COOLING SYSTEM FOR GAS TURBINE LOAD COUPLING
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United States of America Patent
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Issued Date -
Jun 6, 2013
app pub date -
Nov 28, 2012
filing date -
Dec 2, 2011
priority date (Note) -
Abandoned
status (Latency Note)
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Abstract
A gas turbine is provided. The gas turbine comprises a compressor, a power turbine, a load coupling connecting the gas turbine to a load, a gas turbine package comprising a turbomachinery compartment housing the gas turbine, a load-coupling guard at least partly surrounding the load coupling, a cooling air circulation system for circulating cooling air in the turbomachinery compartment, and a cooling air channeling configured to circulate a cooling air flow from the cooling air circulation system in the load-coupling guard sufficient to remove heat from the load coupling.
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