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    • 2. 发明公开
    • TURBINE ROTOR AND TURBOCHARGER INCORPORATING SUCH TURBINE ROTOR
    • TURBINENROTOR UND TURBOLADER MIT SOLCH EINEM TURBINENROTOR
    • EP2960463A4
    • 2016-04-13
    • EP13875417
    • 2013-02-22
    • MITSUBISHI HEAVY IND LTD
    • OTSUBO HITOMIARAI TAKASHINAKAGAWA HIROSHIYAMAGUCHI HIDEKIYOSHIDA MASAKAZU
    • F02B39/00F01D5/02F01D5/04F02B39/16
    • F01D5/027F01D5/04F01D5/048F01D5/28F05D2220/40F05D2300/174
    • A turbine rotor comprising: a turbine wheel 5 obtainable by precision casting of titanium aluminide, including a hub 50 extending along a rotational center of the turbine wheel, and a plurality of impellers 40 arranged along a circumferential direction around an outer circumference of the hub, and having a web-like scallop 30 formed by making a cutout between adjacent impellers among the plurality of the impellers; and a rotor shaft 7 extending along the rotational center line C-C of the turbine wheel on a back side of the hub of the turbine wheel; wherein the turbine wheel has a balance cut portion 11 arranged along the circumferential direction of the rotational turbine wheel on the back side of the hub of the turbine wheel, wherein an area of the balance correcting part arranged in the circumferential direction is placed so that a balance cut minimum diameter BCmin is larger than a maximum diameter of the rotor shaft on the wheel mounting side, and that a balance cut maximum diameter BCmax is smaller than a scallop diameter S of the turbine wheel, and that a thickness t from the back side of the turbine wheel to a surface of the hub satisfies 1.75t‰¥w, where w is a width in a radial direction of the area arranged in the circumferential direction (i.e. balance cut).
    • 一种涡轮转子,其特征在于,包括:通过精密铸造钛酸铝而获得的涡轮机轮5,其包括沿涡轮机叶轮的旋转中心延伸的轮毂50以及围绕轮毂的外周沿圆周方向布置的多个叶轮40, 并且具有通过在多个叶轮之间的相邻叶轮之间形成切口而形成的网状扇贝30; 以及转子轴7,其沿着涡轮机叶轮的轮毂的后侧​​沿着涡轮机叶轮的旋转中心线C-C延伸; 其特征在于,所述涡轮机叶轮具有在所述涡轮机叶轮的所述轮毂的背侧沿着所述旋转涡轮机叶轮的圆周方向配置的平衡切割部11,其中,所述平衡校正部的沿圆周方向配置的区域被配置为 平衡切割最小直径BCmin大于轮安装侧的转子轴的最大直径,平衡切割最大直径BCmax小于涡轮机叶轮的扇形直径S,并且来自后侧的厚度t 涡轮机轮毂到轮毂表面的距离满足1.75t‰,其中w是沿圆周方向排列的区域的径向宽度(即平衡切削)。
    • 6. 发明专利
    • Turbocharger
    • 涡轮增压器
    • JP2013174129A
    • 2013-09-05
    • JP2012037504
    • 2012-02-23
    • Mitsubishi Heavy Ind Ltd三菱重工業株式会社
    • YAMAGUCHI HIDEKIARAI TAKASHIYOKOYAMA TAKAO
    • F02B39/00F01D11/02F01D25/24
    • F04D29/102F01D11/02F01D11/025F01D25/125F02B37/00F02C6/12F04D29/5853F05D2220/40
    • PROBLEM TO BE SOLVED: To provide a turbocharger which includes a turbine rotor comprising a turbine wheel and a shaft that are joined by a brazing filler metal and in which an amount of exhaust gas leaking from an entrance side of the turbine wheel through a back face to a brazed part is decreased to suppress reduction in the strength of the brazed part due to a rise in the temperature in the brazed part during an operation.SOLUTION: A turbocharger including a turbine housing 3 and a bearing housing 10 includes; a back plate 11 disposed on a back side of the turbine wheel 5 along the back side, leaving a clearance from the back side; a fixing part 11a of the back plate formed on an outer periphery of the back plate 11 and fixed to a joined part between the turbine housing 3 and the shaft housing 10; an opening 35 that is formed in an inner periphery of the back plate 11 and into which a cylindrical flange 10b is inserted while leaving a clearance; and a throttle part 36 formed between the back side of the turbine wheel 5 and a side face on the inner periphery of the back plate 11, for suppressing a flow volume of exhaust gas leaking from an entrance side of the turbine wheel 5 through the back side to a joined part B of a brazing filler metal.
    • 要解决的问题:提供一种涡轮增压器,其包括涡轮转子,所述涡轮转子包括涡轮机叶轮和轴,所述涡轮机叶轮和轴由钎焊金属接合,并且其中从涡轮机叶轮的入口侧泄漏的废气量通过背面 减少到钎焊部分以抑制由于钎焊部件在操作期间的温度升高导致的钎焊部件的强度降低。解决方案:包括涡轮机壳体3和轴承壳体10的涡轮增压器包括: 背板11,其沿着后侧设置在涡轮机叶轮5的后侧,从后侧留出间隙; 背板的固定部分11a形成在背板11的外周上并固定在涡轮机壳体3和轴壳体10之间的接合部分上; 在后板11的内周形成开口部35,并且在离开间隙的同时插入有圆筒状的凸缘10b; 以及形成在涡轮机叶轮5的后侧和后板11的内周的侧面之间的节流部36,用于抑制从涡轮机叶轮5的入口侧通过背面泄漏的废气的流量 一侧到钎焊料的接合部分B.