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    Support pole with a prefabricated engaging thread and method of using the same
    5.
    发明授权
    Support pole with a prefabricated engaging thread and method of using the same 有权
    带有预制接合螺纹的支撑杆及其使用方法

    公开(公告)号：US09447599B1

    公开(公告)日：2016-09-20

    申请号：US14741703

    申请日：2015-06-17

    申请人： Richard Parent

    发明人： Richard Parent

    IPC分类号： F16M13/00 ,  E04H12/22 ,  A47G29/122 ,  E04H17/22 ,  F16B1/00

    CPC分类号： E04H12/2223 ,  A47G29/1216 ,  E04H17/22 ,  F16B11/008 ,  F16B2001/0035

    摘要： The present invention generally relates to a support pole having a spike unit with a prefabricated engaging thread and a method of using the same. The top of the spike unit is internally secured within a bottom opening of the support pole by an epoxy wherein the bottom of the support pole rests on a generally circular ridge of the spike unit. The support pole is especially suitable for use with mailbox posts, birdhouse posts, volleyball posts, fences, or the like. The support pole may be securely inserted or removed from the ground without the need for concrete, shovels and other numerous tools. The support pole has an opening on its exterior side for temporarily receiving a perpendicularly inserted rod which is inserted therein so as to provide leverage for driving the support pole into the ground by rotating the support pole clockwise or counter-clockwise.

    摘要翻译： 本发明一般涉及具有带预制接合线的尖峰单元的支撑杆及其使用方法。 尖钉单元的顶部通过环氧树脂内部固定在支撑杆的底部开口内，其中支撑杆的底部位于尖钉单元的大致圆形的脊上。 支撑杆特别适用于邮箱，鸟舍，排球柱，围栏等。 支撑杆可以牢固地从地面上插入或移除，而不需要混凝土，铲子和其他许多工具。 支撑杆在其外侧具有开口，用于临时接收插入其中的垂直插入的杆，以便通过顺时针或逆时针旋转支撑杆来提供用于将支撑杆驱动到地面中的杠杆作用。

    TRUSS STRUCTURE OPTIMIZATION TECHNIQUES
    6.
    发明申请
    TRUSS STRUCTURE OPTIMIZATION TECHNIQUES 审中-公开
    TRUSS结构优化技术

    公开(公告)号：US20160253444A1

    公开(公告)日：2016-09-01

    申请号：US15053993

    申请日：2016-02-25

    申请人： Space Systems/Loral, LLC

    发明人： Daniel Albino Rodrigues ,  Michael Paul Freestone

    IPC分类号： G06F17/50

    CPC分类号： B64G9/00 ,  B64G1/10 ,  F16B7/00 ,  F16B7/185 ,  F16B11/008 ,  G06F17/5018

    摘要： Design of a 3-D truss structure, including a plurality of coupling nodes and a plurality of struts, is optimized by performing a quantitative optimization of an objective function corresponding to a figure of merit of the design. The quantitative optimization includes: generating a finite element analysis model, the analysis model a 3-D lattice mesh of strut-like finite elements; computing, with the finite element analysis model, a value for the objective function; and optimizing the objective function by executing at least two cycles of an optimization loop. The optimization loop includes a) computing a respective parameter of each strut-like finite element; b) deleting, from the finite element analysis model, selected finite elements for which a resulting mechanical property is less than a threshold; (c) computing an updated value for the objective function; and repeating the optimization loop until the objective function is within a desired tolerance of the specified value.

    摘要翻译： 通过执行对应于设计品质因数的目标函数的定量优化来优化包括多个耦合节点和多个支柱的3-D桁架结构的设计。 定量优化包括：生成有限元分析模型，分析模型支撑样有限元的3-D网格; 用有限元分析模型计算目标函数的值; 并通过执行优化循环的至少两个循环来优化目标函数。 优化循环包括：a）计算每个支柱样有限元的相应参数; b）从有限元分析模型中删除所得到的机械特性小于阈值的有限元; （c）计算目标函数的更新值; 并重复优化循环，直到目标函数在指定值的期望公差内。

    COAXIAL ASSEMBLY AND ASSEMBLY METHOD USING THE SAME
    7.
    发明申请
    COAXIAL ASSEMBLY AND ASSEMBLY METHOD USING THE SAME 有权
    同轴组装及组装方法

    公开(公告)号：US20160195120A1

    公开(公告)日：2016-07-07

    申请号：US14753563

    申请日：2015-06-29

    申请人： Fu Tai Hua Industry (Shenzhen) Co., Ltd. ,  HON HAI PRECISION INDUSTRY CO., LTD.

    发明人： AN-GUO HU

    IPC分类号： F16B11/00 ,  F16B7/04

    CPC分类号： F16B11/008 ,  F16B7/0413

    摘要： An coaxial assembly includes a first member, a second member, and at least two position members. The first member has an assembly hole with a sidewall. The second member having an lateral wall. The at least two position members are evenly arranged along a circumference of the lateral wall of the second member. The second member and assembly hole are configured such that when the second member is within the assembly hole, the at least two position members tightly abut the sidewall of the assembly hole, thereby causing the second assembly member to be coaxial with the first assembly member. An assembly method is also provided.

    摘要翻译： 同轴组件包括第一构件，第二构件和至少两个位置构件。 第一构件具有带侧壁的组装孔。 第二构件具有侧壁。 所述至少两个位置构件沿着所述第二构件的侧壁的圆周均匀地布置。 第二构件和组装孔被构造成使得当第二构件在组合孔内时，至少两个位置构件紧密地邻接组装孔的侧壁，从而使第二组合构件与第一组合构件同轴。 还提供了组装方法。

    Self pumping and priming adhesive joint system
    8.
    发明授权
    Self pumping and priming adhesive joint system 有权
    自吸和起泡胶接系统

    公开(公告)号：US09382933B2

    公开(公告)日：2016-07-05

    申请号：US13430117

    申请日：2012-03-26

    申请人： Daniel P. Sottiaux ,  Frank B. Stamps

    发明人： Daniel P. Sottiaux ,  Frank B. Stamps

    IPC分类号： C09J5/00 ,  F16B11/00 ,  B64D27/26

    CPC分类号： F16B11/008 ,  B64D27/26 ,  C09J5/00 ,  Y10T403/343 ,  Y10T403/473 ,  Y10T403/52

    摘要： A tube form assembly includes an inner member and an outer member. Each of the inner and outer members has an offset which creates a cavity therebetween. During assembly of the tube form assembly, an adhesive is located in the cavity and squeezed out and through the adjacent bond lines between the inner member and outer member. The pressurization and flow of adhesive outward from the cavity facilitates removal of air bubbles, as well as prevents the introduction of air bubbles into the bond line.

    摘要翻译： 管形组件包括内部构件和外部构件。 内部和外部构件中的每一个具有在其之间形成空腔的偏移。 在组装管形组件期间，粘合剂位于空腔中并挤出并穿过内部构件和外部构件之间的相邻接合线。 从空腔向外的粘合剂的加压和流动有助于除去气泡，同时防止气泡进入粘合线。

    Precision Optical Mount for Optical Devices
    9.
    发明申请
    Precision Optical Mount for Optical Devices 有权
    光学器件精密光学支架

    公开(公告)号：US20160018618A1

    公开(公告)日：2016-01-21

    申请号：US14337034

    申请日：2014-07-21

    申请人： Raytheon Company

    发明人： Lyale F. Marr ,  Douglas J. Hartnett ,  Randy W. White ,  Richard L. Scott

    IPC分类号： G02B7/00 ,  B32B37/18 ,  B32B37/12 ,  B32B37/14

    CPC分类号： G02B7/003 ,  B32B37/1292 ,  B32B37/142 ,  B32B37/18 ,  B32B2037/1253 ,  B32B2551/00 ,  F16B5/025 ,  F16B9/026 ,  F16B11/008 ,  G02B7/008 ,  G02B7/1822

    摘要： An optical mount and mounting system including an optical device, a housing, and a plurality of optical mounts that couple the optical device to the optical housing. Each mount includes a sleeve attached to the optical device and each sleeve includes a bore. Studs are attached to the optical housing and each stud includes an outer bonding surface extending through the bore of each sleeve. Once the optical device is aligned properly, a curable material is deposited into the sleeve and cured between the sleeve and the stud, such that the curable material couples the sleeve and the stud to each other to provide a robust structural joint that minimizes self-induced stresses into the optic. A series of annular conical portions and corresponding surfaces are provided to retain registration of the optical device against dynamic shearing and bending forces. A method of aligning and mounting an optical device is provided.

    摘要翻译： 一种光学安装和安装系统，包括光学装置，壳体和将光学装置耦合到光学壳体的多个光学安装座。 每个安装件包括附接到光学装置的套筒，并且每个套筒包括孔。 螺柱连接到光学壳体，并且每个螺柱包括延伸穿过每个套筒的孔的外部接合表面。 一旦光学装置正确对准，可固化材料沉积到套筒中并在套管和螺柱之间固化，使得可固化材料将套筒和螺柱彼此连接，以提供坚固的结构接头，使自诱导 强调进入视神经。 提供一系列环形锥形部分和对应的表面以保持光学装置的对准以抵抗动态剪切和弯曲力。 提供了一种对准和安装光学装置的方法。

    HOLDER FOR CONNECTING A MODULE TO A COMPONENT OF AN AIRCRAFT OR SPACECRAFT, ARRANGEMENT, AIRCRAFT OR SPACECRAFT, AND METHOD
    10.
    发明申请
    HOLDER FOR CONNECTING A MODULE TO A COMPONENT OF AN AIRCRAFT OR SPACECRAFT, ARRANGEMENT, AIRCRAFT OR SPACECRAFT, AND METHOD 审中-公开
    将模块连接到飞机或飞机组件，安装，飞机或机架和方法的持有人

    公开(公告)号：US20150252824A1

    公开(公告)日：2015-09-10

    申请号：US14636507

    申请日：2015-03-03

    申请人： Airbus Operations GmbH

    发明人： Hermann Benthien ,  Matthias Hegenbart ,  Sheriff Shehata

    IPC分类号： F16B2/02 ,  F16M11/22 ,  F16B11/00

    CPC分类号： F16B2/02 ,  B64C1/406 ,  F16B2/12 ,  F16B11/006 ,  F16B11/008 ,  F16M11/22 ,  Y02T50/46 ,  Y10T156/10

    摘要： A holder for connecting a module to a component of an aircraft or spacecraft includes a first holder portion having a first adhesive face and a second holder portion having a second adhesive face. The first and second holder portions are movable relative to one another in an initial state of the holder such that a portion of the component can be received between the holder portions so as to glue the holder portions to the component by means of an adhesive layer in each case. The holder has two or more guided parts which are movable relative to one another by means of mutually cooperating guide faces in the initial state of the holder. The guide faces are suitably formed for being glued together using an adhesive. The holder can be used to counter peeling stress of an adhesive connection of the holder in the region of the first and/or second adhesive face.

    摘要翻译： 用于将模块连接到飞机或航天器的部件的保持器包括具有第一粘合面的第一保持器部分和具有第二粘合面的第二保持器部分。 第一和第二保持器部分可以在保持器的初始状态下相对于彼此移动，使得部件的一部分可以容纳在保持器部分之间，以便通过粘合剂层将保持器部分粘合到部件上 每个案例。 保持器具有两个或更多个引导部件，它们在保持器的初始状态下可通过相互配合的引导面相对于彼此移动。 引导面适当地形成用于使用粘合剂胶合在一起。 保持器可以用于抵抗在第一和/或第二粘合面的区域中保持器的粘合连接的剥离应力。