General Electric DS6800CCID1D1D !!! ---mail to: sales3@amikon.cn
Email: sales3@amikon.cn
Contact: Jessica | Skype: jessica01235483
Wechat: hu18030235311 | Mobile: 86-18030235311(WhatsApp)
Seals in the turbine
shell prevent leakage of combustion gases around the nozzle from the inlet to the
exhaust. Compressor discharge air is fed to these sealing rings through orifices in
the shell. A key feature of the first-stage nozzle is the air-cooled partition which
increases nozzle life substantially. Cooling air from the compressor discharge is
directed through the body of the individual nozzle partitions, exiting through
holes near the trailing edge.
This not only cools the metal, but blankets the
trailing edge with a film of air. Additionally, relatively thick nozzle partition
trailing edges provide increased strength and oxidation resistance, again
providing longer nozzle life.
General Electric DS6800CCID1D1D
GE DS6800CCID1D1D | General Electric | BOARD MODULE
sales3@amikon.cn
The long shank bucket design lowers the turbine wheel rim a substantial distance below the hot
gas path. The high thermal resistance of the shank results in a considerable temperature drop
between the hot bucket vane and the wheel dovetail slot
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Emal:sales3@amikon.cn
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