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    • 1. 发明授权
    • Panel deployment system
    • 面板部署系统
    • US4151872A
    • 1979-05-01
    • US863036
    • 1977-12-21
    • Paul SlyshLeRoy E. Siden
    • Paul SlyshLeRoy E. Siden
    • H01Q1/08H01Q15/16H01Q15/20E06B3/32
    • H01Q15/20H01Q1/08H01Q15/162
    • A mechanism for deploying and retracting an isogrid structure particularly suited for use in supporting low weight reflective or absorbtive surfaces, characterized by a plurality of hinged isogrid panels stowed in an accordion folded stack arranged for automatic deployment into a long continuous strip or array. Two deployment arms in contact with the stack of panels are rotated to a position perpendicular to the stack, carrying with them a perforated deployment tape that is attached to the first panel. The tape is engaged to sprocket drives which draw the first panel from the stack. Thereafter, the panels are extended by the powered sprockets which engage perforations in the panel edges. A shutter sequentially releases pairs of panels during deployment. For retraction, the sprockets drive the panels back toward the stack where a creaser arm hinges pairs of panels which are thereafter folded into a stack by means of the shutter capturing and stowing each folded pair of panels.
    • 一种用于部署和缩回特别适合用于支撑低重量反射或吸收表面的等网格结构的机构,其特征在于,多个铰接的等网格板被放置在手风琴折叠的叠层中,其布置成自动展开成长的连续条带或阵列。 与堆叠的面板接触的两个展开臂旋转到垂直于堆叠的位置,与其一起携带连接到第一面板的穿孔展开胶带。 带子与从链轮拉出第一个面板的链轮驱动器啮合。 此后,面板通过在面板边缘处接合穿孔的动力链轮延伸。 快门在部署期间顺序地释放成对的面板。 为了缩回,链轮驱动面板返回到堆叠,在那里一个折臂铰链成对的面板,然后通过快门捕获和收起每对折叠的面板将其折叠成堆叠。
    • 2. 发明授权
    • Parts orbiter for chem-milling vat
    • 用于化学加工大桶的零件轨道器
    • US4921565A
    • 1990-05-01
    • US344688
    • 1989-04-28
    • Paul Slysh
    • Paul Slysh
    • C23F1/08
    • C23F1/08
    • An improved parts orbiter for use in a chem-milling vat. The orbiter has a major frame assembly that is self standing which is lowered into the chem-milling vat. A minor frame assembly is positioned within the major frame assembly and it is pivotally mounted thereto about a horizontal axis. A first motor is connected to a drive sprocket gear, a chain, and a driven sprocket gear for rotating the minor frame assembly about the horizontal axis. A planetary gear is mounted on a shaft extending upwardly from the bottom cross member of the minor frame assembly. Its teeth are in meshing engagement with a sun gear that is mounted on a shaft whose one end passes through one of the horizontal side members of the minor frame assembly and has its end also passing through one of the upright side members of the major frame assembly. A second drive motor is connected through a drive sprocket gear, a chain, and a driven gear which itself is also mounted on the same shaft that the sun gear is mounted on. The second motor allows the planetary gear to be rotated around a vertical axis at the same time that the minor frame assembly is rotating around its horizontal axis.
    • 用于化学加工槽的改进的零件轨道器。 轨道飞行器具有自主站立的主要框架组件,其下降到化学研磨槽中。 小框架组件定位在主框架组件内,并且其围绕水平轴线枢转地安装到其上。 第一马达连接到驱动链轮齿轮,链条和从动链轮齿轮,用于使小框架组件围绕水平轴线旋转。 行星齿轮安装在从小框架组件的底部横向构件向上延伸的轴上。 其齿与安装在轴上的太阳齿轮啮合,其一端穿过小框架组件的水平侧构件中的一个,并且其端部也穿过主框架组件的直立侧构件之一 。 第二驱动马达通过驱动链轮齿轮,链条和从动齿轮连接,该自动齿轮本身也安装在安装太阳齿轮的同一轴上。 第二马达允许行星齿轮围绕垂直轴旋转,同时小框架组件围绕其水平轴线旋转。
    • 3. 发明授权
    • Expandable panel and truss system/antenna/solar panel
    • 可扩展面板和桁架系统/天线/太阳能电池板
    • US4380013A
    • 1983-04-12
    • US234830
    • 1981-02-17
    • Paul Slysh
    • Paul Slysh
    • F24S23/70H01Q1/28H01Q15/16H01Q1/08
    • H01Q1/288F24J2/1052H01Q15/161Y02E10/40Y10S136/292Y10S343/02
    • Disclosed is an expandable panel and truss structure capable of being stowed in a storage container (canister) for transportation into space and deployed to form structures such as antennas, solar panels or similar space or terrestial structures. The antenna formed comprises the panels stored as hinged pairs (sets) folded in accordian-like fashion together with the expandable trusses and other devices necessary for antenna space operation, such as attitude control and antenna feed. The panel sets are deployed from the canister to form a toroidal ring, circular in cross-section when deployed, for supporting the antenna lens and to form a feed support boom utilizing the canister as part of the antenna structure. The canister is connected to the ring and support boom in the deployed state by the expandable trusses. A fully automatic system is included for deploying the antenna and for holding the antenna structure in its deployed state. By adding a second (back) boom and reflector screen, a paraboloidal antenna is formed.In a second embodiment, utilizing the same storage and deployment principle but with panel sets which are triangular in cross-section, when deployed, either an offset (asymmetrical) paraboloidal or a feed horn type antenna structure is formed.In another embodiment of the invention, utilizing the same principle and with panel sets which are triangular in cross-section, when deployed, a solar panel array is formed.Also disclosed is a foldable truss geostationary platform and package for transfer into a geostationary orbit.Finally, an alternate mechanism is disclosed in the form of a pantograph for deploying panel sets to form a truss.
    • 公开了一种可扩展的面板和桁架结构,其能够被收纳在存储容器(罐)中以便运输到空间中并展开以形成诸如天线,太阳能电池板或类似空间或地面结构的结构。 形成的天线包括作为铰接对(集合)存储的面板,其与可扩展桁架和天线空间操作所需的其它装置(例如姿态控制和天线馈送)一起折叠成一体。 面板组从罐展开形成环形环,其展开时为横截面圆形,用于支撑天线透镜,并形成利用该罐作为天线结构的一部分的进料支撑臂。 罐通过可扩展的桁架连接到环和支撑臂处于展开状态。 包括用于部署天线和用于将天线结构保持在其部署状态的全自动系统。 通过添加第二(后)悬臂和反射器屏幕,形成抛物面天线。 在第二实施例中,利用相同的存储和部署原理,但是具有横截面为三角形的面板组,当展开时,形成偏移(非对称)抛物面或馈电喇叭型天线结构。 在本发明的另一个实施例中,利用相同的原理和具有横截面为三角形的面板组,当展开时形成太阳能电池板阵列。 还披露了一种用于转移到地球静止轨道的可折叠桁架对地静止平台和包装。 最后,以用于部署面板组以形成桁架的缩放仪的形式公开了一种替代机构。
    • 4. 发明授权
    • Structural node for large space structures
    • 大型空间结构的结构节点
    • US4332501A
    • 1982-06-01
    • US225549
    • 1981-01-16
    • Paul Slysh
    • Paul Slysh
    • E04B1/19E04H12/18E04H12/00
    • E04B1/19E04H12/182E04B2001/1918E04B2001/1927E04B2001/1933E04B2001/1936E04B2001/1957E04B2001/1963E04B2001/1987Y10T403/342Y10T403/447Y10T403/53
    • An automated assembly, maintenance, and repair system for the construction of a large space structure. The space structure comprises a plurality of trusses and truss junctions that in turn are made up of a plurality of individual struts and nodes. The truss assemblies are progressively built by an assembler trolley as the trolley crawls along the constructed truss. The trolley comprises a forward crawler and a rear crawler joined by an articulated coupler. The crawlers are carried along the structure by belt transports incorporating grippers that engage the truss structure at the nodes. Manipulator arms for strut and node assembly are located on the forward crawler, and the majority of control, power, and communication systems are located in the rear crawler. Cargo canisters filled with component parts for constructing the space structure are carried by the forward crawler. The space structure configuration is determined by the arrangement of the individual struts and nodes during the assembly process.
    • 一种用于建造大型空间结构的自动组装,维护和修理系统。 空间结构包括多个桁架和桁架结,其又由多个独立的支柱和节点组成。 桁架组件由组装推车逐步建成,因为手推车沿着构造的桁架爬行。 手推车包括前履带和由铰接式联接器连接的后履带。 爬行器通过带式输送装置沿着结构承载,该输送装置包括在节点处接合桁架结构的夹具。 用于支柱和节点组装的操纵臂是位于前履带上的,大多数控制,动力和通讯系统位于后履带。 填充有用于构造空间结构的部件的货物容器由前向履带承载。 空间结构配置由组装过程中各个支柱和节点的布置决定。
    • 6. 发明授权
    • Method for assembling large space structures
    • 组合大型空间结构的方法
    • US4337560A
    • 1982-07-06
    • US103990
    • 1979-12-17
    • Paul Slysh
    • Paul Slysh
    • B64G99/00E04B1/19E04H12/18B23P11/00B64G1/10
    • E04H12/182B64G9/00E04B1/19E04B2001/1918E04B2001/1927E04B2001/1933E04B2001/1936E04B2001/1957E04B2001/1963E04B2001/1987Y10T29/49625Y10T29/4987Y10T403/347
    • An automated assembly, maintenance, and repair system for the construction of a large space structure. The space structure comprises a plurality of trusses and truss junctions that in turn are made up of a plurality of individual struts and nodes. The truss assemblies are progressively built by an assembler trolley as the trolley crawls along the constructed truss. The trolley comprises a forward crawler and a rear crawler joined by an articulated coupler. The crawlers are carried along the structure by belt transports incorporating grippers that engage the truss structure at the nodes. Manipulator arms for strut and node assembly are located on the forward crawler, and the majority of control, power, and communication systems are located in the rear crawler. Cargo canisters filled with component parts for constructing the space structure are carried by the forward crawler. The space structure configuration is determined by the arrangement of the individual struts and nodes during the assembly process.
    • 一种用于建造大型空间结构的自动组装,维护和修理系统。 空间结构包括多个桁架和桁架结,其又由多个独立的支柱和节点组成。 桁架组件由组装推车逐步建成,因为手推车沿着构造的桁架爬行。 手推车包括前履带和由铰接式联接器连接的后履带。 爬行器通过带式输送装置沿着结构承载,该输送装置包括在节点处接合桁架结构的夹具。 用于支柱和节点组装的操纵臂是位于前履带上的,大多数控制,动力和通讯系统位于后履带。 填充有用于构造空间结构的部件的货物容器由前向履带承载。 空间结构配置由组装过程中各个支柱和节点的布置决定。
    • 8. 发明授权
    • Panel deployment and retraction system
    • 面板部署和退回系统
    • US4116258A
    • 1978-09-26
    • US870305
    • 1978-01-18
    • Paul SlyshLeRoy E. Siden
    • Paul SlyshLeRoy E. Siden
    • H01Q1/08H01Q15/16E06B3/32
    • H01Q15/162H01Q1/08
    • A mechanism for deploying and retracting an isogrid structure particularly suited for use in supporting low weight reflective or absorbtive surfaces, characterized by a plurality of hinged isogrid panels stowed in an accordian folded stack arranged for deployment into a long continuous strip or array. Two deployment frames in contact with the stack of panels are rotated to a position perpendicular to the stack. Attached at the outermost ends of each panel hinge are panel rollers. In the accordian folded position, these rollers are alternately located near the top and bottom of the folded stack. The deployment frames each contain an arced raceway for engagement of the upper panel rollers and a straight raceway for engagement of the lower rollers. An upper roller travels down the arced raceway thereby progressively unfolding a pair of hinged panels until they are flat and lie in the deployment plane where they are subsequently extended into the deployed position. For retraction the panels are driven back toward the stack where the upper rollers travel up the arced raceway causing a hinged pair of panels to be refolded together and thereafter be moved into the stack stowage container.
    • 一种用于部署和缩回特别适合用于支撑低重量反射或吸收表面的等网格结构的机构,其特征在于,多个铰接的等网格板被收纳在一起,被布置成展开成长的连续条带或阵列。 与堆叠的面板接触的两个展开框架旋转到垂直于堆叠的位置。 每个面板铰链的最外端附有板辊。 在折叠式折叠位置,这些辊子交替地位于折叠堆叠的顶部和底部附近。 部署框架每个都包含一个弧形滚道,用于接合上面板滚子和一个直线滚道,用于啮合下部滚筒。 上滚轮沿着弧形滚道行进,从而逐渐展开一对铰链板,直到它们平坦并且位于展开平面中,随后它们延伸到展开位置。 为了缩回,板被驱回到堆叠,其中上辊沿着弧形轨道向上行进,导致铰接的一对面板重新折叠在一起,然后移动到堆叠存放容器中。
    • 9. 发明授权
    • Panel deployment system
    • 面板部署系统
    • US4015653A
    • 1977-04-05
    • US675007
    • 1976-04-08
    • Paul SlyshLeRoy E. Siden
    • Paul SlyshLeRoy E. Siden
    • H01Q1/12H01Q15/20E06B3/32
    • H01Q15/20H01Q1/1235
    • A mechanism for deploying and retracting an isogrid structure particularly suited for use in supporting low weight reflective or absorbtive surfaces, characterized by a plurality of hinged isogrid panels stowed in an accordian folded stack arranged for automatic deployment into a long continuous strip or array. Two deployment arms in contact with the stack of panels are rotated to a position perpendicular to the stack, carrying with them the first panels. Thereafter the panels are extended by powered sprockets which engage the panel edges. A shutter bar sequentially releases pairs of panels during deployment. For retraction, the sprockets drive the panels back toward the stack where a creaser bar hinges pairs of panels which are thereafter folded into a stack by means of the shutter bar capturing and stowing each folded pair of panels.
    • 一种用于部署和缩回特别适合于用于支撑低重量反射或吸收表面的等网格结构的机构,其特征在于,多个铰接的等网格板被放置在以折叠式折叠堆叠布置,用于自动展开成长的连续条带或阵列。 与堆叠的面板接触的两个展开臂旋转到垂直于堆叠的位置,与它们一起携带第一面板。 此后,面板通过接合面板边缘的动力链轮延伸。 快门条在部署期间顺序地释放成对的面板。 为了缩回,链轮驱动面板返回到堆叠,在那里一个压紧杆铰链成对的面板,然后通过快门棒捕获和收起每对折叠的面板将其折叠成堆叠。