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1. 发明申请

WO2012138816A2 ROTARY WING AIRCRAFT INSTRUMENTED MOTION CONTROL BEARINGS 审中-公开
标题翻译：旋转飞行器仪表运动控制轴承
公开(公告)号：WO2012138816A2
公开(公告)日：2012-10-11
申请号：PCT/US2012/032249
申请日：2012-04-05
申请人： ALLRED, Charles , DOWNING, Marshall , FUHRER, Zachary , JOLLY, Mark , SMITH, Matthew , LORD CORPORATION
发明人： ALLRED, Charles , DOWNING, Marshall , FUHRER, Zachary , JOLLY, Mark , SMITH, Matthew
IPC分类号： F16C27/06 , B23P17/00
CPC分类号： F16C27/06 , B64C27/35 , F16F1/41 , Y10T29/49643
摘要： Motion control bearings and methods making such with the capability to monitor properties therein is provided. Devices and methods for creating and using motion control bearings for rotary wing aircraft in particular are disclosed using wireless communication and monitoring of multiple load, motion and health related information items related to the bearing and blade at the wing hub. Static and dynamic blade orientation provides additional information on flight regime, thrust vectors, and gross vehicle weight. Power is provided using kinetic energy power harvesting.
摘要翻译：提供了运动控制轴承和使其具有监控其性能的方法。特别是用于创建和使用用于旋翼飞机的运动控制轴承的装置和方法公开了使用无线通信和监视与翼中心轴承和叶片相关的多个负载，运动和健康相关信息项。静态和动态叶片方向提供有关飞行状态，推力矢量和车辆总重量的更多信息。使用动能收集功率提供动力。

2. 发明申请

WO2012138816A3 ROTARY WING AIRCRAFT INSTRUMENTED MOTION CONTROL BEARINGS 审中-公开
标题翻译：旋转飞行器仪表运动控制轴承
公开(公告)号：WO2012138816A3
公开(公告)日：2014-05-08
申请号：PCT/US2012032249
申请日：2012-04-05
申请人： ALLRED CHARLES , DOWNING MARSHALL , FUHRER ZACHARY , JOLLY MARK , SMITH MATTHEW , LORD CORP
发明人： ALLRED CHARLES , DOWNING MARSHALL , FUHRER ZACHARY , JOLLY MARK , SMITH MATTHEW
IPC分类号： B64C27/35 , F16F1/41
CPC分类号： F16C27/06 , B64C27/35 , F16F1/41 , Y10T29/49643
摘要： Motion control bearings and methods making such with the capability to monitor properties therein is provided. Devices and methods for creating and using motion control bearings for rotary wing aircraft in particular are disclosed using wireless communication and monitoring of multiple load, motion and health related information items related to the bearing and blade at the wing hub. Static and dynamic blade orientation provides additional information on flight regime, thrust vectors, and gross vehicle weight. Power is provided using kinetic energy power harvesting.
摘要翻译：提供了运动控制轴承和使其具有监控其性能的方法。特别是用于创建和使用用于旋翼飞机的运动控制轴承的装置和方法公开了使用无线通信和监视与翼中心轴承和叶片相关的多个负载，运动和健康相关信息项。静态和动态叶片方向提供有关飞行状态，推力矢量和车辆总重量的更多信息。使用动能收集功率提供动力。

3. 发明申请

WO2011062639A3 A ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS 审中-公开
标题翻译：旋转式飞机轴承用于旋转式飞机运动
公开(公告)号：WO2011062639A3
公开(公告)日：2011-10-20
申请号：PCT/US2010003024
申请日：2010-11-23
申请人： LORD CORP , HALLADAY JAMES R , SHERIDAN PATRICK M , DOWNING MARSHALL W , FUHRER ZACHARY
发明人： HALLADAY JAMES R , SHERIDAN PATRICK M , DOWNING MARSHALL W , FUHRER ZACHARY
IPC分类号： B64C27/35 , F16F1/40
CPC分类号： F16C41/008 , B64C27/35 , F16C33/04 , F16F1/406
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：一种旋转翼飞行器轴承，其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。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，靠近外表面的外部弹性体区域，由外部固化的弹性体组合物形成的外部弹性体区域，其具有至少第二外部光学特征成分，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外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可光学地区分开。

4. 发明申请

WO2011062639A9 A ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS 审中-公开
标题翻译：用于旋翼飞机运动的旋翼飞机轴承
公开(公告)号：WO2011062639A9
公开(公告)日：2011-07-21
申请号：PCT/US2010003024
申请日：2010-11-23
申请人： LORD CORP , HALLADAY JAMES R , SHERIDAN PATRICK M , DOWNING MARSHALL W , FUHRER ZACHARY
发明人： HALLADAY JAMES R , SHERIDAN PATRICK M , DOWNING MARSHALL W , FUHRER ZACHARY
IPC分类号： B64C27/35
CPC分类号： F16C41/008 , B64C27/35 , F16C33/04 , F16F1/406
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：提供第一旋翼飞机构件和第二旋翼飞机构件之间受约束的相对运动的旋翼飞机轴承。所述轴承包括弹性体模制结合的叠层轴承叠层，所述弹性体模制结合叠层轴承叠层包括多个非弹性垫片构件层和弹性体垫片构件层的多个模制结合的交替层，所述交替层具有外表面和远离外表面。至少一个弹性垫片构件层具有远离外表面的内部弹性体区域，内部弹性体区域形成为具有至少第一内部光学特性成分的内部固化弹性体组合物，以及包围内部弹性体区域的外部弹性体区域，所述外部弹性体区域靠近所述外部表面，所述外部弹性体区域由外部固化的弹性体组合物形成，所述外部固化的弹性体组合物具有至少第二外部光学特征成分，所述至少第二外部光学特征成分不同于所述内部固化的弹性体组合物其中随着从外表面向内朝向内部弹性体区域传播的弹性体空隙裂缝以及第一旋翼飞行器构件和第二旋翼飞机构件之间的重复的旋翼飞行器相对运动产生一个套筒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碎屑与外部固化的弹性体组合物光学区分。

5. 发明申请

WO2011062639A2 A ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS 审中-公开
标题翻译：用于旋翼飞机运动的旋翼飞机轴承
公开(公告)号：WO2011062639A2
公开(公告)日：2011-05-26
申请号：PCT/US2010/003024
申请日：2010-11-23
申请人： LORD CORPORATION , HALLADAY, James, R. , SHERIDAN, Patrick, M. , DOWNING, Marshall, W. , FUHRER, Zachary
发明人： HALLADAY, James, R. , SHERIDAN, Patrick, M. , DOWNING, Marshall, W. , FUHRER, Zachary
IPC分类号： B64C27/35
CPC分类号： F16C41/008 , B64C27/35 , F16C33/04 , F16F1/406
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：旋翼飞机轴承在第一旋翼飞机构件和第二旋翼飞机构件之间提供约束的相对运动。所述轴承包括弹性体模制结合的叠层轴承叠层，所述弹性体模制结合叠层轴承叠层包括多个非弹性垫片构件层和弹性体垫片构件层的多个模制结合的交替层，所述交替层具有外表面和远离外表面。至少一个弹性垫片构件层具有远离外表面的内部弹性体区域，内部弹性体区域形成为具有至少第一内部光学特性成分的内部固化弹性体组合物，以及包围内部弹性体区域的外部弹性体区域，所述外部弹性体区域靠近所述外部表面，所述外部弹性体区域由外部固化的弹性体组合物形成，所述外部固化的弹性体组合物具有至少第二外部光学特征成分，所述至少第二外部光学特征成分不同于所述内部固化的弹性体组合物其中随着从外表面向内朝向内部弹性体区域传播的弹性体空隙裂缝以及第一旋翼飞行器构件和第二旋翼飞机构件之间的重复的旋翼飞行器相对运动产生一个套筒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碎屑与外部固化的弹性体组合物在光学上可区分开。

6. 发明申请

WO2014036131A1 VIBRATION ISOLATION MEMBER 审中-公开
标题翻译：振动隔离构件
公开(公告)号：WO2014036131A1
公开(公告)日：2014-03-06
申请号：PCT/US2013/057068
申请日：2013-08-28
申请人： LORD CORPORATION , RAWSON, Scott A. , DOWNING, Marshall W. , NEGRO, Mark F.
发明人： RAWSON, Scott A. , DOWNING, Marshall W. , NEGRO, Mark F.
IPC分类号： F16F13/20 , F16F1/373 , F16F1/376 , F16F13/10 , F16F13/14 , F16F15/08 , F16F1/38
CPC分类号： F16F3/0873 , F16F1/3732 , F16F1/41
摘要： A snubbed isolator comprising:an inner member, the inner member (12) having: a lower member (25) including an upper surface (27) and base (32), wherein the base is wider than the upper surface; a stem (24) integral with the lower member, the stem including a top, wherein the top is oppositely positioned from the base; a surface associated with the top of the stem, the surface being capable of bearing load; an outer member (14) positioned outwardly from the inner member, the outer member having a surface that is wider near the base of the lower member and narrower proximate the upper surface of the lower member; an interlock between the inner and outer members; an elastomeric element (16) bonded between the inner and outer members; and at least one snubbing elastomeric element (34) bonded to the inner member and positioned to snub against a mounting structure.
摘要翻译：一种缓冲隔离器，包括：内部构件，所述内部构件（12）具有：包括上表面（27）和底座（32）的下构件（25），其中所述基部比所述上表面宽; 与所述下部构件一体的杆（24），所述杆包括顶部，其中所述顶部与所述基部相对定位; 与杆的顶部相关联的表面，该表面能承受负载; 外部构件（14），其从所述内部构件向外定位，所述外部构件具有在所述下部构件的基部附近更宽的表面，并且在所述下部构件的上表面附近更窄; 内部和外部构件之间的互锁; 粘合在内部和外部构件之间的弹性体元件（16）以及至少一个缓冲弹性体元件（34），其结合到所述内部构件并且定位成与所述安装结构相连。

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