APPARATUS AND METHOD FOR PURGING A GAS TURBOMACHINE NOZZLE
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United States of America Patent
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Jun 23, 2016
app pub date -
Dec 17, 2014
filing date -
Dec 17, 2014
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Abstract
A gas turbomachine includes a compressor portion, a turbine portion operatively connected to the compressor portion, and a combustor assembly fluidically connected to the turbine portion. The combustor assembly includes at least one nozzle including at least one fuel gas injector portion and at least one water injector portion. A fuel system is fluidically connected to the at least one nozzle. The fuel system includes at least one fuel gas manifold, a water injector purge manifold and a water injector manifold. The at least one fuel gas manifold is selectively fluidically connectable to the water injector portion of the nozzle through the water injector purge manifold.
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