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    DEPLOYABLE ANTENNA
    2.
    发明申请
    DEPLOYABLE ANTENNA 有权
    可配天线

    公开(公告)号：US20120193498A1

    公开(公告)日：2012-08-02

    申请号：US13361234

    申请日：2012-01-30

    Applicant: Minoru TABATA ,  Kiyoshi FUJII ,  Kyoji SHINTATE ,  Satoru OZAWA

    Inventor： Minoru TABATA ,  Kiyoshi FUJII ,  Kyoji SHINTATE ,  Satoru OZAWA

    IPC: H01Q1/08

    CPC classification number: H01Q15/161 ,  H01Q1/288

    Abstract: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.

    Abstract translation: 一种可展开的天线，其具有通过设置在至少三个级中的四侧链路具有较大孔径的直径，并且包括：从中心轴径向布置的六个展开连杆机构（20），以支撑柔性反射镜的外缘部分 表面; 以及布置在六个部署链接机构的布置中心的下部的一个部署驱动机构（30），用于展开六个部署链接机构。 六个展开连杆机构中的每一个包括从中心轴的位置起依次布置的第一四侧连杆（5），第二四侧连杆（6）和第三四侧连杆（7） 六个部署链接机构围绕着六个部署链接机构排列，朝向六个部署链接机构中的每一个的外侧，使得六个部署链接机构中的每一个被构造成可分三个阶段折叠。

    DEPLOYABLE ANTENNA REFLECTOR
    4.
    发明申请
    DEPLOYABLE ANTENNA REFLECTOR 有权
    可配置的天线反射器

    公开(公告)号：US20130207881A1

    公开(公告)日：2013-08-15

    申请号：US13763148

    申请日：2013-02-08

    Applicant: Kiyoshi FUJII ,  Minoru TABATA ,  Kyoji SHINTATE

    Inventor： Kiyoshi FUJII ,  Minoru TABATA ,  Kyoji SHINTATE

    IPC: H01Q15/14

    CPC classification number: H01Q15/147 ,  H01Q1/288 ,  H01Q15/161 ,  H01Q15/168 ,  H01Q15/20

    Abstract: A deployable antenna reflector includes a surface cable network formed of a plurality of cables coupled to each other in a mesh pattern. The surface cable network includes at least one rigid rod member that reduces a maximum tensile force caused in the surface cable network.

    Abstract translation: 可部署的天线反射器包括由网格图案彼此耦合的多个电缆形成的表面电缆网络。 表面电缆网络包括至少一个刚性杆构件，其减小了表面电缆网络中引起的最大张力。

    ELECTRIC PARKING BRAKE DEVICE
    5.
    发明申请
    ELECTRIC PARKING BRAKE DEVICE 有权
    电动停车制动装置

    公开(公告)号：US20120247895A1

    公开(公告)日：2012-10-04

    申请号：US13432700

    申请日：2012-03-28

    Applicant: Keiichi Tsurumi ,  Hideyuki Kai ,  Mitsuyasu Mizuno ,  Eiji Inaya ,  Jin Yamada ,  Hisashi Kobayashi ,  Minoru Tabata ,  Kazuhiro Suzuki

    Inventor： Keiichi Tsurumi ,  Hideyuki Kai ,  Mitsuyasu Mizuno ,  Eiji Inaya ,  Jin Yamada ,  Hisashi Kobayashi ,  Minoru Tabata ,  Kazuhiro Suzuki

    IPC: F16D51/18 ,  F16D51/20

    CPC classification number: F16D65/22 ,  B60T13/741 ,  F16D51/22 ,  F16D2121/24 ,  F16D2125/40

    Abstract: In the interior of a brake drum, the arrangement space in the rotational axis direction of the brake drum is spacious in comparison with that in the direction orthogonal to the rotational axis direction in which an anchor portion, hub components on the vehicle body side and the like are arranged. An electric parking brake device is provided with the anchor portion that supports respective one ends of brake shoes. A parking lever is pivotally moved by a drive unit operated by an electric motor for pushing the brake shoes toward the brake drum. The anchor portion and the drive unit are arranged to be piled up in the rotational axis direction of the brake drum which is spacious in comparison with the direction orthogonal to the rotational axis direction.

    Abstract translation: 在制动鼓的内部，制动鼓的旋转轴方向的配置空间与在与车体侧的主体部，轮毂部和车身侧的旋转轴方向正交的方向相比较宽， 喜欢安排。 一种电动驻车制动装置，其具有支撑制动蹄相应一端的固定部。 驻车杆由用于将制动蹄推向制动鼓的电动机操作的驱动单元枢转地移动。 锚定部和驱动单元相对于与旋转轴方向正交的方向，与制动鼓的旋转轴方向相比，被构成为宽敞。

    Deployable antenna
    6.
    发明授权
    Deployable antenna 有权
    可部署天线

    公开(公告)号：US08922456B2

    公开(公告)日：2014-12-30

    申请号：US13361234

    申请日：2012-01-30

    Applicant: Minoru Tabata ,  Kiyoshi Fujii ,  Kyoji Shintate ,  Satoru Ozawa

    Inventor： Minoru Tabata ,  Kiyoshi Fujii ,  Kyoji Shintate ,  Satoru Ozawa

    IPC: H01Q15/20 ,  H01Q1/12 ,  H01Q15/16 ,  H01Q1/28

    CPC classification number: H01Q15/161 ,  H01Q1/288

    Abstract: A deployable antenna which has a larger aperture diameter by four-side links provided in at least three stages and which includes: six deployment link mechanisms (20) arranged radially from a central shaft so as to support an outer edge portion of a flexible reflector mirror surface; and one deployment driving mechanism (30) arranged at a lower portion of a center of arrangement of the six deployment link mechanisms, for unfolding the six deployment link mechanisms. Each of the six deployment link mechanisms includes a first four-side link (5), a second four-side link (6), and a third four-side link (7) arranged in an order from a position of the central shaft, around which the six deployment link mechanisms are arranged, toward an outer side of the each of the six deployment link mechanisms so that the each of the six deployment link mechanisms is structured to be foldable in three stages.

    Abstract translation: 一种可展开的天线，其具有通过设置在至少三个级中的四侧链路具有较大孔径的直径，并且包括：从中心轴径向布置的六个展开连杆机构（20），以支撑柔性反射镜的外缘部分 表面; 以及布置在六个部署链接机构的布置中心的下部的一个部署驱动机构（30），用于展开六个部署链接机构。 六个展开连杆机构中的每一个包括从中心轴的位置起依次布置的第一四侧连杆（5），第二四侧连杆（6）和第三四侧连杆（7） 六个部署链接机构围绕着六个部署链接机构排列，朝向六个部署链接机构中的每一个的外侧，使得六个部署链接机构中的每一个被构造成可分三个阶段折叠。

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