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公开(公告)号：US08172195B2
公开(公告)日：2012-05-08
申请号：US10948599
申请日：2004-09-23
IPC分类号： F16M11/20
CPC分类号： B60P7/0815 , B63B29/06
摘要： A tiedown system foundation adapter system provides greater flexibility in spotting equipment on a support surface. An adapter module includes a plate assembly that drops into a slotted track system and is slid along the track system until it fits into an attachment point that restrains the plate assembly from vertical pullout and motion transverse to the track. The plate assembly is then locked into position to restrain it from further translation along the track. An equipment fitting is translatably mounted with respect to the upper surface and attaches to a complementary attachment fitting on the bottom of a piece of equipment. By locating a number of modules in desired locations along the tracks and locating the equipment fitting in each module, a piece of equipment can be oriented in virtually any position and location in the space to be furnished. A deck system for a flush floor is also provided.
摘要翻译： 系统基础适配器系统在支撑表面上的设备点检中提供了更大的灵活性。 适配器模块包括板组件，其落入开槽轨道系统中并且沿着轨道系统滑动，直到其适合于限制板组件垂直拉出并横向于轨道的运动的附接点。 然后将板组件锁定到位以限制其沿着轨道的进一步平移。 设备配件相对于上表面可平移地安装并且附接到一件设备的底部上的互补附件。 通过将轨道上的多个模块定位在期望的位置并将设备配件定位在每个模块中，一件设备可以被定位在要被提供的空间中的几乎任何位置和位置。 还提供了一个平齐地板的甲板系统。
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公开(公告)号：US07854410B2
公开(公告)日：2010-12-21
申请号：US11803720
申请日：2007-05-15
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/128 , B64C2201/165 , B64C2201/185 , B64C2201/201 , F42B10/14 , F42B10/143 , F42B10/56 , F42B12/365 , F42B15/08 , F42B15/105
摘要： An unmanned aerial vehicle mounts a payload section to an air delivery vehicle. The air delivery vehicle includes deployable wings and tail fins for gliding or powered flight. A set of propeller blades are provided for powered flight. The propeller blades are mounted for movement from a stowed position to deployed position extending radially from the fuselage for powered flight.
摘要翻译： 无人驾驶飞行器将空载部分安装到空气输送车辆。 空气输送车辆包括用于滑行或动力飞行的可展开的翼和尾翼。 一组螺旋桨叶片用于动力飞行。 螺旋桨叶片安装成从收起位置移动到从机身径向延伸用于动力飞行的展开位置。
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公开(公告)号：US20120216699A1
公开(公告)日：2012-08-30
申请号：US12220910
申请日：2008-07-28
CPC分类号： F42B12/06 , F42B12/207 , F42B12/74 , F42B14/064 , F42B33/00
摘要： A composite penetrator or projectile is formed of a core of uniaxial tungsten wires embedded in a matrix material. The core may be overwrapped to improve hoop or radial strength. The core is mounted in a sabot for use as an ordnance projectile. The penetrator is frangible and can include a detonatable energetic resin to provide a self-destruct capability. A pultrusion process is provided to manufacture the penetrator.
摘要翻译： 复合穿透器或抛射体由嵌入基质材料的单轴钨丝芯形成。 芯可以被包裹以改善箍或径向强度。 核心安装在一个sabot作为弹药弹药使用。 穿透器是易碎的，并且可以包括可引爆的能量树脂以提供自毁能力。 提供拉挤成型工艺来制造穿透器。
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4.发明授权公开(公告)号：US08053068B2
公开(公告)日：2011-11-08
申请号：US12080090
申请日：2008-03-31
申请人： Jerome P. Fanucci , Pavel Bystricky
发明人： Jerome P. Fanucci , Pavel Bystricky
IPC分类号： D04H1/00
CPC分类号： F16F15/04 , E04H9/028 , F16F2224/0258 , Y10T428/249924 , Y10T428/249927 , Y10T428/24994
摘要： A shock and vibration isolator device has one or more connecting elements of a superelastic shape memory alloy composite material extending between a base member, configured to mount to a structure or ground, and a mounting member, configured to support equipment or machinery. The superelastic shape memory alloy composite material is formed of a plurality of superelastic wires embedded in an elastomeric matrix material.
摘要翻译： 冲击和隔振装置具有一个或多个超弹性形状记忆合金复合材料的连接元件，所述超弹性形状记忆合金复合材料在构造成安装到结构或地面的基底构件和构造成支撑设备或机械的安装构件之间延伸。 超弹性形状记忆合金复合材料由嵌入弹性体基体材料中的多个超弹性线形成。
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公开(公告)号：US07926677B2
公开(公告)日：2011-04-19
申请号：US12409812
申请日：2009-03-24
CPC分类号： B65D45/02 , B65D21/0204
摘要： A modular packaging system of containers each having a generally tubular, hollow container body of a fiber-reinforced composite material with cooperative mating interlocking elements extending axially along its length. The interlocking elements allow the containers to be stacked and palletized in a stable manner. An interface between a closure mechanism and the container body provides a good seal and prevents fraying or brooming of the fiber-reinforced composite material at the end face of the body.
摘要翻译： 一种容器的模块化包装系统，每个容器均具有通常为管状的纤维增强复合材料的中空容器体，其具有沿其长度轴向延伸的协同配合互锁元件。 互锁元件允许容器以稳定的方式堆放和堆垛。 闭合机构和容器主体之间的界面提供良好的密封，并防止在身体的端面处的纤维增强复合材料的磨损或破裂。
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公开(公告)号：US20100039900A1
公开(公告)日：2010-02-18
申请号：US11985319
申请日：2007-11-14
申请人： Michael McAleenan , Ray Nagem , Darcy Hornberger
发明人： Michael McAleenan , Ray Nagem , Darcy Hornberger
IPC分类号： G10K11/00
摘要： A volumetric displacement transducer is provided for generating acoustic signals. The transducer housing incorporates at least one pair of opposed plates mounted for radial vibration. A driving mechanism is coupled to the opposed plates for driving the plates simultaneously in opposition to each other at a desired frequency, whereby an acoustic signal is radiated into a medium, such as water, surrounding the housing.
摘要翻译： 提供体积位移传感器用于产生声信号。 换能器壳体包括至少一对相对的板，用于径向振动。 驱动机构联接到相对的板上，用于以期望的频率相互同时地驱动板，由此将声信号辐射到围绕壳体的诸如水的介质中。
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公开(公告)号：US20100012774A1
公开(公告)日：2010-01-21
申请号：US11803720
申请日：2007-05-15
IPC分类号： B64C3/56
CPC分类号： B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/082 , B64C2201/102 , B64C2201/128 , B64C2201/165 , B64C2201/185 , B64C2201/201 , F42B10/14 , F42B10/143 , F42B10/56 , F42B12/365 , F42B15/08 , F42B15/105
摘要： An unmanned aerial vehicle mounts a payload section to an air delivery vehicle. The air delivery vehicle includes deployable wings and tail fins for gliding or powered flight. A set of propeller blades are provided for powered flight. The propeller blades are mounted for movement from a stowed position to deployed position extending radially from the fuselage for powered flight.
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8.发明授权Impact resistant, thin ply composite structures and method of manufacturing same 失效耐冲击，薄层复合结构及其制造方法公开(公告)号：US07407901B2
公开(公告)日：2008-08-05
申请号：US11331437
申请日：2006-01-12
申请人： Pavel Bystricky , Jerome P. Fanucci
发明人： Pavel Bystricky , Jerome P. Fanucci
CPC分类号： D03D15/00 , B82Y30/00 , C04B35/83 , C04B2235/5256 , C04B2235/5268 , C04B2235/5288 , D03D15/0088 , D10B2101/12 , D10B2401/063 , Y10T428/249927 , Y10T428/249945 , Y10T428/31504 , Y10T428/31511 , Y10T428/31594 , Y10T442/3041 , Y10T442/335 , Y10T442/3488 , Y10T442/3496 , Y10T442/3683
摘要： A reinforced carbon-carbon (RCC) composite material has improved impact resistance. The RCC composite material is formed from a fiber reinforcement of layers or plies of thin ply carbon fiber fabric impregnated with a carbon matrix. Carbon nanotube reinforcement in the matrix further improves impact resistance. The stacking arrangement of the plies of the thin ply fabric also further improves impact resistance.
摘要翻译： 增强碳 - 碳（RCC）复合材料具有改善的耐冲击性。 RCC复合材料由浸渍有碳基质的薄层碳纤维织物的层或层的纤维增强材料形成。 基体中的碳纳米管增强剂进一步提高耐冲击性。 薄层织物的层叠的堆叠布置还进一步提高耐冲击性。
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9.发明申请Lattice fin for missiles or other fluid-born bodies and method for producing same 失效用于导弹或其他液体体的物体的翅片及其制造方法公开(公告)号：US20030173459A1
公开(公告)日：2003-09-18
申请号：US10313222
申请日：2002-12-06
IPC分类号： B64C001/00 , B64C003/00 , B64C005/00
CPC分类号： F42B10/143 , B64C5/12 , B64C9/34 , Y10T29/49885 , Y10T29/49895
摘要： A method for the manufacture of lattice fins for fluid-born bodies is provided. In one embodiment, lattice fins having a metallic cell structure are manufactured from strips or sheets of metal. In another embodiment, composite lattice fins are manufactured from a log assembly of elongated mandrels covered with a fiber reinforced composite material. After curing, individual fins are sliced from the log assembly. Upon removal of the mandrels, a cell structure is obtained. Combinations of the two embodiments are also provided.
摘要翻译： 提供了一种用于制造用于流体体的晶格翅片的方法。 在一个实施例中，具有金属电池结构的格子片由条或金属片制成。 在另一个实施例中，复合网格翅片由覆盖有纤维增强复合材料的细长心轴的对数组件制造。 固化后，将各个翅片从原木组件切片。 在去除心轴时，获得电池结构。 还提供了两个实施例的组合。
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10.发明授权Buckling restrained brace for structural reinforcement and seismic energy dissipation and method of producing same 失效屈曲约束支架用于结构加固和地震能量消耗及其生产方法公开(公告)号：US07707788B2
公开(公告)日：2010-05-04
申请号：US11725582
申请日：2007-03-19
申请人： Pavel Bystricky , Jerome P. Fanucci
发明人： Pavel Bystricky , Jerome P. Fanucci
CPC分类号： E04H9/021 , E04H9/028 , Y10T29/49623
摘要： A buckling restrained brace includes a deformable core contained within an outer casing. Ends of the core protrude from the casing for connection to a frame or other structure. A length of the deformable core between its ends, referred to as the gauge or yielding section, is capable of deforming during an earthquake or blast loading. The gauge section is differentially heat treated from the ends so that the gauge section has a lower yield strength than the ends. The casing provides containment of the core to prevent buckling of the core. A metal foil interface or unbonding layer is provided between the deformable core and the casing so that the deformable core does not bind to the casing. The buckling restrained brace provides significant performance improvements over prior art BRBs coupled with simplified assembly.
摘要翻译： 屈曲约束支架包括容纳在外壳内的可变形芯。 芯的端部从壳体突出以连接到框架或其他结构。 其可变形芯在其端部之间的长度（称为量规或屈服部分）能够在地震或爆炸加载期间变形。 仪表部分从端部进行差别热处理，使得量规部分的屈服强度比端部低。 壳体提供了芯的容纳以防止芯的屈曲。 在可变形的芯和壳体之间设置有金属箔界面或非粘合层，使得可变形的芯不结合到壳体。 相对于现有技术的BRB与简化组装相结合，弯曲限制支架提供显着的性能改进。
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