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New Humidification Concept for Evaporative Gas Turbine Cycles Applied to a Modern Aeroderivative Gas Turbine

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Abstract A new humidification concept in evaporative gas turbine cycles is presented. This involves a humidfication column with multiple sections of counter-current humidification with different water flows in each section. The advantages of multiple sections are analyzed in combination with part-flow humidification, where less than 50% of the compressed air from the air compressor is led through the humidification column and the rest is passed on directly to the recuperator. The part flow humidification is a concept that noticeably reduces mass and heat transfer equipment costs in the EvGT cycle. It is shown that, for a part flow configuration, a more efficient cycle can be attained than in a system with customary single-section humidification. In this paper an EvGT system is modeled in the GATE/CYCLE gas turbine simulation program. The simulations are based on the modem aeroderivative gas turbine Rolls Royce Trent in non-intercooled mode. The results include performance data as well as dimensions and design considerations of the humidification column and the heat exchangers.
Title: New Humidification Concept for Evaporative Gas Turbine Cycles Applied to a Modern Aeroderivative Gas Turbine
Description:
Abstract A new humidification concept in evaporative gas turbine cycles is presented.
This involves a humidfication column with multiple sections of counter-current humidification with different water flows in each section.
The advantages of multiple sections are analyzed in combination with part-flow humidification, where less than 50% of the compressed air from the air compressor is led through the humidification column and the rest is passed on directly to the recuperator.
The part flow humidification is a concept that noticeably reduces mass and heat transfer equipment costs in the EvGT cycle.
It is shown that, for a part flow configuration, a more efficient cycle can be attained than in a system with customary single-section humidification.
In this paper an EvGT system is modeled in the GATE/CYCLE gas turbine simulation program.
The simulations are based on the modem aeroderivative gas turbine Rolls Royce Trent in non-intercooled mode.
The results include performance data as well as dimensions and design considerations of the humidification column and the heat exchangers.

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