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    • 1. 发明公开
    • Centrifugal compressor, impeller and operating method of the same
    • Zentrifugalkompressor,Zentrifugallaufrad und Betriebsverfahrendafür
    • EP2020509A2
    • 2009-02-04
    • EP08013769.8
    • 2008-07-31
    • Hitachi Plant Technologies, Ltd.
    • Yagi, ManabuKishibe, TadaharuShibata, TakanoriNishida, HideoKobayashi, HiromiKuwano, Tetsuya
    • F04D29/28F04D29/30
    • F04D29/284F04D29/30
    • It is an object of the prevent invention to provide a centrifugal compressor equipped with an impeller having a blade angle distribution that makes it possible to achieve a relatively wide operating range. In a centrifugal compressor, assuming that a blade angle of a shroud side facing a circular plate of a blade is a first angle and a blade angle of a hub side disposed at the circular plate is a second angle, the shroud side is formed in a curved shape having an angle distribution from a front area in a shaft direction toward a centrifugal direction in which the first angle is the local maximum point before a substantially middle portion and the local minimum point after the substantially middle point, and the hub side is formed in a curved shape having an angle distribution from the front area in the shaft direction toward the centrifugal direction in which the second angle is the maximum local point before the substantially middle portion.
    • 本发明的目的在于提供一种配备有具有叶片角度分布的叶轮的离心式压缩机,其能够实现相对宽的工作范围。 在离心压缩机中,假设面向叶片的圆板的护罩侧的叶片角度为第一角度,并且设置在圆板上的轮毂侧的叶片角度为第二角度,护罩侧形成为 具有从轴方向的前方区域朝向离心方向的角度分布的弯曲形状,其中第一角度在大致中间部分之前的局部最大点和大致中间点之后的局部最小点,并且形成毂侧 其形状为从轴方向的前方区域朝向离心方向的角度分布的曲线形状,其中第二角度为大致中间部分之前的最大局部点。
    • 3. 发明公开
    • Turbo machinery
    • Radialturbomaschine
    • EP2314876A2
    • 2011-04-27
    • EP10188580.4
    • 2010-10-22
    • Hitachi Plant Technologies, Ltd.
    • Shibata, TakanoriYagi, ManabuNishida, HideoKobayashi, HiromiTanaka, Masanori
    • F04D17/12F04D29/44
    • F04D29/444F04D17/12F04D29/681F05D2250/52
    • Turbo machinery 100 comprising an impeller 1 and a diffuser 2 positioned on a downstream side of the impeller 1 that a channel wall surface of the diffuser 2 is composed of a pair of a shroud side diffuser plate 14 and a hub side diffuser plate 9 which surface each other and a channel width is formed so as to be increased downstream, characterized in that guide vanes 12, 13 in a circular arc shape lower in height than the channel width are installed in a line of a plurality of vanes 12, 13 on both channel walls of the shroud side diffuser plate 14 and hub side diffuser plate 9 of the diffuser 2, and a total of vane heights of the two guide vanes 12, 13 at an outlet of the diffuser 2 is set so as to be within a range from 30 to 70% of the channel width at the outlet of the diffuser 2, and assuming an inclination angle of the channel wall surface of the shroud side diffuser plate 14 in a radial direction as θ s , a vane inlet angle of the guide vane 12 installed on the wall surface of the shroud side diffuser plate 14 in a peripheral direction at the inlet as β s, in , an inclination angle of the channel wall surface of the hub side diffuser plate 9 in the radial direction as θ h , and a vane inlet angle of the guide vane 13 installed on the wall surface of the hub side diffuser plate 9 in the peripheral direction at the inlet β h, in , respectively, said four angles conform to a following formula (1), β s in - β h in ⁢ = K ⁢ θ s - θ h 0
      and K of the formula (1) is set so as to conform to a relation of K
    • 涡轮机械100包括叶轮1和位于叶轮1的下游侧的扩散器2,扩散器2的通道壁表面由一对护罩侧扩散板14和毂侧扩散板9组成,该表面 彼此之间形成通道宽度以便在下游增加,其特征在于,高度大于通道宽度的圆弧形状的导向叶片12,13安装在两个叶片12,13上的一条线上 扩散器2的护罩侧扩散板14和轮毂侧扩散板9的通道壁和扩散器2的出口处的两个导叶12,13的总叶片高度被设定在一个范围内 在扩散器2的出口处的通道宽度的30至70%,并且假设护罩侧扩散板14的通道壁表面在径向方向上的倾斜角为¸s,导向叶片的叶片入口角 12安装在t的墙面上 在入口处的周边方向上,护罩侧扩散板14的长度方向上,轮毂侧扩散板9的通道壁面在径向上的倾斜角为¸h,导向件的叶片入口角 叶片13分别安装在轮毂侧扩散板9的壁面上,在入口2 h处于圆周方向,所述四个角分别与下列公式(1)相符:²s in² ¢= 将公式(1)的K ¢¸s-¸h0和K设定为符合K <0的关系。