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    POWDERED PRIMER FOR RUBBER TO METAL BONDING
    1.
    发明申请
    POWDERED PRIMER FOR RUBBER TO METAL BONDING 有权
    用于橡胶的金属接合用粉末

    公开(公告)号：US20110209822A1

    公开(公告)日：2011-09-01

    申请号：US13127768

    申请日：2009-11-09

    申请人： James R. Halladay

    发明人： James R. Halladay

    IPC分类号： B32B37/12 ,  C08L21/00 ,  B32B37/02 ,  B32B37/06 ,  B32B37/10 ,  B32B37/14

    CPC分类号： C09J121/00 ,  C08K3/22 ,  C08L21/00 ,  C08L61/06 ,  C08L65/00 ,  C08L91/00 ,  C09J161/06 ,  Y10T428/31696 ,  Y10T428/31707

    摘要： A powder primer composition particularly useful as a primer intended to be used in conjunction with an adhesive topcoat in rubber to metal bonding. And a method for bonding an elastomeric substrate to a metallic substrate comprising, applying a powder primer composition onto one of said substrates, wherein the powder primer composition comprises a rubbery polymer and at least one of a phenolic resin and a phenoxy resin, applying an adhesive covercoat to form a coated substrate, contacting the coated substrate with the other of said substrates, and heating the contacted substrates to effect bonding of the metallic substrate to the elastomer.

    摘要翻译： 特别可用作底漆的粉末底漆组合物，用于与橡胶中的粘合剂面漆结合使用以进行金属粘合。 和一种将弹性基材粘合到金属基底上的方法，包括：将粉末底漆组合物施加到所述基底之一上，其中所述粉末底漆组合物包含橡胶状聚合物和酚醛树脂和苯氧基树脂中的至少一种， 覆盖涂层以形成涂覆的基底，使涂覆的基底与另一个所述基底接触，并加热接触的基底以实现金属基底与弹性体的结合。

    ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS
    3.
    发明申请
    ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS 有权
    旋转式飞机轴承用于旋转式飞机运动

    公开(公告)号：US20150198201A1

    公开(公告)日：2015-07-16

    申请号：US12927754

    申请日：2010-11-23

    申请人： James R. Halladay ,  Patrick M. Sheridan ,  Marshall W. Downing ,  Zachary Fuhrer

    发明人： James R. Halladay ,  Patrick M. Sheridan ,  Marshall W. Downing ,  Zachary Fuhrer

    IPC分类号： F16C17/24 ,  F16C43/02 ,  F16C33/24 ,  G01N21/88 ,  B32B37/16 ,  B64D45/00 ,  G01M13/04 ,  F16C17/02 ,  B32B37/14

    CPC分类号： F16C17/246 ,  B32B27/08 ,  B32B27/20 ,  B32B37/144 ,  B32B37/16 ,  B32B2307/4026 ,  B32B2307/422 ,  B32B2307/50 ,  B32B2307/56 ,  B32B2475/00 ,  B32B2605/18 ,  B64C27/35 ,  B64D45/00 ,  F16C17/02 ,  F16C27/02 ,  F16C33/24 ,  F16C41/008 ,  F16C43/02 ,  F16F1/3605 ,  F16F1/40 ,  G01M13/04 ,  G01N21/8803 ,  Y10T29/49696

    摘要： A rotary wing aircraft bearing that provides a constrained relative motion between a first rotary wing aircraft member and a second rotary wing aircraft member. The bearing includes an elastomeric mold bonded laminated bearing stack, the elastomeric mold bonded laminated bearing stack including a plurality of mold bonded alternating layers of nonelastomeric shim member layers and elastomeric shim members layers, the alternating layers having an exterior surface and an interior center distal from the exterior surface. At least one of the elastomeric shim members layers has an interior elastomer region distal from the exterior surface, the interior elastomer region formed an interior cured elastomer composition having at least a first interior optical characteristic ingredient, and an exterior elastomer region encompassing the interior elastomer region, the exterior elastomer region proximate the exterior surface, the exterior elastomer region formed from an exterior cured elastomer composition having at least a second exterior optical characteristic ingredient, the at least second exterior optical characteristic ingredient different than the interior cured elastomer composition first interior optical characteristic ingredient, wherein with an elastomer void crack propagating from the exterior surface inward towards the interior elastomer region and a repeated rotary wing aircraft relative motion between the first rotary wing aircraft member and the second rotary wing aircraft member generates a plurality of interior cured elastomer composition crumbs to be expelled from the elastomer void, the interior cured elastomer composition crumbs optically distinguishable from the exterior cured elastomer composition.

    摘要翻译： 一种在第一旋转翼飞行器构件和第二旋转翼飞行器构件之间提供受限的相对运动的旋翼飞机轴承。 轴承包括弹性体模具粘结的层压轴承堆叠，弹性体模具粘合的层压轴承堆叠包括多个模具粘结的非弹性垫片构件层和弹性垫片构件层的交替层，交替层具有远离外部表面和内部中心 外表面。 弹性垫片构件层中的至少一个具有远离外表面的内部弹性体区域，内部弹性体区域形成内部固化的弹性体组合物，其具有至少第一内部光学特性成分和包围内部弹性体区域的外部弹性体区域 外部弹性体区域，外部弹性体区域由具有至少第二外部光学特征成分的外部固化的弹性体组合物形成，所述至少第二外部光学特性成分不同于内部固化的弹性体组合物的第一内部光学特性 成分，其中弹性体空隙裂纹从内表面向内传播到内部弹性体区域，并且重复的旋转翼飞行器在第一旋转翼飞行器构件和第二旋转翼飞行器构件之间的相对运动产生多叶 内部固化的弹性体组合物碎屑从弹性体空隙排出，内部固化的弹性体组合物与外部固化的弹性体组合物光学上可区分开。

    Mount having integrated damper and load carrying spring
    4.
    发明授权
    Mount having integrated damper and load carrying spring 有权
    安装有集成阻尼器和负载弹簧

    公开(公告)号：US06752389B2

    公开(公告)日：2004-06-22

    申请号：US10020356

    申请日：2001-10-30

    申请人： James R. Halladay ,  Wallace C. Flower ,  Roger Cook

    发明人： James R. Halladay ,  Wallace C. Flower ,  Roger Cook

    IPC分类号： F16F100

    CPC分类号： F16F7/09 ,  F16F13/04

    摘要： A mount comprising a unitary resilient member where the unitary resilient member comprises a spring portion, an intermediate stiffening portion and a damping layer, and the resilient member is compressible and extendible. The resilient member is substantially enclosed by a casing. The mount further includes damping means located in contact with said damping layer, the damping means providing damping in response to compression and extension of said resilient member.

    摘要翻译： 包括单一弹性构件的支架，其中整体弹性构件包括弹簧部分，中间加强部分和阻尼层，并且弹性构件是可压缩和延伸的。 弹性构件基本上被壳体封闭。 所述安装件还包括位于与所述阻尼层接触的阻尼装置，所述阻尼装置响应于所述弹性构件的压缩和延伸而提供阻尼。

    High-temperature fluid mounting
    9.
    发明授权
    High-temperature fluid mounting 失效
    高温流体安装

    公开(公告)号：US6022600A

    公开(公告)日：2000-02-08

    申请号：US873309

    申请日：1992-04-24

    申请人： Warren E. Schmidt ,  Randall S. Wayland ,  James R. Halladay ,  Tejbans S. Kohli

    发明人： Warren E. Schmidt ,  Randall S. Wayland ,  James R. Halladay ,  Tejbans S. Kohli

    IPC分类号： B64D27/26 ,  F16F1/36 ,  F16F9/00 ,  F16F13/08 ,  F16F13/26 ,  B29D22/00

    CPC分类号： F16F13/26 ,  B64D27/26 ,  F16F1/3605 ,  F16F13/08 ,  F16F9/003 ,  F16F9/006 ,  F16F2222/02 ,  Y10T428/1359 ,  Y10T428/3154 ,  Y10T428/31663

    摘要： A mounting (20) which provides superior isolation yet which eliminates damaging edge-induced shear strain (ENT) buildup in the elastomer sections (28) and (30) when exposed to high temperatures by having a first elastomer section (28) loaded in compression and a second elastomer section (30) loaded in shear. Exposing the mounting (20) to elevated temperature environments allows the first elastomer section (28) to expand in height and places the second elastomer section (30) in shear to accommodate the height change. The instant invention compensates for fluid and elastomer expansion due to high temperatures by providing a mechanical type compensator (37) which takes up less space and eliminates the pressure loss associated with air-charged compensators (99). Further, a unique combination of fluorinated fluids and polysiloxane polymer enables the mounting (20) to withstand temperatures of greater than 200 deg F. for extended periods of time.

    摘要翻译： 一种提供优异隔离的安装件（20），其通过使第一弹性体部分（28）承受压缩而暴露于高温时消除了弹性体部分（28）和（30）中的损伤边缘引起的剪切应变（ENT） 和装载在剪切中的第二弹性体部分（30）。 将安装件（20）暴露于升高的温度环境允许第一弹性体部分（28）在高度上膨胀并且将第二弹性体部分（30）放置在剪切中以适应高度变化。 本发明通过提供一种机械式补偿器（37）来补偿由于高温导致的流体和弹性体膨胀，其占用较少的空间并消除与充气补偿器（99）相关联的压力损失。 此外，氟化流体和聚硅氧烷聚合物的独特组合使得安装（20）可以长时间耐受大于200°F的温度。

    Oil-resistant coating compositions
    10.
    发明授权
    Oil-resistant coating compositions 失效
    耐油涂料组合物

    公开(公告)号：US5314955A

    公开(公告)日：1994-05-24

    申请号：US7637

    申请日：1993-01-21

    申请人： James R. Halladay

    发明人： James R. Halladay

    IPC分类号： C09D115/00 ,  C08L61/04 ,  C08L33/18 ,  C08L33/20 ,  C08L61/10

    CPC分类号： C09D115/005

    摘要： A coating composition containing a hydrogenated acrylonitrile-butadiene copolymer, a phenolic resin, a curing component, and a solvent. The coating composition is useful for protecting elastomeric materials from corrosive materials such as oil or fuel. The coating composition is resistant to fatigue and provides for excellent adhesion to both rigid and flexible substrates.

    摘要翻译： 含有氢化丙烯腈 - 丁二烯共聚物，酚醛树脂，固化成分和溶剂的涂料组合物。 涂料组合物可用于保护弹性体材料免受腐蚀性物质如油或燃料的影响。 涂料组合物耐疲劳，并且对刚性和柔性基材提供优异的粘合性。