公开(公告)号：US4054617A

公开(公告)日：1977-10-18

申请号：US651959

申请日：1976-01-23

申请人： John G. Papalos ,  James M. Kelly

发明人： John G. Papalos ,  James M. Kelly

IPC分类号： C14C3/18 ,  C07F9/09

CPC分类号： C14C3/18

摘要： Leather treating compositions are prepared which comprise condensed or polymeric alkyl phenol phosphates generally and more particularly a phenol-alkylphenol condensate which is subsequently alkoxylated and phosphated. These compositions may be utilized for leather processing, and specifically for: retanning, lubricating, and imparting water resistance to chrome and/or mineral tanned leather. Additionally, these compositions may be used to effect modifications of base mineral tannages for the purpose of dyeing, bleaching, and fatliquoring leather.

摘要翻译： 制备皮革处理组合物，其通常包含稠合或聚合的烷基酚磷酸盐，更特别是酚烷基酚缩合物，其随后被烷氧基化和磷酸化。 这些组合物可用于皮革加工，特别用于：复鞣，润滑和赋予铬和/或矿物鞣皮革耐​​水性。 此外，这些组合物可用于对染色，漂白和加脂皮革的目的进行基础矿物鞣制的改性。

公开(公告)号：US07387277B2

公开(公告)日：2008-06-17

申请号：US11027570

申请日：2004-12-29

申请人： Jan A. Kordel ,  Richard B. Tanner ,  Ian C. Burford ,  Victor A. Munsen ,  Daniel E. McGinty ,  Scott N. Rampton ,  Bruce R. Fox ,  James M. Kelly ,  Miles O. Johnson

发明人： Jan A. Kordel ,  Richard B. Tanner ,  Ian C. Burford ,  Victor A. Munsen ,  Daniel E. McGinty ,  Scott N. Rampton ,  Bruce R. Fox ,  James M. Kelly ,  Miles O. Johnson

IPC分类号： B64C3/20

CPC分类号： B64C3/00

摘要： Aircraft wing assemblies having both composite and metal panels are disclosed. In one embodiment, a wing assembly includes a support structure, an upper panel assembly formed from a metal material and coupled to the support structure, and a lower panel assembly formed from a composite material and coupled to the support structure. The metal material may be aluminum, titanium, or any other suitable metal, and the composite material may be a carbon fiber reinforced plastic (CFRP) material or other suitable composite material. In another embodiment, the upper panel assembly includes a downwardly depending first web portion, and the lower panel assembly includes an upwardly depending second web portion, the second web portion being proximate the first web portion, and an interface member of an isolating material is disposed between the first and second web portions.

摘要翻译： 公开了具有复合材料和金属板的飞机机翼组件。 在一个实施例中，翼组件包括支撑结构，由金属材料形成并联接到支撑结构的上面板组件，以及由复合材料形成并联接到支撑结构的下部面板组件。 金属材料可以是铝，钛或任何其它合适的金属，并且复合材料可以是碳纤维增强塑料（CFRP）材料或其它合适的复合材料。 在另一个实施例中，上面板组件包括向下悬垂的第一腹板部分，并且下面板组件包括向上悬垂的第二腹板部分，第二腹板部分靠近第一腹板部分，并且设置隔离材料的接口构件 在第一和第二纤维网部分之间。

公开(公告)号：US4718206A

公开(公告)日：1988-01-12

申请号：US904457

申请日：1986-09-08

申请人： Edward R. Fyfe ,  James M. Kelly

发明人： Edward R. Fyfe ,  James M. Kelly

IPC分类号： E04H9/02

CPC分类号： E04H9/021 ,  B60G2204/4504

摘要： Apparatus for limiting the effect of vibrations between a building structure and its foundation is disposed between the foundation and the building structure. A plate is fixedly secured to a lower surface of the building structure. A hollow member having a rectangular cross-section is fixedly secured to the plate. An elastomeric bearing is disposed between and fixed to the hollow member and an upper surface of a foundation. A cable, anchored to the foundation, is centrally disposed within the elastomeric bearing and the hollow member, and has a stop attached to the free end thereof. The stop is disposed within the hollow member. The stop serves to limit horizontal and vertical movement of the elastomeric bearing. In a modified apparatus for limiting the effect of vibrations between the building structure and the foundation, an elastomeric material is disposed between the stop and the base of the hollow member to distribute a load applied by the stop through the deflection of the elastomeric material.

摘要翻译： 用于限制建筑结构与其基础之间的振动影响的装置设置在地基和建筑结构之间。 板固定地固定到建筑结构的下表面。 具有矩形横截面的中空构件牢固地固定在板上。 弹性体轴承设置在中空构件之间并固定到中空构件和基础的上表面上。 锚固在基础上的电缆居中地设置在弹性体轴承和中空构件内，并具有连接到其自由端的止动件。 止动件设置在中空构件内。 止动件用于限制弹性轴承的水平和垂直运动。 在用于限制建筑结构和地基之间的振动的影响的改进装置中，弹性体材料设置在中空构件的止挡件和基座之间，以分布由止动件施加的弹性材料的挠曲所产生的载荷。

公开(公告)号：US10119641B1

公开(公告)日：2018-11-06

申请号：US15369022

申请日：2016-12-05

申请人： James M. Kelly

发明人： James M. Kelly

IPC分类号： F16L27/06 ,  F16L47/18

摘要： A flexible pipe connector, including a tubular housing, a sleeve arranged within the tubular housing, the sleeve including a first end having a first spherical inner surface, the first spherical inner surface having a first inner radius, and a second end having a second spherical inner surface, the second spherical inner surface having a second inner radius, a first tubular member including a first spherical end and a first cylindrical end, the first spherical end having a first outer radius, smaller than the first inner radius, the first spherical end pivotably arranged in the first end, and a second tubular member including a second spherical end and a second cylindrical end, the second spherical end having a second outer radius, smaller than the second inner radius, the second spherical end pivotably arranged in the second end.

公开(公告)号：US20080023585A1

公开(公告)日：2008-01-31

申请号：US11027570

申请日：2004-12-29

申请人： Jan A. Kordel ,  Richard B. Tanner ,  Ian C. Burford ,  Victor A. Munsen ,  Daniel E. McGinty ,  Scott N. Rampton ,  Bruce R. Fox ,  James M. Kelly ,  Miles O. Johnson

发明人： Jan A. Kordel ,  Richard B. Tanner ,  Ian C. Burford ,  Victor A. Munsen ,  Daniel E. McGinty ,  Scott N. Rampton ,  Bruce R. Fox ,  James M. Kelly ,  Miles O. Johnson

IPC分类号： B64C3/00

CPC分类号： B64C3/00

摘要： Aircraft wing assemblies having both composite and metal panels are disclosed. In one embodiment, a wing assembly includes a support structure, an upper panel assembly formed from a metal material and coupled to the support structure, and a lower panel assembly formed from a composite material and coupled to the support structure. The metal material may be aluminum, titanium, or any other suitable metal, and the composite material may be a carbon fiber reinforced plastic (CFRP) material or other suitable composite material. In another embodiment, the upper panel assembly includes a downwardly depending first web portion, and the lower panel assembly includes an upwardly depending second web portion, the second web portion being proximate the first web portion, and an interface member of an isolating material is disposed between the first and second web portions.

摘要翻译： 公开了具有复合材料和金属板的飞机机翼组件。 在一个实施例中，翼组件包括支撑结构，由金属材料形成并联接到支撑结构的上面板组件，以及由复合材料形成并联接到支撑结构的下部面板组件。 金属材料可以是铝，钛或任何其它合适的金属，并且复合材料可以是碳纤维增强塑料（CFRP）材料或其它合适的复合材料。 在另一个实施例中，上面板组件包括向下悬垂的第一腹板部分，并且下面板组件包括向上悬垂的第二腹板部分，第二腹板部分靠近第一腹板部分，并且设置隔离材料的接口构件 在第一和第二纤维网部分之间。

公开(公告)号：US5930843A

公开(公告)日：1999-08-03

申请号：US33168

申请日：1998-03-02

申请人： James M. Kelly

发明人： James M. Kelly

IPC分类号： A42B3/04 ,  A41D13/00 ,  A42B3/00

CPC分类号： A42B3/0473 ,  A41D13/0512

摘要： A cervical spine protective helmet and shoulder harness assembly. The helmet and shoulder-harness assembly includes a yoke or shoulder pad having a central opening for the wearer's head to pass therethrough. A protective helmet is pivotally supported over the central opening. Arcuate tracks allow the head of the wearer to be turned from side to side. Stops within the pivoting joints supporting the helmet limit neck flexion and extension. Stops at the ends of these tracks limit neck torsion. Neck compression is limited by the rigidity of the uprights supporting the helmet.

摘要翻译： 颈椎防护头盔和肩带组件。 头盔和肩带组件包括具有用于穿用者头部的中心开口的轭或肩垫。 保护性头盔枢转地支撑在中央开口上。 弧形轨道允许佩戴者的头部从一侧到另一侧转动。 在支撑头盔的枢转关节内停止限制颈部弯曲和伸展。 在这些轨道的末端停止限制颈部扭转。 颈部压缩受支撑头盔的立柱刚度的限制。

公开(公告)号：US5904010A

公开(公告)日：1999-05-18

申请号：US872775

申请日：1997-06-10

申请人： Ahmad E. Javid ,  James M. Kelly ,  Jerome L. Sackman

发明人： Ahmad E. Javid ,  James M. Kelly ,  Jerome L. Sackman

IPC分类号： E04H9/02

CPC分类号： E04H9/022

摘要： A fiber reinforced elastomeric seismic isolation bearing and method protects structures and their contents from the damaging effects of earthquakes. The bearing is a block of a specially designed composite material consisting of an elastomer matrix in which are embedded, through its depth, high stiffness pretensioned fibers extending in various horizontal directions. This produces a device which has a very low horizontal stiffness compared to its vertical stiffness. The isolator is mounted between, and connected to, the structure it supports and the foundation upon which it bears. Because of its low horizontal stiffness the bearing decouples the structure which it supports from the damaging horizontal components of the ground motion associated with an earthquake while the benign vertical motion is transmitted into the structure almost unchanged. Thus, during an earthquake, the structure, which typically will rest on several supporting isolators, and its contents experience small acceleration, velocity and deformation. The isolation bearing and method includes the use of elastomeric laminae with parallel pretensioned fibers, forming a series of cells which are vulcanized into an adherent connection and positioned to be connected between a structure and a structure foundation.

摘要翻译： 一种纤维增强弹性地震隔震轴承和方法保护结构及其内容免受地震的破坏作用。 轴承是由弹性体基体组成的特殊设计的复合材料的块，其中通过其深度嵌入在各个水平方向上延伸的高刚度预拉伸纤维。 这产生与其垂直刚度相比具有非常低的水平刚度的装置。 隔离器安装在其所支撑的结构之间并连接到其所支撑的结构上，并与其连接在一起。 由于其低水平刚度，轴承将其支撑的结构与地震相关的地面运动的损伤水平分量解耦，而良性垂直运动传递到结构中几乎没有变化。 因此，在地震期间，通常将搁置在几个支撑隔离器上的结构，并且其内容物经受小的加速度，速度和变形。 隔离轴承和方法包括使用具有平行预拉伸纤维的弹性体层，形成一系列细胞，其被硫化成粘合连接并定位成连接在结构和结构基础之间。

公开(公告)号：US5014474A

公开(公告)日：1991-05-14

申请号：US342351

申请日：1989-04-24

申请人： Edward R. Fyfe ,  James M. Kelly

发明人： Edward R. Fyfe ,  James M. Kelly

IPC分类号： E02D31/08 ,  E04H9/02

CPC分类号： E04H9/022 ,  E02D31/08 ,  B60G2202/143 ,  B60G2204/125 ,  B60G2204/4504

摘要： Apparatus for limiting the effect of vibrations between a structure and its foundation having two types of elastomeric load bearing pads. One pad has the capability of absorbing vertically and horizontally applied forces. The other pad has the capability of accommodating sliding motion between the structure and the foundation and additionally to absorb horizontally applied forces. The apparatus includes restraining means for limiting horizontal and vertical displacement of the structure with respect to the foundation for reducing failure of the elastomeric load bearing pads resulting from deformation caused by the applied forces.

摘要翻译： 用于限制具有两种类型的弹性承载垫的结构与其基础之间振动的影响的装置。 一个垫具有吸收垂直和水平施加力的能力。 另一个垫具有容纳结构和基础之间的滑动运动的能力，并且另外吸收水平施加的力。 该装置包括用于限制结构相对于基座的水平和垂直位移的限制装置，用于减少由所施加的力引起的变形导致的弹性体承载垫的失效。

公开(公告)号：USD293045S

公开(公告)日：1987-12-08

申请号：US702796

申请日：1985-02-19

申请人： Michael T. Merritt ,  James M. Kelly

设计人： Michael T. Merritt ,  James M. Kelly

公开(公告)号：US3995115A

公开(公告)日：1976-11-30

申请号：US663307

申请日：1967-08-25

申请人： James M. Kelly

发明人： James M. Kelly

IPC分类号： H04K1/04

CPC分类号： H04K1/04

摘要： The communication of confidential information is generally accomplished by transforming applied message waves into an unintelligible form prior to transmission. Such a transformation may be accomplished by scrambling the applied message waves in either the frequency or time domain. Scrambling, per se, does not render a signal satisfactorily unintelligible. In order to overcome this deficiency, scrambling techniques are utilized jointly with vocoder and selective speech processing methods. In a voice-excited vocoder, the spectrum channel control signals are scrambled in the frequency domain and the baseband signal is severely center clipped in order to enhance unintelligibility. A high degree of privacy during transmission is thus obtained with negligible effect upon the quality or intelligibility of speech synthesized by an authorized recipient.

摘要翻译： 机密信息的通信通常通过在传输之前将应用的消息波变换成难以理解的形式来实现。 这种变换可以通过在频域或时域中加扰应用的消息波来实现。 扰乱本身并不能令人难以置信的令人难以置信的信号。 为了克服这个缺陷，加扰技术与声码器和选择性语音处理方法联合使用。 在语音激励语音编码器中，频谱信道控制信号在频域中被加扰，并且基带信号被严格中心限制，以增强不可理解性。 因此，在由授权的接收者合成的语音的质量或可理解性上可以忽略不计的影响，从而获得传输期间的高度隐私。