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公开(公告)号：EP0575617A4
公开(公告)日：1996-10-16
申请号：EP92906689
申请日：1992-03-16
IPC分类号： B22D11/06
CPC分类号： B22D11/066
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2.发明公开DUAL DRUM TYPE CONTINUOUS CASTING DEVICE AND METHOD FOR CONTINUOUS CASTING 有权ZWEIROLLEN-STRANGGIESSMASCHIENEUND STRANGGIESSVERFAHREN
公开(公告)号：EP1302260A4
公开(公告)日：2004-08-25
申请号：EP01950031
申请日：2001-07-19
发明人： YAMAMOTO KEIICHI , HASHIMOTO RITSUO , TANI MITSUO , YOKOO KAZUTOSHI , YUSA JYOJI , SASAKI K , MIYAKE KATSUYOSHI , ISOGAMI KATSUYUKI , YAMADA MAMORU , TANAKA TSUYOSHI , ARAI TAKASHI , IZU TADAHIRO , TSUNENARI KEIJI , YAMAMURA KAZUTO , IZAKI HIROSHI
IPC分类号： B22D11/06
CPC分类号： B22D11/0651 , B22D11/0622 , B22D11/0682
摘要： A dual drum type continuous casting device capable of casting a sheet metal (4) by feeding molten metal (3) to a molten metal sump formed of a pair of cooling drums (1) rotated in the directions reverse to each other and a side dam (2) and bringing the molten metal into contact with the surface of the cooling drums (1) to cool the molten metal so as to form a solidified shell, wherein the cooling drums (1) are formed of a drum shell body (11) having a shaft part at both side end parts thereof and a drum sleeve (10) fitted onto the outer peripheral part of the drum shell body (11), and a means to avoid various types of adverse effects caused by a difference in thermal expansion between the structural members of the drum shell body (11) in the casting is provided to increase the reliability of the device and the quality of the casting.
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3.发明公开
公开(公告)号：EP3276143A4
公开(公告)日：2018-04-25
申请号：EP15886346
申请日：2015-03-25
发明人： ARAI TAKASHI , WATANABE DAIGO , MURONO WATARU , YAMAGUCHI HIDEKI , TORIGOE TAIJI , INOUE AKI , KONNO YUYA
CPC分类号： F04D29/284 , C23C18/1637 , C23C18/50 , F01D5/288 , F01D9/026 , F02B37/00 , F02B39/00 , F02M26/06 , F04D29/023 , F05D2220/40 , F05D2230/31 , F05D2300/604 , F05D2300/611 , F05D2300/6111
摘要： An impeller for a rotary machine includes: a base material of the impeller comprising Al or an Al alloy; and an electroless plating layer disposed so as to cover the base material, the electroless plating layer forming a surface layer of the impeller. The electroless plating layer comprises a Ni-P based alloy having an amorphous structure, the Ni-P based alloy having a P content rate of not less than 5wt% and not more than 11wt% in the electroless plating layer.
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4.发明公开STRUCTURE AND METHOD FOR BONDING NOZZLE VANE AND LEVER, AND VARIABLE-CAPACITY TURBOCHARGER 审中-公开结构与方法粘结叶片和连杆和涡轮增压可变容量
公开(公告)号：EP3085920A4
公开(公告)日：2017-01-04
申请号：EP13899660
申请日：2013-12-16
发明人： ARAI TAKASHI , OTSUBO HITOMI
IPC分类号： F02B39/00 , B23K31/00 , B23K101/00 , B23K103/18 , F01D17/16 , F02B37/24 , F02C6/12
CPC分类号： F02B37/24 , B23K15/0053 , B23K15/0093 , B23K26/28 , B23K26/323 , B23K31/003 , B23K2201/001 , B23K2203/05 , B23K2203/18 , B23K2203/26 , F01D5/04 , F01D9/02 , F01D17/16 , F01D17/165 , F02B33/40 , F02B39/00 , F02C6/12 , F05D2220/40 , F05D2230/232 , F05D2300/177 , Y02T10/144
摘要： An object is to provide a structure and a method of joining a nozzle vane and a lever, and a variable geometry turbocharger, capable of reducing breakage of a welded part between a shaft portion of the nozzle vane and the lever during usage of the same by reducing generation of a hot crack in weld metal at the welded part. A joint structure includes: a nozzle vane 2 disposed in an exhaust passage for guiding exhaust gas to a turbine wheel 34 of a variable geometry turbocharger 500, and including a shaft portion 2a; and a lever 1 including a fitting surface 42a fitted with a peripheral surface 72 on one end side of the shaft portion, for transmitting torque to the shaft portion to adjust a vane angle of the nozzle vane. Weld metal 50 at a welded part 40 between the lever and the nozzle vane is formed so that a center position 64 of the weld metal is disposed inside a position 17 of the fitting surface with respect to a radial direction of the shaft portion.
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5.发明公开DEMAND FORECASTING DEVICE, DEMAND FORECASTING METHOD, AND DEMAND FORECASTING PROGRAM 审中-公开需求预测设备需求预测程序需求预测计划
公开(公告)号：EP2763096A4
公开(公告)日：2015-06-17
申请号：EP12836050
申请日：2012-09-24
发明人： MITSUHASHI MASATO , MATSUO ATSUSHI , ARAI TAKASHI
CPC分类号： G06Q30/0202 , G06Q10/04
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6.发明公开TURBINE ROTOR AND TURBOCHARGER INCORPORATING SUCH TURBINE ROTOR 有权TURBINENROTOR UND TURBOLADER MIT SOLCH EINEM TURBINENROTOR
公开(公告)号：EP2960463A4
公开(公告)日：2016-04-13
申请号：EP13875417
申请日：2013-02-22
CPC分类号： F01D5/027 , F01D5/04 , F01D5/048 , F01D5/28 , F05D2220/40 , F05D2300/174
摘要： 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).
摘要翻译： 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）。
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公开(公告)号：EP2821618A4
公开(公告)日：2015-12-23
申请号：EP13755039
申请日：2013-02-26
发明人： YAMAGUCHI HIDEKI , ARAI TAKASHI
IPC分类号： F02B39/00 , B23K1/00 , B23K1/19 , B23K103/24 , C22C14/00 , C22C38/00 , C22C38/38 , F01D5/04 , F01D25/00
CPC分类号： F01D5/08 , B22F3/15 , B23K1/00 , B23K1/0008 , B23K1/0018 , B23K1/19 , B23K35/002 , B23K35/004 , B23K35/0222 , B23K35/26 , B23K35/3033 , C22C14/00 , C22C19/03 , C22C38/00 , C22C38/04 , C22C38/18 , C22C38/38 , F01D5/026 , F05D2220/40 , F05D2230/237 , F05D2300/171 , F05D2300/174
摘要： A turbine rotor for a supercharger includes a TiAl turbine wheel and a carbon steel shaft joined to each other via an Ni brazing filler metal at a brazed part distanced from a back face of the turbine wheel so that a turbine wheel outer diameter ratio calculated by "a distance from the back face of the turbine wheel to the brazed part" / "an outer diameter of the turbine wheel" is within a range of from 7 to 10%.
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公开(公告)号：EP2821617A4
公开(公告)日：2015-12-09
申请号：EP13754668
申请日：2013-02-26
发明人： OTSUBO HITOMI , ARAI TAKASHI , EBISU MOTOKI
CPC分类号： F01D5/025 , B23K15/0006 , B23K15/0026 , B23K15/0053 , B23K26/702 , B23K2201/001 , C21D1/09 , C21D1/30 , C21D9/0068 , C21D9/50 , F01D5/063 , F05D2220/40 , F05D2230/234 , F05D2230/40 , F05D2240/60
摘要： To provide a turbine rotor which enables mass production with a low-cost apparatus and which capable of suppressing leaning of the rotor shaft after welding to improve the yield, while a turbine blade rotor 12 and the rotor shaft 14 are fit to each other with concave and convex portions 12a and 14a and are permitted to be rotated, laser beam L from a laser beam generating device 30 is applied to a joint face 16 along the circumferential direction to weld the welding portion. Then, laser beam L is polarized to temper a region X on the rotor shaft side containing the welding portion with laser beam L. In contrast to residual stress R 1 having a local angular distribution generated during the welding, residual stress R 2 is permitted to be generated over the entire circumference by tempering. Leaning of the rotor shaft 14 after cooling is thereby be suppressed.
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公开(公告)号：EP2884073A4
公开(公告)日：2015-10-14
申请号：EP13827476
申请日：2013-08-07
CPC分类号： F04D27/002 , F01D17/165 , F02B37/24 , F02M26/00 , F04D19/02 , F04D29/023 , F05D2220/40 , F05D2300/17 , F05D2300/50212
摘要： An object is to provide a variable-geometry exhaust turbocharger including a variable nozzle mechanism in which nozzle supports may not deform under a high-temperature condition. A variable-geometry exhaust turbocharger (1) includes: a nozzle mount (2); a nozzle support (6) having a first end coupled to a first face (2a) of the nozzle mount; a nozzle plate (4) coupled to the second end of the nozzle support and supported to be separated from the first face (2aa) of the nozzle mount, the nozzle plate having a first face (4a) coupled to the nozzle support and a second face (4b) which is opposite to the first face and which faces an exhaust gas channel (20) through which exhaust gas flows: a plurality of nozzle vanes (8) rotatably supported between the nozzle mount and the nozzle plate; and a variable nozzle mechanism (10) configured to change vane angles of the nozzle vanes to control a flow of the exhaust gas flowing between the nozzle mount and the nozzle plate. The nozzle plate is formed of a material having a smaller linear expansion coefficient than that of a material forming the nozzle mount.
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公开(公告)号：EP2377960A4
公开(公告)日：2016-12-14
申请号：EP09833255
申请日：2009-07-30
发明人： ARAI TAKASHI
摘要： A ductile iron having superior high-temperature strength and oxidation resistance at temperatures exceeding 800°C compared with conventional high Si and Mo ductile iron. The ductile iron comprises, in terms of mass ratio, carbon: 2.0 to 4.0%, silicon: 3.5 to 5.0%, manganese: not more than 1.0%, chromium: 0.1 to 1.0%, molybdenum: 0.2 to 2.0%, vanadium: 0.1 to 1.0%, and magnesium: 0.02 to 0.1%, with the remainder being composed of iron and unavoidable impurities.
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