Production process of gas turbine

Power plants – Combustion products used as motive fluid – Convertible or combined with feature other than combustion...

Reexamination Certificate

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C029S889210

Reexamination Certificate

active

06865893

ABSTRACT:
A production process of a gas turbine capable of being applied to various cycles. A principal part of a gas turbine is initially set based on roughly set conditions, and the number of stages of the compressor and of the turbine for a desired cycle are set for the principal part. The compressor and the turbine each having the set number of stages and included in the principal part are combined to construct the gas turbine. When the set number of stages of the compressor or the turbine differs for a different desired cycle, a disk-shaped member having an outer periphery, which forms an inner peripheral wall of the annular flow passage of the compressor or the turbine, is assembled into the principal part having a smaller number of stages so that the bearing-to-bearing distance is kept constant.

REFERENCES:
patent: 6438837 (2002-08-01), Berry et al.
patent: 11-229894 (1999-08-01), None
patent: WO9848159 (1998-10-01), None
Aviation Week and Space Technology, Jan. 13, 1997, pp. 104, 114.*
GE brochure for LM6000, date unknown.*
P&W brochure for FT8, date unknown.*
“Gas Turbine Cycle, Combined Cycle, Reheat Gas Turbine, Cogeneration, STIG System, Repowering, HAT Cycle, CO Recovery Turbine, WE-NET Project, CAES System”, Journal of Gas Turbine Society of Japan, vol. 25, No. 97, 1997.
“Upgrading of a Small Size Gas Turbine to Hat Cycle Operation Thermodynamic and Economic Analysis”, Umberto Desideri and Francesco di Maria, ASME Paper 99-GT-372, 1999.

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