponsoring Org:
USDOE
Country of Publication:
United States
Language:
English
Subject:
42 ENGINEERING

Works referenced in this record: