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    • 9. 发明公开
    • TURBINE WHEEL
    • 涡轮机轮
    • EP2410126A1
    • 2012-01-25
    • EP10828136.1
    • 2010-07-28
    • Mitsubishi Heavy Industries, Ltd.
    • YOKOYAMA, TakaoOSAKO, KatsuyukiYOSHIDA, ToyotakaEBISU, Motoki
    • F01D1/28F01D5/04F02B39/00F02C3/05
    • F01D5/048F01D1/28F05D2220/40F05D2240/307F05D2250/70F05D2260/20
    • Providing a turbine wheel that includes, but not limited to: a plurality of blade parts and a scallop cut-out profile, the scallop cut-out profile being formed by cutting-out the back side wall part of the turbine wheel between the suction surface side of a blade part and the pressure surface side of the adjacent blade part, wherein the leakage flow on the rear side of the blade part is constrained so as to enhance the turbocharger efficiency. Providing the blade part 5 (i.e. the area between the scallop parts on the tip end side of the blade part) with the suction surface side extended part 25 in the neighborhood of the suction surface 21 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased; or, the pressure surface side extended part 32 in the neighborhood of the pressure surface 19 of the blade part so that the thickness of the blade part on the tip end side of the scallop cut-out profile is increased. Or, the positive/suction surface side extended parts are provided. Thereby, the extended width of the extended part is formed so that the width is an almost constant width along the camber line of the blade part from the tip end side to the root side of the blade, the projecting-out width part forming a strip area.
    • 提供涡轮机叶轮,该涡轮机叶轮包括但不限于:多个叶片部件和扇贝切口轮廓,扇贝切口轮廓通过将涡轮机叶轮的后侧壁部分切除在吸力表面 其中叶片部分后侧的泄漏流被约束以提高涡轮增压器的效率。 在叶片部的吸附面21的附近设置叶片部5(即,叶片部的前端侧的扇贝状部分之间的区域)与吸附面侧延伸部25,使得叶片的厚度 扇贝切出轮廓的顶端侧的部分增加; 或者在叶片部分的压力表面19附近的压力表面侧延伸部分32,以便扇贝切口轮廓的顶端侧上的叶片部分的厚度增加。 或者,设置正/负表面侧延伸部。 由此,延伸部的延伸宽度形成为,从叶片的前端侧到根部侧沿着叶片部的弧线的宽度大致恒定,形成条的突出宽度部 区。