Apparatus and process for converting an aero gas turbine engine into an industrial gas turbine engine for electric power production
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United States of America Patent
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Dec 11, 2018
Grant Date -
Jan 11, 2018
app pub date -
Sep 15, 2015
filing date -
Jan 10, 2015
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Abstract
An apparatus and a process for converting a twin spool aero gas turbine engine to an industrial gas turbine engine, where the fan of the aero engine is removed and replaced with an electric generator, a power turbine is added that drives a low pressure compressor that is removed from the aero engine, variable guide vanes are positioned between the high pressure turbine and the power turbine, and a low pressure compressed air line is connected between the outlet of the low pressure compressor and an inlet to the high pressure compressor, where a hot gas flow produced in the combustor first flows through the high pressure turbine, then through the low pressure turbine, and then through the power turbine.
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