Dual mode power unit having a combustor bypass system
    1.
    发明申请
    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

    公开(公告)号:US20050097896A1

    公开(公告)日:2005-05-12

    申请号:US10705580

    申请日:2003-11-10

    IPC分类号: F02C6/00 F02C7/268

    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.

    摘要翻译: 燃气涡轮发动机将辅助动力单元(APU)的功能与ECS的一个或多个功能集成,并且能够在未燃烧模式和燃烧模式下操作。 燃气涡轮发动机包括燃烧器系统,其被构造成允许燃气涡轮机通过绕流动到燃烧器系统周围的燃烧器的一部分空气而从未燃烧模式快速转变到燃烧模式。