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    • 72. 发明申请
    • Hydraulic Machine
    • 液压机
    • US20140186186A1
    • 2014-07-03
    • US14122212
    • 2012-07-26
    • Voith Patent GmbH
    • Sebastian HyneckGerhard Wengert
    • F03B3/02F03B11/04
    • F03B3/02F03B3/186F03B11/02F03B11/04F05B2230/232Y02E10/223Y02E10/226Y02P70/525
    • The invention relates to a hydraulic machine having an impeller wheel that comprises a plurality of impeller blades; having a spiral housing that encloses the impeller wheel and that is open toward said impeller wheel by a circumferential slit formed by two circumferential edges; having a traverse ring, comprising two traverse ring decks that are connected to one another by tension anchors; wherein the spiral housing is composed of segments that meet in the flow direction and that are welded to each other, the ends of which segments stand on the respective traverse ring deck and are welded to said deck; wherein at the meeting point between two segments that are adjacent to one another and one traverse ring deck a stiffening element is provided that protrudes into the inner space of the spiral housing; and wherein the extension of the stiffening element into the inner space of the spiral housing is so small that the flow is not affected in a significant manner.
    • 本发明涉及一种具有叶轮的液压机,其包括多个叶轮叶片; 具有螺旋壳体,其包围叶轮,并且通过由两个圆周边缘形成的周向狭缝朝向所述叶轮旋转; 具有横动环,包括通过张力锚连接到彼此的两个横越环面板; 其中所述螺旋壳体由在流动方向上相遇并且彼此焊接的段组成,所述段的端部在相应的横越环面上站立并焊接到所述平台; 其特征在于,在彼此相邻的两个段之间的会合点处,并且设置有一个横向环板,该加强元件突出到所述螺旋壳体的内部空间中; 并且其中所述加强元件延伸到所述螺旋壳体的内部空间中非常小,使得所述流动不会以显着的方式受到影响。
    • 76. 发明申请
    • Francis turbine
    • 弗朗西斯涡轮机
    • US20050089404A1
    • 2005-04-28
    • US10914639
    • 2004-08-10
    • Yasuyuki EnomotoToshiaki SuzukiSadao KurosawaTakanori Nakamura
    • Yasuyuki EnomotoToshiaki SuzukiSadao KurosawaTakanori Nakamura
    • F03B3/12F01D17/12F03B3/02F03B3/10
    • F03B3/125Y02E10/223Y10S416/02
    • A Francis turbine with an improved shape of blades, which can reduce a circumferential velocity component generated in the flow downstream of the blades in a condition of a partial load operation, or reduce the secondary flow around the blades, is provided. A Francis turbine comprises a crown, a plurality of blades, and a band. The crown can rotate around a rotating axis. The blades are circumferentially arranged on the crown, each of which including an inner end as a trailing edge. The band is coaxially coupled with the crown by the blades. A distance Rc can be defined as a distance between the rotation axis and an end by the crown side of the trailing edge. A distance Rb can be defined as a distance between the rotation axis and an end by the band side of the trailing edge. The distance Rc and the distance Rb satisfy 0.2 ≤ R c R b ≤ 0.4 .
    • 提供了具有改进的叶片形状的弗朗西斯涡轮机,其可以在局部加载操作的情况下减少在叶片下游的流中产生的圆周速度分量或减小叶片周围的二次流动。 弗朗西斯涡轮机包括冠部,多个叶片和带。 表冠可绕旋转轴线旋转。 叶片周向地布置在冠部上,每个叶片包括作为后缘的内端。 该带与叶片同冠状地共同连接。 距离Rc可以被定义为旋转轴线与末端之间的距离,由后缘的冠侧。 距离Rb可以被定义为在后缘的带侧之间的旋转轴线和端部之间的距离。 距离Rc和距离Rb满足 0.2 <= / MO> <= 0.4
        • 77. 发明授权
        • Runner for Francis-type hydraulic turbine
        • 弗朗西斯型液压涡轮机
        • US6135716A
        • 2000-10-24
        • US194540
        • 1999-01-08
        • Jan Tore BilldalOlav RommetveitHermod Brekke
        • Jan Tore BilldalOlav RommetveitHermod Brekke
        • F03B3/12F03B3/02
        • F03B3/125Y02E10/223
        • Disclosed is a runner for a Francis-type hydraulic turbine, comprising a ring, a hub, and a number of blades all having a curved shape and being attached to the ring and hub. Each blade has an inlet edge and an outlet edge. The blades are characterized in that, in the direction of turbine rotation, the junction point of each blade inlet edge at the ring is located forwardly of the inlet edge attachment point for that blade at the hub, and the junction point of each blade outlet edge at the hub is located forwardly of the outlet edge attachment point for that blade at the ring.
        • PCT No.PCT / NO97 / 00194 Sec。 371日期1999年1月8日第 102(e)1999年1月8日PCT PCT 1997年7月28日PCT公布。 公开号WO98 / 05863 日期1998年2月12日公开是用于弗朗西斯型水轮机的转轮,包括环,轮毂和多个具有弯曲形状并且附接到环和轮毂的叶片。 每个叶片具有入口边缘和出口边缘。 叶片的特征在于,在涡轮机旋转的方向上,环处的每个叶片入口边缘的连接点位于毂处的该叶片的入口边缘连接点的前方,并且每个叶片出口边缘的连接点 在轮毂处位于环上的刀片的出口边缘连接点的前方。