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    ROTARY JOINT, FRAMEWORK CONSTRUCTION KIT, FRAMEWORK WITH ROTARY JOINTS AND METHOD FOR MANUFACTURING A ROTARY JOINT
    96.
    发明申请
    ROTARY JOINT, FRAMEWORK CONSTRUCTION KIT, FRAMEWORK WITH ROTARY JOINTS AND METHOD FOR MANUFACTURING A ROTARY JOINT 审中-公开
    旋转接头，框架结构工具包，带旋转接头的框架和制造旋转接头的方法

    公开(公告)号：US20170058959A1

    公开(公告)日：2017-03-02

    申请号：US15247008

    申请日：2016-08-25

    申请人： AIRBUS OPERATIONS GMBH

    发明人： Herman BENTHIEN ,  Andreas POPPE

    IPC分类号： F16D3/04

    CPC分类号： E04B1/19 ,  B64C1/00 ,  B64C1/08 ,  B64C13/28 ,  E04B1/1909 ,  E04B2001/1942 ,  E04B2001/1969 ,  E04C2003/0495 ,  F16C11/06 ,  F16C2220/24 ,  Y10T403/32213

    摘要： A rotary joint includes a socket rod having a socket rod flange with a basically spheroid concave bearing surface at a first end, a housing nut encircling the socket rod and having a threaded wrenching head, and a ball rod having a basically spheroid convex bearing surface and threaded side walls around the bearing surface. A diameter of the threaded side walls of the ball rod corresponds to a diameter of the threaded wrenching head of the housing nut. First guiding tracks are on the concave bearing surface oriented into a first swivelling direction, the socket rod being swivable to the ball rod along the first guiding tracks into the first swivelling direction. Second guiding tracks are on the convex bearing surface and oriented into a second swivelling direction, the socket rod being swivellable to the ball rod along the second guiding tracks into the second swivelling direction.

    摘要翻译： 一种旋转接头包括一个插座杆，该插座杆具有一个在第一端具有基本上球形的凹形支承表面的插座法兰，一个环绕该插座的壳体螺母，并具有一个带螺纹的扳手头部，以及一个具有基本上球形凸起的支承表面的球杆， 螺纹侧壁围绕轴承表面。 球杆的螺纹侧壁的直径对应于壳体螺母的螺纹扳手头部的直径。 第一引导轨道位于朝向第一旋转方向的凹入轴承表面上，所述插座杆沿着第一引导轨道可选择地沿着第一导轨移动到第一旋转方向。 第二引导轨道位于凸起的支承面上并且被定向成第二旋转方向，该插座杆可沿着第二引导轨道转动到球杆到第二旋转方向。

    GEODESIC STRUCTURE FORMING SYSTEMS AND METHODS
    97.
    发明申请
    GEODESIC STRUCTURE FORMING SYSTEMS AND METHODS 有权
    地质构造系统与方法

    公开(公告)号：US20170057029A1

    公开(公告)日：2017-03-02

    申请号：US14840845

    申请日：2015-08-31

    申请人： THE BOEING COMPANY

    发明人： Sina Golshany ,  Junghyun Ahn ,  Derek Alderks ,  Todd William Erickson

    IPC分类号： B23P23/04 ,  B21J15/30 ,  B23B41/00 ,  B21J15/14

    CPC分类号： B23B41/00 ,  B21J15/142 ,  B21J15/30 ,  B23B2215/04 ,  B64C1/08 ,  B64C1/12 ,  B64F5/10 ,  Y10T29/49616 ,  Y10T29/49622 ,  Y10T29/49867 ,  Y10T29/49943 ,  Y10T29/49947 ,  Y10T29/49956

    摘要： A system and method determine a size and a shape for identical geodesic modules that are used to form a structure. The system and method may include analyzing input data regarding a size and a shape of the structure to be formed, and determining the size and the shape for each of the identical geodesic modules based on the size and the shape of the structure to be formed. The structure may include a framework including the identical geodesic modules. Each of the geodesic modules has a size and a shape that are the same as all of the other of the geodesic modules. A forming system and method position a framework and a covering skin of the structure in relation to a mandrel, and drill and rivet the framework to the covering skin with a plurality of operating heads.

    摘要翻译： 系统和方法确定用于形成结构的相同测地板模块的尺寸和形状。 系统和方法可以包括分析关于要形成的结构的尺寸和形状的输入数据，并且基于要形成的结构的尺寸和形状来确定每个相同测地模块的尺寸和形状。 该结构可以包括包括相同测地板模块的框架。 每个测地线模块具有与所有其他测地线模块相同的尺寸和形状。 成形系统和方法将结构的框架和覆盖层相对于心轴定位，并用多个操作头钻孔并将框架铆接到覆盖表皮上。

    TRUSSED STRUCTURE
    99.
    发明申请
    TRUSSED STRUCTURE 审中-公开
    TRUSSED结构

    公开(公告)号：US20170015401A1

    公开(公告)日：2017-01-19

    申请号：US15277408

    申请日：2016-09-27

    申请人： Airbus Operations Limited

    发明人： Allan Kaye

    IPC分类号： B64C1/06 ,  B64C1/18 ,  E04C3/29 ,  B64C3/18

    CPC分类号： B64C1/061 ,  B64B1/08 ,  B64C1/065 ,  B64C1/08 ,  B64C1/18 ,  B64C3/187 ,  B64C2001/0072 ,  E04C3/28 ,  E04C3/291 ,  E04C2003/0491 ,  Y02T50/43

    摘要： A trussed structure comprising a frame and at least one strut, wherein the frame is of composite material and includes sockets which are integral with the frame. The invention also provides a process of making the trussed structures. The struts are typically of composite material and the trussed structures of the invention are particularly suitable for use in aircraft, for example, as wing ribs or floor beams.

    摘要翻译： 包括框架和至少一个支柱的桁架结构，其中所述框架是复合材料并且包括与所述框架成一体的插座。 本发明还提供了制造桁架结构的方法。 支柱通常是复合材料，并且本发明的桁架结构特别适用于飞机，例如作为翼肋或地板梁。

    SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE AND METHOD OF USE
    100.
    发明申请
    SELF-RIGHTING FRAME AND AERONAUTICAL VEHICLE AND METHOD OF USE 审中-公开
    自动车架和航空汽车及其使用方法

    公开(公告)号：US20160375983A1

    公开(公告)日：2016-12-29

    申请号：US15257904

    申请日：2016-09-06

    申请人： Gaofei YAN ,  James DEES

    发明人： Gaofei YAN ,  James DEES

    IPC分类号： B64C17/02 ,  G05D1/00 ,  B64C1/08 ,  B64C27/10 ,  B64C39/02 ,  B64D47/08

    CPC分类号： B64C17/02 ,  A63H15/06 ,  A63H27/12 ,  A63H30/04 ,  A63H33/005 ,  B64C1/00 ,  B64C1/061 ,  B64C1/08 ,  B64C17/00 ,  B64C27/10 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/146 ,  B64D47/08 ,  G05D1/0011 ,  G05D1/0094

    摘要： A self-righting aeronautical vehicle comprising a hollowed frame and a lift mechanism. The exterior of the frame and center of gravity are adapted to self-right the vehicle. The frame can include sealed, hollowed sections for use in bodies of water. The frame can be spherical in shape enabling inspection of internal surface of partially or fully enclosed structures. Inspection equipment can be integrated into the vehicle and acquired data can be stored or wirelessly communicated to a server. A controlled or other mass can be pivotally assembled to a pivot axle spanning across the interior of the frame. The pivot axis can rotate about a vertical axis (an axis perpendicular to the elongated axis). The propulsion mechanisms can be adapted for use as a terrestrial vehicle when enclosed in a sealed spherical shell.

    摘要翻译： 包括中空框架和提升机构的自动对准的航空运输车辆。 框架的外部和重心适合车辆自行右转。 框架可以包括用于水体的密封的中空部分。 框架可以是球形的，使得能够检查部分或全部封闭结构的内表面。 检查设备可以集成到车辆中，并且获取的数据可以被存储或无线地传送到服务器。 受控或其他质量可以枢转地组装到横跨框架内部的枢转轴。 枢转轴线可绕垂直轴线（垂直于细长轴线的轴线）旋转。 当封闭在密封的球壳中时，推进机构可适用于陆地车辆。