VARIABLE FLOW DIVIDER MECHANISM FOR A MULTI-STAGE COMBUSTOR
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United States of America Patent
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app pub date -
Sep 26, 2013
filing date -
Oct 1, 2012
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Abstract
The present invention discloses a novel apparatus and way for altering the airflow to a gas turbine combustion system. The apparatus comprises a flow divider mechanism which splits the airflow surrounding a combustion liner into two distinct portions, one directed towards a pilot and one directed towards a main stage combustion. The flow divider mechanism is interchangeable so as to provide a way of altering airflow splits between stages of the combustion system.
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