Invention Grant
US09562687B2 Variable volume combustor with an air bypass system 有权
具有空气旁路系统的可变容积燃烧器

Variable volume combustor with an air bypass system
Abstract:
The present application provides a combustor for use with flow of fuel and a flow of air in a gas turbine engine. The combustor may include a number of micro-mixer fuel nozzles positioned within a liner and an air bypass system position about the liner. The air bypass system variably allows a bypass portion of the flow of air to bypass the micro-mixer fuel nozzles.
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