EXHAUST SYSTEM FOR GAS TURBINES
    1.
    发明申请
    EXHAUST SYSTEM FOR GAS TURBINES 审中-公开
    排气系统用于气体涡轮机

    公开(公告)号:US20130327052A1

    公开(公告)日:2013-12-12

    申请号:US13916396

    申请日:2013-06-12

    IPC分类号: F02C6/18 F02C7/141

    摘要: An exhaust system is provided for mitigating condensate formation in a common exhaust stack and for effecting improved heat transfer. Reduced condensate formation and improved heat transfer is achieved by inducing non-laminar flow through the common exhaust stack and a heat exchanger operatively coupled to the common exhaust stack. Heat transfer is further improved by dew point control. Non-laminar flow is induced by connecting more than one gas turbine to the common exhaust stack through non-laminar flow inducing arrangements. The various coupling arrangements also add structural rigidity to the common exhaust stack for increased stack height and improved plume dispersion.

    摘要翻译: 提供了一种排气系统,用于减轻公共排气叠层中的冷凝物形成并实现改进的热传递。 通过引导非层流流经公共排气叠层和可操作地连接到公共排气叠层的热交换器来实现冷凝物形成减少和热传递的改善。 通过露点控制进一步提高了热传递。 通过非层流引导装置将多于一个燃气轮机连接到公共排气叠层引起非层流。 各种联接布置还增加了公共排气叠层的结构刚度,以增加堆叠高度和改进的羽流分散。