Tuning thermal mismatch between turbine rotor parts with a thermal medium
Patent
·
OSTI ID:873560
- Niskayuna, NY
In a turbine rotor, an aft shaft wheel and the final-stage wheel of the rotor are coupled together, including by a rabbeted joint. During shutdown and startup of the turbine, a thermal mismatch between the aft shaft wheel and final-stage wheel is avoided by respectively heating and cooling the aft shaft wheel to maintain the thermal mismatch within acceptable limits, thereby avoiding opening of the rabbeted joint and the potential for unbalancing the rotor and rotor vibration. The thermal medium may be supplied by piping in the aft bearing cavity into the cavity between the forward closure plate and the aft shaft wheel.
- Research Organization:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC21-95MC31176
- Assignee:
- General Electric Co. (Schenectady, NY)
- Patent Number(s):
- US 6190127
- OSTI ID:
- 873560
- Country of Publication:
- United States
- Language:
- English
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including
joint
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maintain
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piping
plate
potential
rabbeted
respectively
rotor
shaft
shutdown
startup
supplied
thermal
thermal medium
thermal mismatch
tuning
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acceptable
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bearing
cavity
closure
cooling
coupled
final-stage
forward
heating
including
joint
limits
maintain
medium
mismatch
piping
plate
potential
rabbeted
respectively
rotor
shaft
shutdown
startup
supplied
thermal
thermal medium
thermal mismatch
tuning
turbine
turbine rotor
unbalancing
vibration
wheel