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    • 1. 发明授权
    • Inflatable vessel and method
    • 充气船和方法
    • US06547189B1
    • 2003-04-15
    • US09826403
    • 2001-04-02
    • Jasen L. RaboinGerard D. ValleGregg A. EdeenHoracio M. de la FuenteWilliam C. SchneiderGary R. SpexarthShalini Gupta PandyaChristopher J. Johnson
    • Jasen L. RaboinGerard D. ValleGregg A. EdeenHoracio M. de la FuenteWilliam C. SchneiderGary R. SpexarthShalini Gupta PandyaChristopher J. Johnson
    • B64G112
    • B64G1/56B64G1/12B64G1/60B64G2001/224
    • An inflatable module comprising a structural core and an inflatable shell, wherein the inflatable shell is sealingly attached to the structural core. In its launch or pre-deployed configuration, the wall thickness of the inflatable shell is collapsed by vacuum. Also in this configuration, the inflatable shell is collapsed and efficiently folded around the structural core. Upon deployment, the wall thickness of the inflatable shell is inflated; whereby the inflatable shell itself, is thereby inflated around the structural core, defining therein a large enclosed volume. A plurality of removable shelves are arranged interior to the structural core in the launch configuration. The structural core also includes at least one longeron that, in conjunction with the shelves, primarily constitute the rigid, strong, and lightweight load-bearing structure of the module during launch. The removable shelves are detachable from their arrangement in the launch configuration so that, when the module is in its deployed configuration and launch loads no longer exist, the shelves can be rearranged to provide a module interior arrangement suitable for human habitation and work. In the preferred embodiment, to provide efficiency in structural load paths and attachments, the shape of the inflatable shell is a cylinder with semi-toroidal ends.
    • 一种可膨胀模块,包括结构芯和可充气壳,其中所述可充气壳密封地附接到所述结构芯。 在其发射或预部署配置中,可膨胀壳体的壁厚度通过真空折叠。 同样在这种构造中,可膨胀的壳被折叠并有效地围绕结构芯折叠。 展开后,充气壳的壁厚膨胀; 从而充气壳本身因此在结构芯周围膨胀,在其中限定了大的封闭容积。 在发射配置中,多个可移除的搁架布置在结构核心的内部。 结构芯还包括至少一个与架子一起构成发射期间模块的刚性,坚固和轻质的承载结构的长度。 可拆卸的货架可以在启动配置中与其布置可拆卸,使得当模块处于其部署配置并且不再存在启动负载时,可以重新布置货架以提供适合于人居住和工作的模块内部装置。 在优选实施例中,为了提供结构负载路径和附件的效率,可膨胀壳体的形状是具有半环形端部的圆柱体。
    • 2. 发明授权
    • Connecting node and method for constructing a connecting node
    • 连接节点和构建连接节点的方法
    • US08047473B2
    • 2011-11-01
    • US12240537
    • 2008-09-29
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • B64G1/00
    • B64G9/00B64G1/646Y10T29/49826Y10T403/342Y10T403/347
    • A connecting node comprises a polyhedral structure comprising a plurality of panels joined together at its side edges to form a spherical approximation, wherein at least one of the plurality of panels comprises a faceted surface being constructed with a passage for integrating with one of a plurality of elements comprising a docking port, a hatch, and a window that is attached to the connecting node. A method for manufacturing a connecting node comprises the steps of providing a plurality of panels, connecting the plurality of panels to form a spherical approximation, wherein each edge of each panel of the plurality is joined to another edge of another panel, and constructing at least one of the plurality of panels to include a passage for integrating at least one of a plurality of elements that may be attached to the connecting node.
    • 连接节点包括多面体结构,其包括在其侧边缘处连接在一起的多个面板以形成球面近似,其中所述多个面板中的至少一个面板包括具有通道的小面,所述通道用于与多个 包括对接端口,舱口盖和连接到连接节点的窗口的元件。 一种用于制造连接节点的方法包括以下步骤:提供多个面板,连接所述多个面板以形成球面近似,其中所述多个面板中的每个面板的每个边缘连接到另一个面板的另一个边缘,并且至少构造 所述多个面板中的一个包括用于集成可附接到所述连接节点的多个元件中的至少一个的通道。
    • 3. 发明授权
    • System and method of designing a load bearing layer that interfaces to a structural pass-through of an inflatable vessel
    • 设计与可膨胀容器的结构通过接口的承载层的系统和方法
    • US07840387B1
    • 2010-11-23
    • US11778858
    • 2007-07-17
    • Gary R. Spexarth
    • Gary R. Spexarth
    • G06F17/50G06F17/00B64G1/00B64G1/22
    • B64G9/00B64G2001/224
    • A method for determining a design of an inflatable module including a rigid member disposed in a restraint layer, wherein the restraint layer includes orthogonal straps, includes modeling a strap adjacent to the rigid member and a strap connected to the rigid member. The adjacent strap and the member strap extend in a first direction. The method further includes selecting a first length of the member strap such that the adjacent strap carries load before the member strap during pressurization of the inflatable module, modeling tensions in the member strap with the first length and the adjacent strap during pressurization of the inflatable model, and outputting the modeled tensions in the member strap with the first length and the adjacent strap. An inflatable module includes a member strap having a length such that an adjacent strap carries load before the member strap during pressurization of the inflatable module.
    • 一种用于确定包括设置在约束层中的刚性构件的可膨胀模块的设计的方法,其中所述约束层包括正交带,包括对邻近所述刚性构件的带进行建模和连接到所述刚性构件的带。 相邻的带和构件带沿第一方向延伸。 该方法还包括选择构件带的第一长度,使得相邻的带在可充气模块的加压期间在构件带之前承载载荷,在充气模型的加压期间模拟具有第一长度的构件带中的张力和相邻的带 并且将第一长度和相邻带的成型带中的建模张力输出。 可膨胀模块包括具有长度的构件带,使得相邻的带在可充气模块的加压期间在构件带之前承载载荷。
    • 5. 发明申请
    • CONNECTING NODE AND METHOD FOR CONSTRUCTING A CONNECTING NODE
    • 连接节点和连接节点的方法
    • US20100077674A1
    • 2010-04-01
    • US12240537
    • 2008-09-29
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • E04B1/00B21D39/03
    • B64G9/00B64G1/646Y10T29/49826Y10T403/342Y10T403/347
    • A connecting node comprises a polyhedral structure comprising a plurality of panels joined together at its side edges to form a spherical approximation, wherein at least one of the plurality of panels comprises a faceted surface being constructed with a passage for integrating with one of a plurality of elements comprising a docking port, a hatch, and a window that is attached to the connecting node. A method for manufacturing a connecting node comprises the steps of providing a plurality of panels, connecting the plurality of panels to form a spherical approximation, wherein each edge of each panel of the plurality is joined to another edge of another panel, and constructing at least one of the plurality of panels to include a passage for integrating at least one of a plurality of elements that may be attached to the connecting node.
    • 连接节点包括多面体结构,其包括在其侧边缘处连接在一起的多个面板以形成球面近似,其中所述多个面板中的至少一个面板包括具有通道的小面,所述通道用于与多个 包括对接端口,舱口盖和连接到连接节点的窗口的元件。 一种用于制造连接节点的方法包括以下步骤:提供多个面板,连接所述多个面板以形成球面近似,其中所述多个面板中的每个面板的每个边缘连接到另一个面板的另一个边缘,并且至少构造 所述多个面板中的一个包括用于集成可附接到所述连接节点的多个元件中的至少一个的通道。
    • 6. 发明授权
    • Inflatable nested toroid structure
    • 充气嵌套环形结构
    • US08070105B2
    • 2011-12-06
    • US11956826
    • 2007-12-14
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • Christopher J. JohnsonJasen L. RaboinGary R. Spexarth
    • B64G1/00
    • B64G1/12B64G1/54B64G1/56B64G9/00B64G2001/224
    • An inflatable structure comprises at least two generally toroidal, inflatable modules. When in a deployed mode, the first, inner module has a major diameter less than that of a second, outer module and is positioned within the inner circumference of the outer module such that the first module is nested circumferentially alongside the second module. The inflatable structure, in a non-deployed, non-inflated mode, is of compact configuration and adapted to be transported to a site of deployment. When deployed, the inflatable structure is of substantially increased interior volume. In one embodiment, access between the interior of the first module and the second module is provided by at least one port or structural pass-through. In another embodiment, the inflatable structure includes at least one additional generally toroidal module external of and circumferentially surrounding the second module.
    • 可充气结构包括至少两个通常为环形的可充气模块。 当处于展开模式时,第一内部模块的主要直径小于第二外部模块的直径,并且定位在外部模块的内圆周内,使得第一模块沿着第二模块沿圆周嵌套。 处于未部署的非充气模式的充气结构具有紧凑的构造并且适于被运送到展开部位。 当展开时,充气结构的内部容积基本上增加。 在一个实施例中,通过至少一个端口或结构通过来提供第一模块的内部和第二模块之间的接入。 在另一个实施例中,可膨胀结构包括至少一个额外的大体上环形模块,并且周向地围绕第二模块。
    • 7. 发明授权
    • Apparatus for integrating a rigid structure into a flexible wall of an inflatable structure
    • 用于将刚性结构集成到可充气结构的柔性壁中的装置
    • US07509774B1
    • 2009-03-31
    • US11610295
    • 2006-12-13
    • Christopher J. JohnsonRoss M. PattersonGary R. Spexarth
    • Christopher J. JohnsonRoss M. PattersonGary R. Spexarth
    • E04G11/04B64G1/14B64G1/00
    • B64G1/222B64G1/12B64G2001/224
    • For an inflatable structure having a flexible outer shell or wall structure having a flexible restraint layer comprising interwoven, load-bearing straps, apparatus for integrating one or more substantially rigid members into the flexible shell. For each rigid member, a corresponding opening is formed through the flexible shell for receiving the rigid member. A plurality of connection devices are mounted on the rigid member for receiving respective ones of the load-bearing straps. In one embodiment, the connection devices comprise inner connecting mechanisms and outer connecting mechanisms, the inner and outer connecting mechanisms being mounted on the substantially rigid structure and spaced along a peripheral edge portion of the structure in an interleafed array in which respective outer connecting mechanisms are interposed between adjacent pairs of inner connecting mechanisms, the outer connecting mechanisms projecting outwardly from the peripheral edge portion of the substantially rigid structure beyond the adjacent inner connecting mechanisms to form a staggered array of connecting mechanisms extending along the panel structure edge portion. In one embodiment, the inner and outer connecting mechanisms form part of an integrated, structure rotatably mounted on the rigid member peripheral edge portion.
    • 对于具有柔性外壳或壁结构的可膨胀结构,其具有柔性约束层,其包括交织的承载带,用于将一个或多个基本上刚性的构件整合到柔性外壳中的装置。 对于每个刚性构件,通过柔性壳体形成相应的开口,用于容纳刚性构件。 多个连接装置安装在刚性构件上用于接收相应的承载带。 在一个实施例中,连接装置包括内部连接机构和外部连接机构,内部和外部连接机构安装在基本上刚性的结构上并且沿着结构的外围边缘部分间隔开,其中相应的外部连接机构是 插入在相邻的一对内部连接机构之间,外部连接机构从基本上刚性结构的外围边缘部分向外突出超过相邻的内部连接机构,以形成沿着面板结构边缘部分延伸的交错排列的连接机构。 在一个实施例中,内部和外部连接机构形成可旋转地安装在刚性构件周边边缘部分上的集成的结构的一部分。
    • 8. 发明授权
    • System and method of designing a load bearing layer of an inflatable vessel
    • 设计充气容器承载层的系统和方法
    • US07295884B1
    • 2007-11-13
    • US11158354
    • 2005-06-20
    • Gary R. Spexarth
    • Gary R. Spexarth
    • G06F19/00B64G1/00
    • B64G1/12B64G2001/224
    • A computer-implemented method is provided for designing a restraint layer of an inflatable vessel. The restraint layer is inflatable from an initial uninflated configuration to an inflated configuration and is constructed from a plurality of interfacing longitudinal straps and hoop straps. The method involves providing computer processing means (e.g., to receive user inputs, perform calculations, and output results) and utilizing this computer processing means to implement a plurality of subsequent design steps. The computer processing means is utilized to input the load requirements of the inflated restraint layer and to specify an inflated configuration of the restraint layer. This includes specifying a desired design gap between pairs of adjacent longitudinal or hoop straps, whereby the adjacent straps interface with a plurality of transversely extending hoop or longitudinal straps at a plurality of intersections. Furthermore, an initial uninflated configuration of the restraint layer that is inflatable to achieve the specified inflated configuration is determined. This includes calculating a manufacturing gap between pairs of adjacent longitudinal or hoop straps that correspond to the specified desired gap in the inflated configuration of the restraint layer.
    • 提供了一种用于设计可充气容器的约束层的计算机实现的方法。 约束层可以从初始未膨胀构型充气到膨胀构型,并且由多个接合纵向带和箍带构成。 该方法涉及提供计算机处理装置(例如,接收用户输入,执行计算和输出结果),并利用该计算机处理装置实现多个后续设计步骤。 计算机处理装置用于输入充气约束层的载荷要求并指定约束层的膨胀构型。 这包括在相邻的纵向或环带之间指定期望的设计间隙,由此相邻的带与多个交叉点处的多个横向延伸的箍或纵向带接合。 此外,确定可充气以实现指定的膨胀构型的约束层的初始未膨胀构造。 这包括计算对应于约束层的膨胀构造中的指定的期望间隙的相邻纵向或箍带对之间的制造间隙。