EXHAUST CHANNEL OF MICROTURBINE ENGINE
    3.
    发明申请

    公开(公告)号:US20190145284A1

    公开(公告)日:2019-05-16

    申请号:US15810374

    申请日:2017-11-13

    Abstract: An exhaust channel of a microturbine engine, characterized by a tapering pipe for reducing the speed at which a high-temperature gas is discharged from the turbine and ensuring that the high-temperature gas induced into a recuperator produces a uniform, low-speed flow field, with a view to preventing any noticeable vortex region from developing in the channel, minimizing the pressure loss in the channel, and enhancing the heat exchange efficiency of the recuperator.

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