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    • 1. 发明申请
    • STAGING FUEL NOZZLE
    • STAGING燃油喷嘴
    • US20100308135A1
    • 2010-12-09
    • US12790154
    • 2010-05-28
    • Takeshi YamamotoKazuo ShimodairaKazuaki MatsuuraYoji KurosawaSeiji Yoshida
    • Takeshi YamamotoKazuo ShimodairaKazuaki MatsuuraYoji KurosawaSeiji Yoshida
    • F02C7/22
    • F23R3/286F23D2900/11101F23R3/343
    • A main swirler of a triple annular configuration that is partitioned by a pre-filmer and a separator is installed in an inlet port of a main air flow channel. The vicinity of the inner wall of the main air flow channel provided with a main fuel injection port is bulged radially outward from the innermost surface (innermost surface of a small swirler) of a main swirler. Further, a distance from the main fuel injection port and the pre-filmer is set such that an effective opening area between the pre-filmer and “the inner wall of the main air flow channel provided with the main fuel injection port” is equal to an effective opening area of the small swirler. The swirling directions of the swirlers of the main swirler are “clockwise”-“counter-clockwise”-“clockwise” respectively along the radial outward direction when the swirling direction of the innermost swirler is taken as “clockwise”.
    • 主空气流通道的入口端安装有由预滤器和分离器分隔的三重环形构造的主旋流器。 设置有主燃料喷射口的主空气流动通道的内壁附近从主旋流器的最内表面(小旋流器的最内表面)径向向外凸出。 此外,与主燃料喷射口和预滤波器的距离被设定为使得预滤波器与“设置有主燃料喷射口的主空气流路的内壁”之间的有效开口面积等于 小旋流器的有效开放面积。 当最内旋流器的旋转方向为“顺时针”时,主旋流器的旋流器的旋转方向分别沿径向向外方向“顺时针” - “逆时针” - “顺时针”。
    • 3. 发明授权
    • Staging fuel nozzle
    • 分段燃油喷嘴
    • US08327643B2
    • 2012-12-11
    • US12790154
    • 2010-05-28
    • Takeshi YamamotoKazuo ShimodairaKazuaki MatsuuraYoji KurosawaSeiji Yoshida
    • Takeshi YamamotoKazuo ShimodairaKazuaki MatsuuraYoji KurosawaSeiji Yoshida
    • F02C1/00F23D11/10F02M61/00F02M61/02F02M63/00
    • F23R3/286F23D2900/11101F23R3/343
    • A main swirler of a triple annular configuration that is partitioned by a pre-filmer and a separator is installed in an inlet port of a main air flow channel. The vicinity of the inner wall of the main air flow channel provided with a main fuel injection port is bulged radially outward from the innermost surface (innermost surface of a small swirler) of a main swirler. Further, a distance from the main fuel injection port and the pre-filmer is set such that an effective opening area between the pre-filmer and “the inner wall of the main air flow channel provided with the main fuel injection port” is equal to an effective opening area of the small swirler. The swirling directions of the swirlers of the main swirler are “clockwise”-“counter-clockwise”-“clockwise” respectively along the radial outward direction when the swirling direction of the innermost swirler is taken as “clockwise”.
    • 主空气流通道的入口端安装有由预滤器和分离器分隔的三重环形构造的主旋流器。 设置有主燃料喷射口的主空气流动通道的内壁附近从主旋流器的最内表面(小旋流器的最内表面)径向向外凸出。 此外,与主燃料喷射口和预滤波器的距离被设定为使得设置有主燃料喷射口的主空气流路的预滤波器与内壁之间的有效开口面积等于有效 开口面积小的旋流器。 主旋流器的旋流器的旋转方向分别沿着径向向外的方向顺时针 - 逆时针顺时针旋转,当最内旋流器的旋转方向被取为顺时针方向时。