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    • 7. 发明授权
    • Hinge actuator for wing mirror of motor vehicle
    • 机动车后视镜铰链执行机构
    • US06926414B2
    • 2005-08-09
    • US10451528
    • 2001-12-17
    • Paulus Gerardus Maria Van Stiphout
    • Paulus Gerardus Maria Van Stiphout
    • B60R1/074G02B5/08G02B7/18
    • B60R1/074Y10S248/90
    • A hinge actuator for a wing mirror of motor vehicle, which is operative between an extreme fold-in position and an extreme fold-out position and between the extreme fold-out position and an extreme fold-over position, comprising a mirror base, provided with a frame with a frame part which extends around a base shaft and supported on a base flange. A first cam track located between the base shaft and the frame part, with at least one bearing element, is present, and a first elastic element extending on a side along this track. During a rotation of the frame relative to the base shaft between the extreme fold-in position and the extreme fold-out position, the first elastic element contact with the bearing element undergoes a deformation, while during a rotation between the extreme fold-out position and the extreme fold-over position, the first elastic element undergoes a further-going deformation.
    • 一种用于机动车辆的机翼的铰链致动器,其在极端折叠位置和极端折叠位置之间以及在极端折叠位置和极端折叠位置之间操作,包括镜底座 具有框架,框架部分围绕基轴延伸并且支撑在基部凸缘上。 存在位于基轴和框架部分之间的第一凸轮轨道,具有至少一个轴承元件,以及沿着该轨道在一侧延伸的第一弹性元件。 在框架相对于基本轴在极端折叠位置和极端折叠位置之间旋转期间,与轴承元件接触的第一弹性元件经历变形,同时在极端折叠位置 和极端折叠位置,第一弹性元件进一步变形。
    • 9. 发明授权
    • Fastening construction, in particular for a wing mirror of a motor vehicle
    • 紧固结构,特别是机动车辆的后视镜
    • US07546997B2
    • 2009-06-16
    • US10493167
    • 2002-10-30
    • Paulus Gerardus Maria Van Stiphout
    • Paulus Gerardus Maria Van Stiphout
    • A47B97/04
    • B60R1/076
    • A fastening construction, in particular for a wing mirror unit of a motor vehicle, comprising a base part (1) which can be fixedly connected with a vehicle, and a rotation part (3) which is arranged to be coupled with the base part (1) and which in coupled condition constitutes a central shaft for pivotally bearing-mounting a wing mirror unit. The base part (1) and the rotation part (3) are provided with at least one projection and groove pair (19, 20) cooperating as a bayonet catch, such that the rotation part (3) can be displaced towards the base part (1) and that when the projection and groove pair are in engagement, the rotation part (3) is pivotable about the geometric axis (2), and, after passing an intermediate angular position (13), through cooperation of the projection and groove pair (19, 20), the rotation part (3) is locked relative to the base part (1), axially along the geometric axis (2). The rotation part (3) and the base part (1) are further provided with blocking means (4, 6) which in a second angular position (5b) restrain the rotation part (3) from rotation relative to the base part (1) about the geometric axis (2).
    • 一种紧固结构,特别是用于机动车辆的机翼反射镜单元,包括可与车辆固定连接的基座部分(1)和设置成与基座部件 1),并且在耦合状态下构成用于枢转地支承机翼反射镜单元的中心轴。 基部(1)和旋转部分(3)设置有至少一个突出和凹槽对(19,20),其配合为卡口卡扣,使得旋转部分(3)能够朝向基部 1),并且当突起和凹槽对啮合时,旋转部分(3)绕几何轴线(2)枢转,并且在通过中间角位置(13)之后,通过突出和凹槽对的配合 (19,20),所述旋转部(3)相对于所述基部(1)沿着所述几何轴线(2)轴向地被锁定。 旋转部分(3)和基部部分(1)还设置有阻挡装置(4,6),其在第二角位置(5b)中限制旋转部分(3)相对于基部部分(1)旋转, 围绕几何轴(2)。