SYSTEM FOR SUPPLYING PRESSURIZED FLUID TO A CAP ASSEMBLY OF A GAS TURBINE COMBUSTOR
A system for supplying pressurized fluid to a combustor of a gas turbine is disclosed. The system may include an end cover and a fuel nozzle extending from the end cover. The fuel nozzle may include a downstream end. Additionally, the system may include a cap assembly configured to receive at least...
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Main Authors | , |
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Format | Patent |
Language | English |
Published |
28.03.2013
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Subjects | |
Online Access | Get full text |
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Summary: | A system for supplying pressurized fluid to a combustor of a gas turbine is disclosed. The system may include an end cover and a fuel nozzle extending from the end cover. The fuel nozzle may include a downstream end. Additionally, the system may include a cap assembly configured to receive at least a portion of the fuel nozzle. The cap assembly may include an upstream wall spaced apart from the downstream end, a downstream wall disposed proximate to the downstream end and a cap chamber defined between the upstream and downstream walls. Moreover, a conduit may extend through the end cover and the upstream wall such that a discharge end of the conduit is in flow communication with the cap chamber. |
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Bibliography: | Application Number: US201113247252 |