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