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    Foldable self-erecting joint
    2.
    发明授权
    Foldable self-erecting joint 失效
    可折叠自立式接头

    公开(公告)号：US4615637A

    公开(公告)日：1986-10-07

    申请号：US588039

    申请日：1984-03-09

    申请人： Timothy E. Pelischek

    发明人： Timothy E. Pelischek

    IPC分类号： B64G1/22 ,  B64G1/44 ,  F16C11/04

    CPC分类号： F16C11/04 ,  B64G1/222 ,  B64G1/44 ,  Y10T16/53843 ,  Y10T16/5476 ,  Y10T403/32271 ,  Y10T403/32409 ,  Y10T403/32606 ,  Y10T403/32827 ,  Y10T403/32967

    摘要： A self-erecting joint for a pair of hinged, tubular members in which the hinging is located at corresponding portions of the members and the opposite edge portions are connected by spring-biased toggle links which in the unfolded position of the members are nested against one of the members in substantial alignment and over-center for securely locking the joint in the unfolded condition.

    摘要翻译： 用于一对铰接的管状构件的自立式接头，其中铰链位于构件和相对边缘部分的对应部分处的连接件通过弹簧偏置的肘节连接件连接，在构件的未展开位置嵌套在一起 的构件基本对准和中心，以将接头牢固地锁定在展开状态。

    Orbiter escape pole
    3.
    发明授权
    Orbiter escape pole 失效
    轨道器逃生杆

    公开(公告)号：US4887780A

    公开(公告)日：1989-12-19

    申请号：US292046

    申请日：1988-12-30

    申请人： Winston D. Goodrich ,  Clarence J. Wesselski ,  Timothy E. Pelischek ,  Bruce H. Becker ,  Jon B. Kahn ,  Margaret E. Grimaldi ,  John P. McManamen ,  Edgar O. Castro

    发明人： Winston D. Goodrich ,  Clarence J. Wesselski ,  Timothy E. Pelischek ,  Bruce H. Becker ,  Jon B. Kahn ,  Margaret E. Grimaldi ,  John P. McManamen ,  Edgar O. Castro

    IPC分类号： B64G1/14 ,  B64G1/52

    CPC分类号： B64G1/52 ,  B64G1/14 ,  Y10S244/905

    摘要： A Shuttle type of aircraft (10) with an escape hatch (12) has an arcuately shaped pole housing (16) attachable to an interior wall and ceiling with its open end adjacent to the escape hatch. The pole housing 16 contains a telescopically arranged and arcuately shaped primary pole member (22) and extension pole member (23) which are guided by roller assemblies (30,35). The extension pole member (23) is slidable and extendable relative to the primary pole member (22). For actuation, a spring actuated system includes a spring (52) in the pole housing. A locking member (90) engages both pole members (22,23) through notch portions (85,86) in the pole members. The locking member selectively releases the extension pole member (23) and the primary pole member (22). An internal one-way clutch or anti-return mechanism prevents retraction of the extension pole member from an extended position. Shock absorbers (54)(150,152) are for absoring the energy of the springs.A manual backup deployment system is provided which includes a canted ring (104) biased by a spring member (108). A lever member (100) with a slot and pin connection (102) permits the mechanical manipulation of the canted ring to move the primary pole member. The ring (104) also prevents retraction of the main pole.The crew escape mechanism includes a magazine (60) and a number of lanyards (62), each lanyard being mounted by a roller loop (68) over the primary pole member (22). The strap on the roller loop has stitching for controlled release, a protection sheath (74) to prevent tangling and a hook member (69) for attachment to a crew harness.

    摘要翻译： 具有逃生舱（12）的穿梭式飞机（10）具有可附接到内壁和天花板的弓形形状的杆壳体（16），其开口端与逃生舱口相邻。 磁极壳体16包含由辊组件（30,35）引导的可伸缩和弓形的主极构件（22）和延伸极构件（23）。 延伸极构件（23）可相对于主极构件（22）滑动和延伸。 为了致动，弹簧致动系统包括在磁极壳体中的弹簧（52）。 锁定构件（90）通过极构件中的切口部分（85,86）接合两个极构件（22,23）。 锁定构件选择性地释放延伸极构件（23）和主极构件（22）。 内部单向离合器或止回机构防止延伸杆构件从延伸位置的缩回。 减震器（54）（150,152）用于吸收弹簧的能量。 提供了一种手动备用部署系统，其包括由弹簧构件（108）偏置的倾斜环（104）。 具有槽和销连接（102）的杆构件（100）允许倾斜环的机械操纵以移动主极构件。 环（104）还防止主极的收回。 机组逃逸机构包括一个杂志架（60）和多个系索（62），每个系索通过一个滚子回路（68）安装在主极构件（22）上。 滚子环上的带子具有用于控制释放的缝合，用于防止缠结的保护套（74）和用于附接到乘员组的钩构件（69）。

    Pre-integrated truss space station and method of assembly
    4.
    发明授权
    Pre-integrated truss space station and method of assembly 失效
    预组合桁架空间站和组装方法

    公开(公告)号：US5407152A

    公开(公告)日：1995-04-18

    申请号：US996763

    申请日：1992-12-24

    申请人： Timothy E. Pelischek ,  Edgar O. Castro ,  Gregg A. Edeen ,  David A. Hamilton ,  Jon B. Kahn ,  James B. McDede ,  Kornel Nagy ,  John V. Rivers ,  Irene E. Verinder ,  Donald C. Wade ,  Clarence J. Wesselski

    发明人： Timothy E. Pelischek ,  Edgar O. Castro ,  Gregg A. Edeen ,  David A. Hamilton ,  Jon B. Kahn ,  James B. McDede ,  Kornel Nagy ,  John V. Rivers ,  Irene E. Verinder ,  Donald C. Wade ,  Clarence J. Wesselski

    IPC分类号： B64G1/12 ,  B64G99/00 ,  B64G1/10

    CPC分类号： B64G9/00 ,  B64G1/12

    摘要： The present invention is directed to methods and apparatus relating to design, construction, integration and assembly of a space station. The present invention uses pre-integrated open (unpressurized) truss segments for modular construction of the space station. Each segment includes a truss structure and utility subsystems which may be fully assembled and tested on Earth. The segments may be latched together on orbit using a remote latching system. Utility subsystems, such as solar panels and radiators, are pre-integrated into the appropriate truss segment, and are deployable from the respective truss segment on orbit. Rails run lengthwise along the assembled truss. The rails may be used with a mobile transporter for translating truss segments with respect to the spacecraft as part of the space station assembly process. The rails may also be used with a mobile transporter for carrying crew personnel, a robotic arm, and other equipment.

    摘要翻译： 本发明涉及与空间站的设计，构造，集成和组装有关的方法和装置。 本发明使用预集成开放（非加压）桁架段用于空间站的模块化构造。 每个部分包括可在地球上完全组装和测试的桁架结构和效用子系统。 这些段可以使用远程锁定系统在轨道上锁定在一起。 诸如太阳能电池板和散热器之类的效用子系统被预先集成到适当的桁架段中，并且可从轨道上的相应的桁架段部署。 轨道沿组装桁架纵向延伸。 作为空间站组装过程的一部分，轨道可以与移动式运输机一起用于相对于航天器平移桁架段。 轨道还可以与移动运输机一起使用，用于携带机组人员，机器人手臂和其他设备。