Invention Grant
US09441544B2 Variable volume combustor with nested fuel manifold system 有权
具有嵌套燃料歧管系统的可变容积燃烧器

Variable volume combustor with nested fuel manifold system
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, a fuel manifold system in communication with the micro-mixer fuel nozzles to deliver a flow of fuel thereto, and a linear actuator to maneuver the micro-mixer fuel nozzles and the fuel manifold system.
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