METHOD OF USING SEGMENTED GAS BURNER WITH GAS TURBINES
    1.
    发明申请
    METHOD OF USING SEGMENTED GAS BURNER WITH GAS TURBINES 有权
    使用带有气体燃烧器的气体燃烧器的方法

    公开(公告)号:US20020148226A1

    公开(公告)日:2002-10-17

    申请号:US10165295

    申请日:2002-06-11

    Abstract: A segmented radiant gas burner features wide modulation of thermal output simply by the independent control of fuel gas flow to each burner segment. The burner also features a porous fiber burner face, preferably having dual porosities, and a metal liner positioned to provide a compact combustion zone adjacent the burner face. The segmented radiant burner is ideally suited for use with gas turbines not only because of its compactness and broad thermal modulation but also because only the flow of fuel gas to each burner segment requires control while the flow of compressed air into all segments of the burner remains unchanged.

    Abstract translation: 分段辐射气体燃烧器仅通过独立控制燃料气体流向每个燃烧器段,就可以很好地调节热量输出。 燃烧器还具有多孔纤维燃烧器面,优选具有双重孔隙度,以及定位成提供邻近燃烧器表面的紧凑燃烧区的金属衬套。 分段辐射燃烧器非常适合用于燃气轮机,不仅因为它的紧凑性和广泛的热调制,而且因为只有燃料气体流向每个燃烧器段才需要控制,同时压缩空气流入燃烧器的所有部分仍然保持 不变

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