Methods for disassembling, replacing and assembling parts of a steam cooling system for a gas turbine
Patent
·
OSTI ID:874864
- Mauldin, SC
- Albany, NY
The steam cooling circuit for a gas turbine includes a bore tube assembly supplying steam to circumferentially spaced radial tubes coupled to supply elbows for transitioning the radial steam flow in an axial direction along steam supply tubes adjacent the rim of the rotor. The supply tubes supply steam to circumferentially spaced manifold segments located on the aft side of the 1-2 spacer for supplying steam to the buckets of the first and second stages. Spent return steam from these buckets flows to a plurality of circumferentially spaced return manifold segments disposed on the forward face of the 1-2 spacer. Crossover tubes couple the steam supply from the steam supply manifold segments through the 1-2 spacer to the buckets of the first stage. Crossover tubes through the 1-2 spacer also return steam from the buckets of the second stage to the return manifold segments. Axially extending return tubes convey spent cooling steam from the return manifold segments to radial tubes via return elbows. The bore tube assembly, radial tubes, elbows, manifold segments and crossover tubes are removable from the turbine rotor and replaceable.
- Research Organization:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC21-95MC31176
- Assignee:
- General Electric Company (Schenectady, NY)
- Patent Number(s):
- US 6477773
- OSTI ID:
- 874864
- Country of Publication:
- United States
- Language:
- English
Advances in Steam Path Technology
|
journal | April 1996 |
Development Requirements for an Advanced Gas Turbine System
|
journal | October 1995 |
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1-2
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circumferentially
convey
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coupled
crossover
direction
disassembling
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axial
axially
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coupled
crossover
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disposed
elbows
extending
flow
flows
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manifold
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replacing
return
rim
rotor
segments
spaced
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spent
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turbine
via