Gas turbine and manufacturing process of gas turbine

Power plants – Combustion products used as motive fluid – Process

Reexamination Certificate

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Details

C060S039530, C060S801000, C029S889200

Reexamination Certificate

active

07441410

ABSTRACT:
The invention is intended to maintain turbine reliability when, based on a gas turbine designed for one desired cycle, a gas turbine for another different cycle is manufactured. A channel of a compressor is formed such that a mass flow of a fluid compressed by the compressor changes. Thus, when manufacturing, based on the gas turbine designed for one desired cycle, the gas turbine for another different cycle, turbine reliability can be maintained.

REFERENCES:
patent: 4829763 (1989-05-01), Rao
patent: 6119445 (2000-09-01), Bronicki et al.
patent: 6305158 (2001-10-01), Nakhamkin et al.
patent: 6389799 (2002-05-01), Hatamiya et al.
patent: 6644013 (2003-11-01), Hatamiya et al.
patent: 6865893 (2005-03-01), Koganezawa et al.
patent: 2001-271792 (2001-10-01), None
Desideri et al., “Upgrading of a Small Size Gas Turbine to HAT Cycle Operation: Thermodynamic and Economic Analysis.” Jun. 7-10, 1999, ASME Paper 99-GT-372, pp. 1-10.
IGTC2003, Tokyo, TS-900.

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