Dual mass flywheel
    3.
    发明授权
    Dual mass flywheel 有权
    双质量飞轮

    公开(公告)号:US09371886B2

    公开(公告)日:2016-06-21

    申请号:US14560901

    申请日:2014-12-04

    发明人: Je Yong Yoon

    摘要: A dual mass flywheel includes a first arcspring and a second arcspring being symmetrically mounted along an inner circumference of a primary cover connected to a crankshaft, a flange being inserted into the primary cover and including a first compressor and a second compressor formed therein, which contact the first arcspring and the second arcspring, respectively, a first stopper and a second stopper configured to support the first arcspring or the second arcspring and being formed on the inner circumference of the primary cover, and a first guide shell and a second guide shell disposed on the inner circumference of the primary cover, guide deformation of the first arcspring or the second arcspring in a radial direction, and including a friction inductor that contacts the first compressor or the second compressor.

    摘要翻译: 双质量飞轮包括第一弧形弹簧和第二弧形弹簧,沿着连接到曲轴的主盖的内圆周对称地安装,凸缘插入主盖中,并且包括形成在其中的第一压缩机和第二压缩机, 所述第一弧形弹簧和所述第二弧形弹簧分别具有第一止动件和第二止动件,所述第一止动器和第二止动器构造成支撑所述第一弧形弹簧或所述第二弧形弹簧并且形成在所述主盖的内周上;以及第一引导壳和第二引导壳, 在主盖的内圆周上,沿径向引导第一弧形弹簧或第二弧形弹簧的变形,并且包括接触第一压缩机或第二压缩机的摩擦感应器。

    DUAL MASS FLYWHEEL
    4.
    发明申请
    DUAL MASS FLYWHEEL 有权
    双色飞甲

    公开(公告)号:US20160084344A1

    公开(公告)日:2016-03-24

    申请号:US14560901

    申请日:2014-12-04

    发明人: Je Yong YOON

    IPC分类号: F16F15/134 F16F15/139

    摘要: A dual mass flywheel includes a first arcspring and a second arcspring being symmetrically mounted along an inner circumference of a primary cover connected to a crankshaft, a flange being inserted into the primary cover and including a first compressor and a second compressor formed therein, which contact the first arcspring and the second arcspring, respectively, a first stopper and a second stopper configured to support the first arcspring or the second arcspring and being formed on the inner circumference of the primary cover, and a first guide shell and a second guide shell disposed on the inner circumference of the primary cover, guide deformation of the first arcspring or the second arcspring in a radial direction, and including a friction inductor that contacts the first compressor or the second compressor.

    摘要翻译: 双质量飞轮包括第一弧形弹簧和第二弧形弹簧,沿着连接到曲轴的主盖的内圆周对称地安装,凸缘插入主盖中,并且包括形成在其中的第一压缩机和第二压缩机, 所述第一弧形弹簧和所述第二弧形弹簧分别具有第一止动件和第二止动件,所述第一止动器和第二止动器构造成支撑所述第一弧形弹簧或所述第二弧形弹簧并且形成在所述主盖的内周上;以及第一引导壳和第二引导壳, 在主盖的内圆周上,沿径向引导第一弧形弹簧或第二弧形弹簧的变形,并且包括接触第一压缩机或第二压缩机的摩擦感应器。

    Flywheel assembly
    5.
    发明授权
    Flywheel assembly 有权
    飞轮总成

    公开(公告)号:US08568243B2

    公开(公告)日:2013-10-29

    申请号:US13059017

    申请日:2009-08-06

    IPC分类号: F16D3/14

    CPC分类号: F16F15/1343 F16F15/13469

    摘要: A first flywheel assembly a first flywheel, a second flywheel, a first spring set, a first spring seat, and a second spring set. The first spring set is arranged between the first flywheel and the second flywheel in a pre-compressed state. The first spring seat is a member that supports an end portion of the first spring set and is pushed in a radially outward direction against the first flywheel. The second spring set is a member having a lower stiffness than a stiffness of the first spring set and is arranged between the second flywheel and the first spring set in a pre-compressed state such that it acts in series with the first spring set.

    摘要翻译: 第一飞轮组件,第一飞轮,第二飞轮,第一弹簧组,第一弹簧座和第二弹簧组。 第一弹簧组以预压缩状态布置在第一飞轮和第二飞轮之间。 第一弹簧座是支撑第一弹簧组件的端部并且朝向第一飞轮沿径向向外的方向推动的构件。 第二弹簧组是具有比第一弹簧组的刚度低的刚度的构件,并且以预压缩状态布置在第二飞轮和第一弹簧组之间,使得其与第一弹簧组串联起来。

    Damper mechanism
    6.
    发明申请
    Damper mechanism 失效
    阻尼机制

    公开(公告)号:US20060009296A1

    公开(公告)日:2006-01-12

    申请号:US11226254

    申请日:2005-09-15

    IPC分类号: F16D3/12

    摘要: A damper mechanism 6 is provided to transmit torque while absorbing and damping torsional vibrations. A small coil spring 45 achieves characteristics of a low rigidity in a small torsion angle region of the torsion characteristics when compressed by rotary members. A coil spring 33 achieves characteristics of a high rigidity in a large torsion angle region of the torsion characteristics when compressed by the rotary members rotating relatively to each other. A frictional resistance generating mechanism 7 generates a frictional resistance while each spring is being compressed. Owing to a rotating-direction space 79, the frictional resistance generating mechanism 7 does not operate in the second stage of the torsion characteristics and also does not in the first stage while a torsion angle is in a predetermined range.

    摘要翻译: 提供阻尼机构6以在吸收和阻尼扭转振动的同时传递扭矩。 当由旋转部件压缩时,小螺旋弹簧45实现扭转特性的小扭转角区域的低刚性特性。 螺旋弹簧33在相对于彼此旋转的旋转构件进行压缩时,在扭转特性的大扭转扭转区域中实现高刚性的特性。 摩擦阻力产生机构7在每个弹簧被压缩时产生摩擦阻力。 由于旋转方向空间79,摩擦阻力产生机构7在扭转特性的第二阶段中不工作,并且在扭转角处于预定范围内也不处于第一阶段。

    Apparatus for damping vibrations
    7.
    发明授权
    Apparatus for damping vibrations 失效
    用于阻尼振动的装置

    公开(公告)号:US06699132B2

    公开(公告)日:2004-03-02

    申请号:US10001773

    申请日:2001-10-31

    IPC分类号: F16D366

    摘要: Apparatus for damping vibrations between the output element of the engine and the power train in a motor vehicle has flywheels which are rotatable relative to each other. One flywheel is mounted on the output element of the engine and the other flywheel is connectable to the power train by a friction clutch. Vibration dampers are installed between the flywheels, and such dampers are confined in a housing which is provided on the one flywheel and contains a supply of viscous fluid medium for the parts of the dampers. The housing is the input element of the dampers and the output member of the dampers is a flange which extends into the housing and is axially movably coupled to the other flywheel. The flywheels rotate with respect to one another and the dampers contain resilient elements which selectively oppose rotation of the flywheels during various stages of rotation. The resilient elements are also arranged not to oppose rotation of the flywheels during an initial stage.

    摘要翻译: 用于减轻发动机的输出元件和机动车辆中的动力传动系之间的振动的装置具有可相对于彼此旋转的飞轮。 一个飞轮安装在发动机的输出元件上,另一个飞轮可通过摩擦离合器连接到动力传动系。 振动阻尼器安装在飞轮之间,并且这种阻尼器被限制在设置在一个飞轮上的壳体中,并且包含用于部件的阻尼器的粘性流体介质。 壳体是阻尼器的输入元件,并且阻尼器的输出构件是延伸到壳体中并且轴向可移动地联接到另一个飞轮的凸缘。 飞轮相对于彼此旋转,并且阻尼器包含弹性元件,其在旋转的各个阶段选择性地对抗飞轮的旋转。 在初始阶段,弹性元件还被布置成不与飞轮的旋转相反。