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    • 1. 发明授权
    • Deployable/retractable telescoping mast assembly and method
    • 可部署/伸缩式伸缩杆总成及方法
    • US5315795A
    • 1994-05-31
    • US862009
    • 1992-04-01
    • Daniel S. H. ChaeDavid J. RohwellerMark W. Thomson
    • Daniel S. H. ChaeDavid J. RohwellerMark W. Thomson
    • B66C23/687B66F11/00E04H12/18B66C23/06
    • B66F11/00E04H12/182E04H12/185Y10T403/32516
    • A deployable and retractable, telescoping style mast assembly and method employs a plurality of tubular sections of differing diameters. The tubular sections are nested one-in-another and are slidable with respect to each other, in a telescoping manner, to provide a deployable/retractable telescoping mast assembly. Retractable pins are provided to retractably extend from a collar coupled to at least one of the tube sections. In their extended state, the retractable pins are adapted to extend through apertures provided in an adjacent tube section. The retractable pins are provided with a head at one end thereof. The head of each pin is adapted to be engaged by a guide coupled to a third tube section upon the third tube section being in a collapsed state. Upon engagement with the pin head, the guide operates to pull the pin into a retracted state so as to retract the pin out of the pin receiving aperture.
    • 可部署和可伸缩的伸缩式桅杆组件和方法采用不同直径的多个管状部分。 管状部分一个接一个地嵌套并且可以以伸缩的方式相对于彼此滑动,以提供可展开/可伸缩的伸缩式桅杆组件。 提供伸缩销以从联接到至少一个管段的套环伸缩地延伸。 在伸展状态下,伸缩销适于延伸通过设置在相邻管部分中的孔。 可伸缩销在其一端设置有头部。 每个销的头部适于在第三管部分处于折叠状态时由连接到第三管部分的引导件接合。 在与销头接合时,引导件操作以将销拉入缩回状态,以将销从销接收孔缩回。
    • 3. 发明授权
    • Micro fold reflector
    • 微折反射器
    • US06323827B1
    • 2001-11-27
    • US09479839
    • 2000-01-07
    • L. Dwight GilgerMark W. ThomsonJohn C. Gereau
    • L. Dwight GilgerMark W. ThomsonJohn C. Gereau
    • H01Q1520
    • H01Q15/161H01Q1/08
    • A perimeter truss structure (103) that may be used, for example, to support an RF reflector may include multiple deployed bays (200) arranged in a ring. Each deployed bay (200) includes a first upper horizontal support member (726) attached to a first vertical support member (706) and collapsible on a first joint (728) translating on a second vertical support member (708), as well as a first lower horizontal support member (714) attached to the second vertical support member (708) and collapsible on a second joint (744) translating on the first vertical support member (706). The first and second vertical support members (706, 708) define a ring inside (122) and a ring outside (124). The first upper horizontal support member (712) is disposed on one ring side (e.g., the outside), while the first lower horizontal support member (714) is disposed on the opposite ring side. The horizontal support members (712, 714) (which are oriented vertically in the stowed position) are thus non-interfering in the stowed position.
    • 可以例如用于支撑RF反射器的周边桁架结构(103)可以包括布置在环中的多个部署的托架(200)。 每个部署间隔(200)包括附接到第一垂直支撑构件(706)并可折叠在第二垂直支撑构件(708)上平移的第一接头(728)上的第一上部水平支撑构件(726),以及 第一下部水平支撑构件(714),其附接到第二垂直支撑构件(708)并且可折叠在在第一垂直支撑构件(706)上平移的第二接头(744)上。 第一和第二垂直支撑构件(706,708)在内部(122)和环(124)内限定环。 第一上水平支撑构件(712)设置在一个环侧(例如外侧)上,而第一下水平支撑构件(714)设置在相对的环侧。 因此,水平支撑构件(712,714)(其在收起位置中垂直取向)因此在收起位置中不干扰。
    • 5. 发明授权
    • Spacecraft with deployable panel array
    • 具有可部署面板阵列的航天器
    • US06478261B2
    • 2002-11-12
    • US09184625
    • 1998-11-02
    • Peter B. LarawayMark W. Thomson
    • Peter B. LarawayMark W. Thomson
    • B64G144
    • B64G1/222B64G1/443B64G1/66E05D3/16E05Y2900/502
    • A spacecraft, such as a satellite, comprises a panel array including a plurality of panels that are rotatably coupled to one another. The panel array is movable between a folded state and an extended state. In the folded state, the panels are stacked atop one another. In the extended state, the panels are positioned such that active surfaces of the panels are aligned within a common plane. A plurality of hinge mechanisms preferably rotatably couple the panels to one another. The hinge mechanisms are configured to move the panel array from the folded state to the extended state without interfering with the active surfaces of the panels when the panel array is extended.
    • 诸如卫星的航天器包括面板阵列,其包括彼此可旋转地联接的多个面板。 面板阵列可在折叠状态和伸出状态之间移动。 在折叠状态下,面板彼此堆叠。 在扩展状态下,面板被定位成使得面板的有效表面在公共平面内对准。 多个铰链机构优选地将面板彼此可旋转地联接。 铰链机构构造成当面板阵列延伸时,将面板阵列从折叠状态移动到伸展状态,而不会妨碍面板的活动表面。