Invention Grant
US09587562B2 Variable volume combustor with aerodynamic support struts 有权
具有气动支撑支柱的可变容积燃烧器

Variable volume combustor with aerodynamic support struts
Abstract:
The present application provides a combustor for use with a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles and a fuel injection system for providing a flow of fuel to the micro-mixer fuel nozzles. The fuel injection system may include a number of support struts supporting the fuel nozzles and providing the flow of fuel therethrough. The support struts may include an aerodynamic contoured shape so as to distribute evenly a flow of air to the micro-mixer fuel nozzles.
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