Multiloop gas turbine system and method of operation thereof
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United States of America Patent
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Mar 16, 2021
Grant Date -
Apr 19, 2018
app pub date -
Apr 16, 2016
filing date -
Apr 17, 2015
priority date (Note) -
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Abstract
The present disclosure relates to a novel gas turbine system having applications, for example, in thermal power generation in an environmentally friendly manner. The multiloop gas turbine system may have multiple functional units each comprising a compressor, a regenerator, a combustion unit, and a turbine. Typically, exhaust flow of a turbine of a preceding loop may be routed to the combustion unit of the next loop, allowing mixing of exhaust flow with hot compressed air of the next loop, and the expanded exhaust from the turbine of the ultimate loop is fed back into the regenerators of each loop to recover exhaust heat.
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