METHOD FOR THE PRODUCTION OF A ROTATIONALLY SYMMETRICAL PART, AND PART PRODUCED ACCORDING TO SAID METHOD
    2.
    发明申请
    METHOD FOR THE PRODUCTION OF A ROTATIONALLY SYMMETRICAL PART, AND PART PRODUCED ACCORDING TO SAID METHOD 有权
    生产旋转对称部件的方法,以及按照方法生产的部件

    公开(公告)号:US20090312110A1

    公开(公告)日:2009-12-17

    申请号:US12307865

    申请日:2007-07-05

    IPC分类号: F16C3/00 B21D31/00

    CPC分类号: B21H1/18

    摘要: A method for producing a rotationally symmetrical hollow metal part, particularly a shaft. According to the method, bar-shaped ductile solid matrial is provided, the solid material is heated from about 300° C. below the forging temperature to the forging temperature, the solid material is transversally spline-rolled until weakenings are created in the core zone (3) of the solid material and the sold material is torn open. Two mandrels (5,6) are forcibly introduced into the center of the bar-shaped solid material during the rolling process, and then one mandrel is retracted while the other mandrel continues advancing so as to produce a tubular part. A transversally spline-rolled rotationally symmetrical hollow part, especially a shaft, which is produced accoridng to noted method can be embodied as a transmission shaft, camshaft, drive shaft, output shaft, starter shaft, hollow shaft, or can bea preform for molded parts and the like.

    摘要翻译: 用于制造旋转对称的中空金属部件,特别是轴的方法。 根据该方法,提供棒状延性固体材料,将固体材料从锻造温度以下的约300℃加热至锻造温度,将固体材料横向花键滚动直至在芯部区域产生弱化 (3)的固体材料和销售的材料被撕开。 两个心轴(5,6)在轧制过程中强制地引入到棒状固体材料的中心,然后一个心轴缩回,而另一个心轴继续前进,以便产生管状部分。 横向花键滚动的旋转对称的中空部分,特别是根据所指出的方法制造的轴,可以被实现为传动轴,凸轮轴,驱动轴,输出轴,起动轴,空心轴,或者可以是用于模制部件的预成型件 等等。

    Exhaust-gas turbocharger
    3.
    发明授权
    Exhaust-gas turbocharger 有权
    排气涡轮增压器

    公开(公告)号:US09222366B2

    公开(公告)日:2015-12-29

    申请号:US13816516

    申请日:2011-08-18

    IPC分类号: F01D25/16 F01D25/18 F16C17/18

    摘要: An exhaust-gas turbocharger (1), having a shaft (2) on which a compressor wheel (3) and a turbine wheel (4) are arranged, and a bearing housing (5) which has a turbine-side radial bearing bush (6) and which has an oil collecting chamber (7) arranged between the turbine-side radial bearing bush (6) and a turbine-side bearing housing end region (8). The shaft (2) has a shoulder (9) which extends outward in the radial direction (R) into the oil collecting chamber (7) and, together with a radial-bearing-side first delimiting wall (10) of the oil collecting chamber (7), delimits a gap (11).

    摘要翻译: 具有设置有压缩机叶轮(3)和涡轮机叶轮(4)的轴(2)的排气涡轮增压器(1)和具有涡轮侧径向轴承衬套的轴承壳体(5) 6),其具有布置在涡轮机侧径向轴承衬套(6)和涡轮机侧轴承座端部区域(8)之间的集油室(7)。 轴(2)具有沿径向(R)向外延伸进入集油室(7)的肩部(9),并与集油室的径向支承侧第一分隔壁(10)一起 (7),界定了一个差距(11)。

    Turbocharger with improved charge pressure regulating flap configuration
    4.
    发明授权
    Turbocharger with improved charge pressure regulating flap configuration 有权
    具有改进的充气压力调节翼片配置的涡轮增压器

    公开(公告)号:US08205448B2

    公开(公告)日:2012-06-26

    申请号:US12517441

    申请日:2007-10-23

    IPC分类号: F02D23/00 F16K1/16

    摘要: The invention relates to a turbocharger (1) comprising a compressor (2), a turbine connected to the compressor (2) by means of a shaft (3) and provided with an exhaust inlet (5) and an exhaust outlet (7), and a bypass line (6) which branches off from the exhaust inlet (5), bypassing the turbine, and leads to the exhaust outlet in which a boost-pressure regulating flap is arranged, said regulating flap comprising a flap plate (13) which is connected to a flap shaft (14) by means of a connecting device (12).

    摘要翻译: 本发明涉及一种涡轮增压器(1),其包括压缩机(2),通过轴(3)连接到压缩机(2)并且设置有排气入口(5)和排气出口(7)的涡轮机, 和旁路管路(6),其从排气入口(5)分支,绕过涡轮机,并且通向排气出口,其中布置有增压压力调节挡板,所述调节挡板包括挡板(13),该挡板 通过连接装置(12)连接到翼片轴(14)。

    EXHAUST-GAS TURBOCHARGER
    6.
    发明申请
    EXHAUST-GAS TURBOCHARGER 有权
    排气涡轮增压器

    公开(公告)号:US20130236336A1

    公开(公告)日:2013-09-12

    申请号:US13882602

    申请日:2011-11-03

    IPC分类号: F01D25/16

    摘要: An exhaust-gas turbocharger (1) having a compressor (2) which has a compressor wheel (3) in a compressor housing (4); a turbine (5) which has a turbine wheel (6) in a turbine housing (7); a bearing housing (8) which receives a static bearing bush (9) for a rotor shaft (10) and which has, at the compressor side, a bearing housing cover (11), and a bearing bush rotation prevention means (12) which has at least one lug (13, 14, 15) supported in the bearing housing (8) and which engages into at least one of two grooves (16, 17) of the bearing bush (9). The grooves (16, 17) are arranged diametrically oppositely on an outer circumferential region (18) of the bearing bush (9).

    摘要翻译: 具有在压缩机壳体(4)内具有压缩机叶轮(3)的压缩机(2)的废气涡轮增压器(1) 在涡轮壳体(7)中具有涡轮机叶轮(6)的涡轮机(5); 接收用于转子轴(10)的静态轴承衬套(9)并且在压缩机侧具有轴承座盖(11)的轴承壳体(8)和轴承衬套旋转防止装置(12) 具有支撑在所述轴承壳体(8)中并且与所述轴承衬套(9)的两个凹槽(16,17)中的至少一个接合的至少一个凸耳(13,14,15)。 槽(16,17)在轴承衬套(9)的外圆周区域(18)上沿径向相对设置。

    EXHAUST-GAS TURBOCHARGER
    7.
    发明申请
    EXHAUST-GAS TURBOCHARGER 有权
    排气涡轮增压器

    公开(公告)号:US20130142679A1

    公开(公告)日:2013-06-06

    申请号:US13816516

    申请日:2011-08-18

    IPC分类号: F01D25/18

    摘要: An exhaust-gas turbocharger (1), having a shaft (2) on which a compressor wheel (3) and a turbine wheel (4) are arranged, and a bearing housing (5) which has a turbine-side radial bearing bush (6) and which has an oil collecting chamber (7) arranged between the turbine-side radial bearing bush (6) and a turbine-side bearing housing end region (8). The shaft (2) has a shoulder (9) which extends outward in the radial direction (R) into the oil collecting chamber (7) and, together with a radial-bearing-side first delimiting wall (10) of the oil collecting chamber (7), delimits a gap (11).

    摘要翻译: 具有设置有压缩机叶轮(3)和涡轮机叶轮(4)的轴(2)的排气涡轮增压器(1)和具有涡轮侧径向轴承衬套的轴承壳体(5) 6),其具有布置在涡轮机侧径向轴承衬套(6)和涡轮机侧轴承座端部区域(8)之间的集油室(7)。 轴(2)具有沿径向(R)向外延伸进入集油室(7)的肩部(9),并与集油室的径向支承侧第一分隔壁(10)一起 (7),界定了一个差距(11)。

    Method for the production of a rotationally symmetrical part, and part produced according to said method
    8.
    发明授权
    Method for the production of a rotationally symmetrical part, and part produced according to said method 有权
    用于制造旋转对称部分的方法,以及根据所述方法制造的部分

    公开(公告)号:US08312750B2

    公开(公告)日:2012-11-20

    申请号:US12307865

    申请日:2007-07-05

    IPC分类号: B21D17/04 B21D17/08

    CPC分类号: B21H1/18

    摘要: A method for producing a rotationally symmetrical hollow metal part, particularly a shaft. According to the method, bar-shaped ductile solid material is provided, the solid material is heated from about 300° C. below the forging temperature to the forging temperature, the solid material is transversally spline-rolled until weakenings are created in the core zone (3) of the solid material and the sold material is torn open. Two mandrels (5,6) are forcibly introduced into the center of the bar-shaped solid material during the rolling process, and then one mandrel is retracted while the other mandrel continues advancing so as to produce a tubular part. A transversally spline-rolled rotationally symmetrical hollow part, especially a shaft, which is produced according to noted method can be embodied as a transmission shaft, camshaft, drive shaft, output shaft, starter shaft, hollow shaft, or can be a preform for molded parts and the like.

    摘要翻译: 用于制造旋转对称的中空金属部件,特别是轴的方法。 根据该方法,提供棒状延性固体材料,将固体材料从锻造温度以下的约300℃加热至锻造温度,将固体材料横向花键滚动直至在芯部区域产生弱化 (3)的固体材料和销售的材料被撕开。 两个心轴(5,6)在轧制过程中强制地引入到棒状固体材料的中心,然后一个心轴缩回,而另一个心轴继续前进,以便产生管状部分。 可以将传动轴,凸轮轴,驱动轴,输出轴,起动轴,空心轴等形成为根据所述方法制造的横向花键状的旋转对称的中空部,特别是轴。 零件等。

    TURBOCHARGER
    9.
    发明申请
    TURBOCHARGER 有权
    涡轮增压器

    公开(公告)号:US20100083654A1

    公开(公告)日:2010-04-08

    申请号:US12517441

    申请日:2007-10-23

    IPC分类号: F02D23/00

    摘要: The invention relates to a turbocharger (1) comprising a compressor (2), a turbine connected to the compressor (2) by means of a shaft (3) and provided with an exhaust inlet (5) and an exhaust outlet (7), and a bypass line (6) which branches off from the exhaust inlet (5), bypassing the turbine, and leads to the exhaust outlet in which a boost-pressure regulating flap is arranged, said regulating flap comprising a flap plate (13) which is connected to a flap shaft (14) by means of a connecting device (12).

    摘要翻译: 本发明涉及一种涡轮增压器(1),其包括压缩机(2),通过轴(3)连接到压缩机(2)并且设置有排气入口(5)和排气出口(7)的涡轮机, 和旁路管路(6),其从排气入口(5)分支,绕过涡轮机,并且通向排气出口,其中布置有增压压力调节挡板,所述调节挡板包括挡板(13),所述挡板 通过连接装置(12)连接到翼片轴(14)。