Combustor burner arrangement
    1.
    发明授权

    公开(公告)号:US10533748B2

    公开(公告)日:2020-01-14

    申请号:US15305450

    申请日:2015-04-30

    摘要: A fuel lance for a burner of a combustor has a fuel lance body defining a fuel flow passage and a liquid fuel tip attached thereto and in flow communication with fuel flow passage. The liquid fuel tip has a fuel outlet and an array of air passages having outlets which are arranged outside a blank sector of a circumference around the fuel outlet, the blank sector defined by an angle from 30° to 160°. A burner includes the fuel lance and the igniter and a main air flow passage to direct at least a part of a main air flow over the fuel lance and over the igniter, the blank sector has a centre-line angled between +120° and −120° from a radial line from the axis and passing through the fuel lance. A method includes rotating the fuel lance between a start-up condition and a second condition.

    COMBUSTOR BURNER ARRANGEMENT
    2.
    发明申请
    COMBUSTOR BURNER ARRANGEMENT 审中-公开
    COMBUSTOR燃烧器装置

    公开(公告)号:US20170045231A1

    公开(公告)日:2017-02-16

    申请号:US15305450

    申请日:2015-04-30

    摘要: A fuel lance for a burner of a combustor has a fuel lance body defining a fuel flow passage and a liquid fuel tip attached thereto and in flow communication with fuel flow passage. The liquid fuel tip has a fuel outlet and an array of air passages having outlets which are arranged outside a blank sector of a circumference around the fuel outlet, the blank sector defined by an angle from 30° to 160°. A burner includes the fuel lance and the igniter and a main air flow passage to direct at least a part of a main air flow over the fuel lance and over the igniter, the blank sector has a centre-line angled between +120° and −120° from a radial line from the axis and passing through the fuel lance. A method includes rotating the fuel lance between a start-up condition and a second condition.

    摘要翻译: 用于燃烧器燃烧器的燃料喷枪具有燃料喷枪体,其限定燃料流动通道和附接到其上的液体燃料尖端并与燃料流动通道流动连通。 液体燃料尖端具有燃料出口和一排空气通道,其具有出口,该出口布置在围绕燃料出口的圆周的空白扇区的外侧,空白扇区由30°至160°的角度限定。 燃烧器包括燃料喷枪和点火器以及主空气流动通道,用于将主气流的至少一部分引导到燃料喷枪上方和点火器上方,空白扇区具有在+ 120°和+ 距离轴线的径向线120°,并穿过燃料喷枪。 一种方法包括在启动条件和第二状态之间旋转燃料喷枪。