RETRACTABLE DEPLOYABLE STRUCTURE USING A TAPE SPRING
    1.
    发明申请
    RETRACTABLE DEPLOYABLE STRUCTURE USING A TAPE SPRING 有权
    可拆卸的可拆卸结构使用带状弹簧

    公开(公告)号:US20160144984A1

    公开(公告)日:2016-05-26

    申请号:US14945273

    申请日:2015-11-18

    Applicant: THALES

    CPC classification number: B64G1/222 B64G1/44 B64G1/503 B64G1/66 B65H75/364

    Abstract: A deployable structure comprises: a mount comprising a first point and a second point opposite and a third point, a storage reel able to rotate about an axis Z, a tape spring able to switch from a configuration in which it is wound about the axis Z in the storage reel into a configuration in which it is deployed along an axis X substantially perpendicular to the axis Z, the first and second points forming a double support with the tape spring to keep the tape spring in the deployed configuration. The third point is able to form a simple support with the tape spring, the storage reel is able to move with respect to the third point and the storage reel is pressed against the third point to guide the deployment of the tape spring.

    Abstract translation: 可部署结构包括:安装件,其包括第一点和相对的第二点,第三点,能够围绕轴线Z旋转的存储卷轴,能够绕其围绕轴线Z缠绕的构造切换的带弹簧 在存储卷轴中,其沿着基本上垂直于轴线Z的轴线X展开的构造,第一和第二点与带弹簧形成双重支撑,以将带弹簧保持在展开构型中。 第三点能够用带​​状弹簧形成简单的支撑,存储卷轴能够相对于第三点移动,并且存储卷轴被压靠在第三点上以引导带弹簧的展开。

    AUTONOMOUS SPONTANEOUS DEPLOYMENT DEPLOYABLE MAST AND SATELLITE INCLUDING AT LEAST ONE SUCH MAST
    2.
    发明申请
    AUTONOMOUS SPONTANEOUS DEPLOYMENT DEPLOYABLE MAST AND SATELLITE INCLUDING AT LEAST ONE SUCH MAST 有权
    自动自动部署可部署的MAST和卫星,包括至少一个这样的MAST

    公开(公告)号:US20140291451A1

    公开(公告)日:2014-10-02

    申请号:US14223658

    申请日:2014-03-24

    Applicant: THALES

    CPC classification number: B64G1/222 B64G1/66 B64G2001/1092

    Abstract: An autonomous spontaneous deployment deployable mast includes at least one elementary structural unit having a longitudinal deployment axis X and two platforms parallel to a plane YZ orthogonal to the axis X. The elementary structural unit includes N stages stacked above one another parallel to the longitudinal deployment axis X, where N is greater than 1. Each stage includes at least three longitudinal flexible tape-springs, the N stages being fixed to one another two by two by means of connecting platforms parallel to the plane YZ and two contiguous lower and upper stages being offset angularly relative to each other by rotation about the deployment axis X, the tape-springs of the lower stage being interleaved between the tape-springs of the upper stage.

    Abstract translation: 自主自发展开的桅杆包括具有纵向展开轴线X和平行于与轴线X正交的平面YZ的两个平台的至少一个基本结构单元。基本结构单元包括平行于纵向展开轴线 X,其中N大于1.每个阶段包括至少三个纵向柔性带弹簧,N个阶段通过平行于平面YZ的连接平台彼此两个彼此固定,并且两个连续的下部和上部阶段是 通过围绕展开轴线X的旋转而相对于彼此成角度地偏移,下层的带 - 弹簧交错在上层的带 - 弹簧之间。

    DEPLOYABLE MAST WITH SPONTANEOUS AUTONOMOUS DEPLOYMENT, AND SATELLITE COMPRISING AT LEAST ONE MAST OF THIS TYPE
    3.
    发明申请
    DEPLOYABLE MAST WITH SPONTANEOUS AUTONOMOUS DEPLOYMENT, AND SATELLITE COMPRISING AT LEAST ONE MAST OF THIS TYPE 有权
    具有自动自动部署的可配置的弹药,以及包含该类型的至少一个的卫星

    公开(公告)号:US20160068281A1

    公开(公告)日:2016-03-10

    申请号:US14846242

    申请日:2015-09-04

    Applicant: THALES

    CPC classification number: B64G1/222 H01Q1/1235

    Abstract: A deployable mast with spontaneous autonomous deployment comprises at least one elementary structural block with a longitudinal axis of deployment X, the elementary structural block comprising two, respectively lower and upper platforms parallel to a plane YZ orthogonal to axis X, and N stages stacked on one another parallel to axis X, where N is more than 1, and where i is between 1 and N−1. Each stage comprises at least six flexible longitudinal connection arms which are articulated by tape springs, which arms are, in the deployed position, on planes parallel to axis X and are inclined relative to axis X, the N stages being secured to one another in pairs by means of connection platforms parallel to the plane YZ; two adjacent lower and upper stages are offset angularly relative to one another by rotation around the axis of deployment X.

    Abstract translation: 具有自发自主部署的可展开的桅杆包括至少一个具有展开X的纵向轴线的基本结构块,所述基本结构块包括平行于与轴线X正交的平面YZ的平行于平面YZ的两个分别的下平台和上平台,以及堆叠在一个上的N个平台 另一个平行于X轴,其中N大于1,其中i在1和N-1之间。 每个阶段包括至少六个柔性的纵向连接臂,其通过带状弹簧铰接,该臂在展开位置处在平行于轴线X的平面上并且相对于轴线X倾斜,N个阶段彼此成对地固定 通过平行于YZ平面的连接平台; 两个相邻的下级和上级通过围绕部署X的轴线的旋转相对于彼此成角度地偏移。

    TAPE SPRING DEPLOYABLE STRUCTURE
    4.
    发明申请
    TAPE SPRING DEPLOYABLE STRUCTURE 有权
    TAPE弹簧可配置结构

    公开(公告)号:US20160023781A1

    公开(公告)日:2016-01-28

    申请号:US14805317

    申请日:2015-07-21

    Applicant: THALES

    Abstract: A deployable structure comprises: a support, a tape spring fixed to the support, able to pass from a wound configuration wound about an axis Z, to a deployed configuration, and a mobile arm able to rotate with respect to the support about the Z-axis, able to form a first contact with the tape spring so as to control the deployment of the tape spring.

    Abstract translation: 可展开的结构包括:支撑件,固定到支撑件上的带弹簧,能够绕绕Z轴缠绕的缠绕构型穿过到展开构型,以及能够相对于支撑件围绕Z轴旋转的移动臂, 能够与带状弹簧形成第一接触,从而控制带状弹簧的展开。

    DEPLOYMENT AND AIMING DEVICE
    5.
    发明申请

    公开(公告)号:US20170253352A1

    公开(公告)日:2017-09-07

    申请号:US15443932

    申请日:2017-02-27

    Applicant: THALES

    Abstract: A deployment and aiming device of an instrument comprises: a first support, a second support to receive the instrument, N mandrels, N being an integer number greater than or equal to 1, positioned around the first support, each of the N mandrels rotationally mobile relative to the first support about a mandrel axis ZN intersecting the mandrel, N linear elements, each of the N linear elements cooperating with one of the N mandrels, each of the N linear elements having first and second ends, wherein the first end of the N linear elements is fixed in the mandrel with which it cooperates at a fixing point, wherein the second end of the N linear elements is linked to the second support, such that a rotation of the mandrel about its axis ZN generates a displacement of the fixing point.

    TAPE WITH SMOOTH DEPLOYMENT
    6.
    发明申请
    TAPE WITH SMOOTH DEPLOYMENT 审中-公开
    带平滑部分的胶带

    公开(公告)号:US20160185073A1

    公开(公告)日:2016-06-30

    申请号:US14980014

    申请日:2015-12-28

    Abstract: A tape having a fully wound stable state and a fully unwound stable state, configured for space applications, the intermediate states between the fully wound state and the fully unwound state comprises a single continuous portion of wound tape with a first radius of curvature greater than a threshold value and a single continuous portion of unwound tape with a second radius of curvature less than the threshold value, the value of the second radius of curvature being continuous over the unwound portio; the tape comprises a stack comprising fibrous layers extending in a longitudinal direction, the resulting stack having symmetry with respect to a longitudinal plane of its fibres to compensate for torsional deformations generated by variations in temperature.

    Abstract translation: 具有完全卷绕的稳定状态和完全展开的稳定状态的带,被配置用于空间应用,完全卷绕状态和完全展开状态之间的中间状态包括具有大于第一曲率半径的第一曲率半径的卷绕带的单个连续部分 阈值和具有小于阈值的第二曲率半径的展开带的单个连续部分,所述第二曲率半径的值在所述退绕端口上连续; 胶带包括包括沿纵向方向延伸的纤维层的堆叠,所得到的叠层相对于其纤维的纵向平面具有对称性,以补偿由温度变化产生的扭转变形。

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