Vent system for use in a gas turbine and method of operating thereof
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United States of America Patent
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Nov 21, 2017
Grant Date -
Apr 23, 2015
app pub date -
Dec 18, 2012
filing date -
Dec 21, 2011
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Abstract
A vent for use in a gaseous fuel supply circuit of a gas turbine is provided. The vent includes an inlet in flow communication with the gaseous fuel supply circuit, a first outlet in flow communication with the gaseous fuel supply circuit and configured to release gaseous fuel at atmospheric pressure, a first valve coupled between the inlet and the first outlet, wherein the first valve includes a second outlet configured to channel the gaseous fuel towards a combustion device. The system also includes a second valve coupled between the inlet and the second outlet, and a control device configured to selectively open and close the first and second valves based on a pressure of the gaseous fuel.
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