Seat belt apparatus of a vehicle
    111.
    发明授权
    Seat belt apparatus of a vehicle 失效
    车辆安全带装置

    公开(公告)号:US4667980A

    公开(公告)日:1987-05-26

    申请号:US703675

    申请日:1985-02-20

    申请人: Kazuo Yamamoto

    发明人: Kazuo Yamamoto

    摘要: A three-point type seat belt apparatus is characterized in that the free end side of webbing is supported for movement in the longitudinal direction of a vehicle and the free end side of the webbing is driven in response to the tilting movement of the seat back of a seat.

    摘要翻译: 一种三点式座椅安全带装置,其特征在于,所述织带的自由端侧被支撑以沿车辆的纵向方向运动,并且所述织带的自由端侧响应于座椅靠背的倾斜运动而被驱动 座位。

    Automatic seat belt driving device
    112.
    发明授权
    Automatic seat belt driving device 失效
    自动安全带驱动装置

    公开(公告)号:US4564218A

    公开(公告)日:1986-01-14

    申请号:US601003

    申请日:1984-04-16

    IPC分类号: B60R22/06 G03F1/00

    CPC分类号: B60R22/06

    摘要: In a driving device for moving an automatic seat belt between a seat occupant restraining position and a seat occupant liberating position, a rotatable member to which one end of an elongate drive member is attached and by which the drive member is taken up or pushed out is formed with a portion for containing the drive member therein, and the drive member is guided from the portion to an exit lying at a position deviated in the direction of the rotational axis of the rotatable member and is pushed out from the exit.

    摘要翻译: 在用于在座椅乘员约束位置和乘坐者释放位置之间移动自动安全带的驱动装置中,安装有细长驱动构件的一端并​​且驱动构件通过该旋转构件被卷取或推出的可旋转构件是 形成有用于将驱动构件容纳在其中的部分,并且驱动构件从该部分被引导到位于沿可旋转构件的旋转轴线的方向偏离的位置处,并从出口被推出。

    Buckle assembly for seat belt
    114.
    发明授权
    Buckle assembly for seat belt 失效
    安全带带扣组合

    公开(公告)号:US4228567A

    公开(公告)日:1980-10-21

    申请号:US941164

    申请日:1978-09-11

    IPC分类号: A44B11/25 A44B11/26

    摘要: A buckle assembly for seat belt comprises cover means consisting of a first and a second cover member forming a tongue insertion opening and a hollow chamber connected to the opening. The first cover member has a push button operating opening connected to the hollow chamber. A latch means including a plurality of members is disposed within the cover means and capable of taking up two positions, i.e. tongue locking position and non-locking position. The members comprising the latch means are a base member having a tongue guide path contiguous to the tongue insertion opening and extending in the direction in which the tongue is to be inserted, the base member having guide means formed transversely of the direction in which the tongue is inserted, a latch member having a first portion and a second portion and slidably disposed in the guide means of the base member, the first portion adapted to contact the tongue when inserted and slide the latch member in the guide slot to permit insertion of the tongue, the second portion being for restraining the tongue in its locked position, and bias means disposed in the second cover member and biasing the latch member into its tongue locking position. In assembling the buckle assembly the members of the latch means are serially disposed in a half hollow chamber of the second cover in order to be assembled. A push button for operating the latch member is provided in the first cover member and engaged with the latch member.

    摘要翻译: 用于安全带的带扣组件包括由第一和第二盖构件组成的盖装置,第一和第二盖构件形成舌插入口和连接到开口的中空室。 第一盖构件具有连接到中空室的按钮操作开口。 包括多个构件的闩锁装置设置在盖装置内并且能够占据两个位置,即舌锁定位置和非锁定位置。 包括闩锁装置的构件是基部构件,其具有与舌片插入口相邻并且沿舌片插入方向延伸的舌片引导路径,基部构件具有横向于舌部的方向形成的导向装置, 插入的闩锁构件,具有第一部分和第二部分并且可滑动地设置在基部构件的引导装置中的闩锁构件,第一部分在插入时适于接触舌头,并将闩锁构件滑动在引导狭槽中,以允许插入 舌部,第二部分用于将舌片限制在其锁定位置,以及偏置装置,其设置在第二盖构件中并将闩锁构件偏压到其舌锁定位置。 在组装带扣组件时,闩锁装置的构件被串联地布置在第二盖的半空心腔中以便被组装。 用于操作闩锁构件的按钮设置在第一盖构件中并与闩锁构件接合。

    Cap, fastening structure using the same, and aircraft including the fastening structure
    116.
    发明授权
    Cap, fastening structure using the same, and aircraft including the fastening structure 有权
    盖,使用其的紧固结构,以及包括紧固结构的飞机

    公开(公告)号:US09108743B2

    公开(公告)日:2015-08-18

    申请号:US13583332

    申请日:2011-03-22

    IPC分类号: B64D45/02 F16B37/14

    CPC分类号: B64D45/02 F16B37/14

    摘要: A cap capable of achieving enhanced safety by inhibiting the occurrence of sparks thereinside even if a lightning current has flowed through a fastener, a fastening structure using the same, and an aircraft including the fastening structure. The cap (27) is attached so as to cover a portion of a fastener (15) that couples an upper skin (3) of an aircraft and a stringer (11) located inside the upper skin. The covered portion projects through the stringer (11). An outer surface (33) of the cap that comes into contact with an interior space of the upper skin (3) is a curved surface, and the cap is made of a conductive material.

    摘要翻译: 即使雷电流已经通过紧固件,使用其的紧固结构,也包括紧固结构的飞行器,能够通过抑制其内部的火花的发生来实现增强的安全性。 帽(27)被附接以覆盖联接飞机的上部皮肤(3)和位于上部皮肤内部的纵梁(11)的紧固件(15)的一部分。 覆盖部分通过桁条(11)突出。 与上皮肤(3)的内部空间接触的帽的外表面(33)是弯曲表面,帽由导电材料制成。

    Spring guide and cushion device
    117.
    发明授权
    Spring guide and cushion device 有权
    弹簧导轨和缓冲装置

    公开(公告)号:US08740198B2

    公开(公告)日:2014-06-03

    申请号:US13028141

    申请日:2011-02-15

    IPC分类号: F16F1/06

    摘要: A spring guide is provided between a coil spring and a cylindrical outer shaft member. The coil spring coaxially houses therein a shaft portion of a damper set in which an inner shaft member is fitted in the outer shaft member slidably in an axial direction of the spring guide. The spring guide includes a barrel, at least one first projecting portion, and at least one second projecting portion. The barrel has a substantially cylindrical shape and includes a first end portion and a second end portion opposite to the first end portion in the axial direction. The at least one first projecting portion is provided at the first end portion of the barrel to project toward an axis of the barrel. The at least one second projecting portion is provided at the second end portion of the barrel to project toward the axis of the barrel.

    摘要翻译: 弹簧导向件设置在螺旋弹簧和圆柱形外轴构件之间。 螺旋弹簧同轴地容纳阻尼器组件的轴部,其中内轴构件沿弹簧引导件的轴向方向可滑动地装配在外轴构件中。 弹簧引导件包括筒体,至少一个第一突出部分和至少一个第二突出部分。 枪管具有大致圆柱形形状,并且包括在轴向方向上与第一端部相对的第一端部和第二端部。 至少一个第一突出部分设置在筒的第一端部处以朝向筒的轴线突出。 至少一个第二突出部分设置在筒的第二端部处以朝向筒的轴线突出。

    Circular accelerator and operating method therefor
    118.
    发明授权
    Circular accelerator and operating method therefor 有权
    圆形加速器及其操作方法

    公开(公告)号:US08525448B2

    公开(公告)日:2013-09-03

    申请号:US13368435

    申请日:2012-02-08

    IPC分类号: H05H13/00

    CPC分类号: H05H13/005 H05H7/12 H05H13/02

    摘要: The circular accelerator comprises: a bending electromagnet that generates a bending magnetic field; a radio-frequency power source that generates a radio-frequency electric field in accordance with an orbital frequency of charged particles; a radio-frequency electromagnetic field coupling part connected to the radio-frequency power source; an acceleration electrode connected to the radio-frequency electromagnetic field coupling part; and an acceleration-electrode-opposing ground plate provided to form an acceleration gap between the plate itself and the acceleration electrode, for generating the radio-frequency electromagnetic field in an orbiting direction of the charged particles; wherein the bending electromagnet generates the bending magnetic field varying in such a way that the orbital frequency of the charged particles varies in a variation range of 0.7% to 24.7% with respect to an orbital frequency at the charged-particles' extraction portion, during a time of injection to extraction of the particles.

    摘要翻译: 圆形加速器包括:产生弯曲磁场的弯曲电磁体; 射频电源,其根据带电粒子的轨道频率产生射频电场; 连接到所述射频电源的射频电磁场耦合部; 连接到射频电磁场耦合部分的加速电极; 以及加速电极对置的接地板,其设置成在板本身和加速电极之间形成加速间隙,用于在带电粒子的运动方向上产生射频电磁场; 其中所述弯曲电磁体产生所述弯曲磁场,所述弯曲磁场以使得所述带电粒子的轨道频率相对于所述带电粒子提取部分的轨道频率在0.7%至24.7%的变化范围内变化的方式变化, 注射时间来提取颗粒。

    CAP, FASTENING STRUCTURE USING THE SAME, AND AIRCRAFT INCLUDING THE FASTENING STRUCTURE
    119.
    发明申请
    CAP, FASTENING STRUCTURE USING THE SAME, AND AIRCRAFT INCLUDING THE FASTENING STRUCTURE 有权
    CAP,使用相同的快速结构,以及包括快速结构的飞机

    公开(公告)号:US20130043351A1

    公开(公告)日:2013-02-21

    申请号:US13583332

    申请日:2011-03-22

    IPC分类号: B64D45/02 B64C1/12

    CPC分类号: B64D45/02 F16B37/14

    摘要: There is provided a cap capable of achieving enhanced safety by inhibiting the occurrence of sparks thereinside even if a lightning current has flowed through a fastener, a fastening structure using the same, and an aircraft including the fastening structure. A cap (27) according to the present invention is attached so as to cover a portion of a fastener (15) that couples an upper skin (3) of an aircraft and a stringer (11) located inside the upper skin (3), the portion projecting through the stringer (11), wherein an outer surface (33) of the cap that comes into contact with an interior space of the upper skin (3) is a curved surface, and the cap is made of a conductive material.

    摘要翻译: 即使雷电流已经通过紧固件,使用该紧固件的紧固结构,也包括紧固结构的飞行器,提供了能够通过抑制其内部火花发生而实现增强的安全性的盖。 根据本发明的盖(27)被附接以覆盖联接飞行器的上皮肤(3)和位于上皮肤(3)内的纵梁(11)的紧固件(15)的一部分, 所述突出部分穿过所述纵梁(11),其中与所述上皮肤(3)的内部空间接触的所述盖的外表面(33)是曲面,并且所述盖由导电材料制成。

    SPRING GUIDE AND CUSHION DEVICE
    120.
    发明申请
    SPRING GUIDE AND CUSHION DEVICE 有权
    弹簧导杆和垫圈装置

    公开(公告)号:US20110204551A1

    公开(公告)日:2011-08-25

    申请号:US13028141

    申请日:2011-02-15

    IPC分类号: B60G15/06 F16F1/12 F16F13/00

    摘要: A spring guide is provided between a coil spring and a cylindrical outer shaft member. The coil spring coaxially houses therein a shaft portion of a damper set in which an inner shaft member is fitted in the outer shaft member slidably in an axial direction of the spring guide. The spring guide includes a barrel, at least one first projecting portion, and at least one second projecting portion. The barrel has a substantially cylindrical shape and includes a first end portion and a second end portion opposite to the first end portion in the axial direction. The at least one first projecting portion is provided at the first end portion of the barrel to project toward an axis of the barrel. The at least one second projecting portion is provided at the second end portion of the barrel to project toward the axis of the barrel.

    摘要翻译: 弹簧导向件设置在螺旋弹簧和圆柱形外轴构件之间。 螺旋弹簧同轴地容纳阻尼器组件的轴部,其中内轴构件沿弹簧引导件的轴向方向可滑动地装配在外轴构件中。 弹簧引导件包括筒体,至少一个第一突出部分和至少一个第二突出部分。 枪管具有大致圆柱形形状,并且包括在轴向方向上与第一端部相对的第一端部和第二端部。 至少一个第一突出部分设置在筒的第一端部处以朝向筒的轴线突出。 至少一个第二突出部分设置在筒的第二端部处以朝向筒的轴线突出。