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    • 1. 发明公开
    • MOTOR ROTOR STRUCTURE FOR ELECTRIC TURBO CHARGER AND METHOD OF ASSEMBLING SAME
    • 电动涡轮增压器的电动机转子结构及其组装方法
    • EP3279446A1
    • 2018-02-07
    • EP17190092.1
    • 2012-06-04
    • Mitsubishi Heavy Industries, Ltd.
    • YAMASHITA, YukioHAYASHI, NoriyukiIBARAKI, SeiichiOSAKO, KatsuyukiEBISU, MotokiAN, ByeongilSUZUKI, HiroshiARITA, HideakiGOTO, TakashiMIYAKE, Toshihiko
    • F02B39/00F02B37/10F02B39/10H02K1/28H02K1/30H02K11/00F02C6/12
    • H02K1/22F02C6/12F05D2220/76F05D2230/60H02K1/28H02K1/30H02K7/08H02K11/21H02K15/02Y10T29/49012
    • An object of the invention is to provide a motor rotor structure for an electric turbo charger which can be manufactured at a low cost while ensuring the assembly quality of a motor rotor for an electric turbo charger by fixedly fitting, over a shaft, a rotor core having electromagnetic steel sheets pre-formed as an integrated stack in such a manner as to prevent the rotor core from rotating relative to the shaft. The motor rotor structure for an electric turbo charger is characterized by including: a rotor core (80) which is rotated by a magnetic field formed by a stator placed in a housing; a shaft (100) configured to rotate a compressor impeller (3) and the rotor core (80) together; and a bearing which supports the shaft (100) rotatably, wherein the motor rotor includes: the rotor core (80) which has electromagnetic steel sheets previously integrated as a stack; a stopper portion (28) which is formed at an intermediate portion of the shaft (100) in the thrust direction of the shaft to restrict axial movement of the rotor core (80); and a pressing unit (28, 43) which presses the rotor core (80) fitted over the shaft (100) against the stopper portion (28), the pressing unit preventing a circumferential phase shift between the shaft (100) and the rotor core (80) by a pressing force thereof, wherein the rotor core (80) has an inner sleeve (81) fitted over the shaft (100) and the plurality of electromagnetic steel sheets (67) which are fitted over the inner sleeve (81) and stacked on one another in a thrust direction of the inner sleeve (81), wherein
      the pressing unit (28, 43) presses the inner sleeve (81), and wherein the bearing arrangement (83 , 84) consists of ball bearings and the rotor core (80) has a side surface which is opposed to the ball bearings and which is formed with a flange portion (82) extending radially from an open end peripheral edge of the inner sleeve (81), wherein an elastic member (28) is interposed between the flange portion (82) and a bearing (83) of the ball bearing arrangement (83, 84).
    • 本发明的目的是提供一种用于电涡轮增压器的电动机转子结构,该电动涡轮增压器能够以低成本制造,同时通过在轴上固定地安装转子芯来确保用于电动涡轮增压器的电动机转子的组装质量 具有以防止转子芯相对于轴旋转的方式预先形成为整体堆叠的电磁钢板。 用于电动涡轮增压器的电机转子结构的特征在于包括:转子铁心(80),其通过由放置在壳体中的定子形成的磁场而旋转; 轴(100),其构造成使压缩机叶轮(3)和转子芯(80)一起旋转; (100)可旋转地支承的轴承,其中,所述电动机转子包括:具有预先集成为电池堆的电磁钢板的转子铁芯(80) 止动部(28),其沿所述轴的推力方向形成在所述轴(100)的中间部分处,以限制所述转子芯(80)的轴向移动; 和按压单元(28,43),所述按压单元将安装在所述轴(100)上的所述转子芯(80)压靠所述止动部(28),所述加压单元防止所述轴(100)和所述转子芯 (80),其中转子铁芯(80)具有装配在轴(100)上的内套筒(81)和装配在内套筒(81)上的多个电磁钢板(67) 并且在内套筒(81)的推力方向上彼此堆叠,其中挤压单元(28,43)挤压内套筒(81),并且其中轴承装置(83,84)由滚珠轴承组成并且 转子铁芯80具有与滚珠轴承相对的侧表面,并且形成有从内套筒81的开口端周缘沿径向延伸的凸缘部分82, 介于凸缘部分(82)和滚珠轴承装置(83,84)的轴承(83)之间。
    • 4. 发明公开
    • SCROLL STRUCTURE OF TURBINE HOUSING
    • RADIATIONCHNECKENSTRUKTURFÜREINTURBINENGEHÄUSE
    • EP2803839A1
    • 2014-11-19
    • EP12864916.7
    • 2012-10-10
    • Mitsubishi Heavy Industries, Ltd.
    • YOSHIDA, ToyotakaYOKOYAMA, TakaoEBISU, Motoki
    • F02B39/00
    • F04D29/403F01D9/026F02B37/025F02C6/12F05D2220/40
    • An object of the invention is to provide a scroll structure of a turbine housing of a twin scroll turbocharger of which flow-through abilities of two exhaust gas passages are equal to each other. A tongue (44), which partitions a scroll portion (26) into an outer peripheral portion (26a) and an inner peripheral portion (26b) in a longitudinal section parallel to a flow direction of an exhaust gas, is formed at the turbine housing (32), the tongue (44) includes a front-side tongue (46) and a rear-side tongue (48) that respectively close the two exhaust gas passages at the outer peripheral portion (26a) in a cross-section, and respective inner sides (46a, 48a) of the front-side tongue (46) and the rear-side tongue (48) and respective minimal outflow width portions (56a, 58a) of a front-side passage (22) and a rear-side passage (24) are formed substantially parallel to each other in the cross-section at a downstream end of the outer peripheral portion (26a).
    • 本发明的目的是提供一种双涡旋涡轮增压器的涡轮壳体的涡旋结构,其中两个排气通道的流通能力彼此相等。 在涡轮机壳体上形成有将涡旋部分(26)分隔成外周部分(26a)和沿着与废气的流动方向平行的纵截面的内周部分(26b)的舌片(44) (32)中,所述舌部(44)包括在所述外周部(26a)处截面分别封闭所述两个排气通路的前侧舌片(46)和后侧舌片(48),以及 前侧襟翼(46)和后侧榫舌(48)的内侧(46a,48a)和前侧通道(22)和后侧通道(22)的相应最小流出宽度部分(56a,58a) 在所述外周部(26a)的下游端的横截面形成有大致平行的侧通路(24)。
    • 6. 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。
    • 8. 发明公开
    • EXHAUST TURBO-SUPERCHARGER
    • Abgasturbolader
    • EP1785613A2
    • 2007-05-16
    • EP06121974.7
    • 2006-10-09
    • MITSUBISHI HEAVY INDUSTRIES, LTD.
    • YOKOYAMA, TakaoIBARAKI, SeiichiOSAKO, KatsuyukiEBISU, Motoki
    • F02C6/12
    • F02C7/24F01D9/026F05D2220/40F05D2240/12F05D2250/323F05D2260/94
    • An exhaust turbo-supercharger having a high efficiency is provided. The exhaust turbo-supercharger includes therein an exhaust turbine housing including a spiral channel and a turbine-accommodating chamber connected to an innermost peripheral part of the spiral channel; an exhaust turbine provided in the turbine-accommodating chamber so that the axial line of the exhaust turbine is parallel to that of the spiral channel; a shaft that is concentrically connected to one side of the exhaust turbine in the axial line direction; a bearing housing disposed at the side of the exhaust turbine in the axial line direction so as to be adjacent to the exhaust turbine housing; a bearing that is provided in the bearing housing and that rotatably supports the shaft around the axial line; and a heat shield component interposed between the exhaust turbine housing and the bearing housing. The heat shield component constitutes a part disposed near the entrance of the turbine-accommodating chamber, the part being a part of the inner wall surface of the spiral channel. The part composed of the heat shield component, the part being a part of the inner wall surface of the spiral channel, forms a protruding part protruding toward the inside of the channel relative to an upstream part.
    • 提供了具有高效率的排气涡轮增压器。 排气涡轮增压器包括:排气涡轮机壳体,其包括螺旋通道和连接到螺旋通道的最内周部分的涡轮容纳室; 设置在所述涡轮机容纳室中的排气涡轮,使得所述排气涡轮机的轴线与所述螺旋通道的轴线平行; 同轴地连接到所述排气涡轮机的轴线方向的一侧的轴; 轴承壳体,其在所述排气涡轮机的一侧沿轴线方向设置成与所述排气涡轮机壳体相邻; 轴承,其设置在所述轴承壳体中并且可旋转地支撑所述轴围绕所述轴线; 以及插入在所述排气涡轮壳体和所述轴承壳体之间的隔热部件。 隔热部件构成设置在涡轮容纳室的入口附近的部分,该部分是螺旋通道的内壁表面的一部分。 由隔热部件构成的部分,作为螺旋形通道的内壁面的一部分的部分形成相对于上游部向通道内侧突出的突出部。