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    Bicycle front wheel control mechanism
    2.
    发明公开
    Bicycle front wheel control mechanism 失效
    Fahrrad mit Vorderradkontrollmechanismus。

    公开(公告)号：EP0644108A1

    公开(公告)日：1995-03-22

    申请号：EP94306770.2

    申请日：1994-09-15

    申请人： Motobu, Hirotetsu ,  Yoshioka, Koji ,  Kita, Masanobu ,  Kanno, Akira ,  Saiba, Takayoshi

    发明人： Motobu, Hirotetsu, 21, Tsutsui-Iga-Nishi-machi ,  Yoshioka, Koji ,  Kita, Masanobu ,  Kanno, Akira

    IPC分类号： B62K25/04 ,  B62L1/06

    CPC分类号： B62K25/04 ,  B62K2201/02 ,  B62L1/06

    摘要： A bicycle front wheel control mechanism of this invention comprises a suspension system (100) and a brake system (200). The suspension system (100) has an eccentric retainer (10) comprising an axle (22) and two L-shaped members (21), and a shaft portion (23) carried by each housing (10) extends through a respective elastic body (41) at a perpendicularly upper part of the axle. The suspension system (100) is so designed that it makes possible rocking motion relative to the front wheel and around the axis of the shaft portion (23) with the distance between the shaft portion (23) and the axle (21) as its radius, within a range of specified limited rocking angles, and the brake system (200) is so designed that a side surface of its rim (62) is made wide in a radial direction and the side surface (62a) is approximately perpendicular. Since this invention is made by inventing a principle of a new suspension system having the simplest structure, the lightest weight and the smallest cost and can improve properties of running and braking.

    摘要翻译： 本发明的自行车前轮控制机构包括悬架系统（100）和制动系统（200）。 悬挂系统（100）具有包括轴（22）和两个L形构件（21）的偏心保持器（10），并且由每个壳体（10）承载的轴部分（23）延伸穿过相应的弹性体 41）在轴的垂直上部。 悬挂系统（100）被设计成使得相对于前轮和围绕轴部（23）的轴线的摆动运动使得轴部（23）和轴（21）之间的距离作为其半径 在规定的有限摆动角度的范围内，并且制动系统（200）被设计成使得其轮辋（62）的侧表面在径向方向上变宽并且侧表面（62a）近似垂直。 由于本发明是通过发明具有最简单的结构，最轻的重量和最小的成本的新的悬架系统的原理来实现的，并且可以改善运行和制动的性能。

    AIRCRAFT WHEEL SUPPORT MECHANISM
    4.
    发明公开
    AIRCRAFT WHEEL SUPPORT MECHANISM 审中-公开
    飞机轮支撑机构

    公开(公告)号：EP1424279A1

    公开(公告)日：2004-06-02

    申请号：EP02758884.7

    申请日：2002-09-05

    申请人： Yoshioka, Koji ,  Aruze Corp.

    发明人： YOSHIOKA, Koji

    IPC分类号： B64C25/58

    CPC分类号： B64C25/60 ,  B64C25/001 ,  B64C25/10 ,  B64C2025/008

    摘要： An aircraft wheel support mechanism capable of reducing the impact to the tire at the time of landing and capable of reducing the impact to the tire at the time of the wheel colliding with an obstacle lying on the runway. The mechanism comprises a suspension mechanism (3) for rotatably supporting a wheel (13) by the lower end of a support member (2) connected to the fuselage, the suspension mechanism (3) having a crank shaft assembly (5), and is characterized in that the crank shaft assembly comprises a horizontal support shaft (51) rotatably supported by the lower end of the support member, an axle (52) for rotatably supporting the wheel, and an arm (53) positioned at right angles with the horizontal support shaft and axle for connecting one end of the horizontal support shaft to one end of the axle.

    摘要翻译： 一种飞机轮支撑机构，其能够降低着陆时对轮胎的冲击，并且能够减少在轮子与跑道上的障碍物碰撞时对轮胎的冲击。 该机构包括用于通过连接到机身的支撑构件（2）的下端可旋转地支撑车轮（13）的悬架机构（3），悬架机构（3）具有曲轴组件（5），并且 其特征在于，所述曲轴组件包括由所述支撑构件的下端可旋转地支撑的水平支撑轴（51），用于可旋转地支撑所述轮子的轴（52）和与所述水平轴成直角布置的臂（53） 支撑轴和轴，用于将水平支撑轴的一端连接到轴的一端。