Humidification of the flow through a gas turbine has been proposed in a variety of forms. The STIG plant involves the generation of steam by the gas turbine exhaust in a heat recovery steam generator (HRSG), and its injection into or downstream of the combustion chamber. This increases the mass flow through the turbine and the power output from the plant, with a small increase in efficiency. In the evaporative gas turbine (or EGT) cycle, water is injected in the compressor discharge in a regenerative gas turbine cycle (a so-called CBTX plant—compressor [C], burner [B], turbine [T], heat exchanger [X]); the air is evaporatively cooled before it enters the heat exchanger. While the addition of water increases the turbine mass flow and power output, there is also apparent benefit in reducing the temperature drop in the exhaust stack. In one variation of the basic EGT cycle, water is also added downstream of the evaporative aftercooler, even continuously in the heat exchanger. There are several other variations on the basic cycle (e.g., the cascaded humidified advanced turbine [CHAT]). The present paper analyzes the performance of the EGT cycle. The basic thermodynamics are first discussed, and related to the cycle analysis of a dry regenerative gas turbine plant. Subsequently some detailed calculations of EGT cycles are presented. The main purpose of the work is to seek the optimum pressure ration in the EGT cycle for given constraints (e.g., fixed maximum to minimum temperature). It is argued that this optimum has a relatively low value.
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April 1998
Research Papers
The Evaporative Gas Turbine [EGT] Cycle
J. H. Horlock
J. H. Horlock
Whittle Laboratory, Madingley Road, Cambridge CB3 ODY, United Kingdom
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J. H. Horlock
Whittle Laboratory, Madingley Road, Cambridge CB3 ODY, United Kingdom
J. Eng. Gas Turbines Power. Apr 1998, 120(2): 336-343 (8 pages)
Published Online: April 1, 1998
Article history
Received:
February 1, 1997
Online:
November 19, 2007
Citation
Horlock, J. H. (April 1, 1998). "The Evaporative Gas Turbine [EGT] Cycle." ASME. J. Eng. Gas Turbines Power. April 1998; 120(2): 336–343. https://doi.org/10.1115/1.2818127
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