发明申请
US20050097896A1 Dual mode power unit having a combustor bypass system 失效
具有燃烧器旁路系统的双模式动力单元

Dual mode power unit having a combustor bypass system
摘要:
A gas turbine engine integrates the functions of an auxiliary power unit (APU) with one or more functions of an ECS, and that is capable of operating in both an unfired mode and a fired mode. The gas turbine engine includes a combustor system that is configured to allow the gas turbine to quickly transition from the unfired mode to the fired mode, by bypassing a portion of the air flowing to the combustor system around the combustor.
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