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1. 发明授权

US08752784B2 Aircraft rotary wing motion control and instrumented motion control fluid device 有权
标题翻译：飞机旋翼运动控制和仪表运动控制流体装置
公开(公告)号：US08752784B2
公开(公告)日：2014-06-17
申请号：US13439980
申请日：2012-04-05
申请人： Mark R. Jolly , Zachary Fuhrer , Robert E. Fogle , David M. Catanzarite
发明人： Mark R. Jolly , Zachary Fuhrer , Robert E. Fogle , David M. Catanzarite
IPC分类号： B64C27/64
CPC分类号： B64C27/51 , B64D2045/0085
摘要： An aircraft rotary wing motion control fluid device providing motion control and with wireless sensing of at least one fluid property inside the fluid device is provided. The wireless sensing system is integrated with at least one of the first and second aircraft rotary wing motion control fluid device bodies. The wireless sensing system includes at least one fluid property sensor in sensing proximity to the at least one fluid chamber and a communications device for wirelessly conveying a measurement made by the at least one fluid property sensor to a remote location.
摘要翻译：提供一种提供运动控制并且在流体装置内部具有至少一种流体特性的无线感测的飞行器旋转翼运动控制流体装置。该无线感测系统与第一和第二飞行器旋转翼运动控制流体装置主体中的至少一个集成。无线感测系统包括至少一个感测与至少一个流体室接近的流体特性传感器和用于将由至少一个流体特性传感器制成的测量无线传送到远程位置的通信装置。

2. 发明申请

US20120256055A1 AIRCRAFT ROTARY WING MOTION CONTROL AND INSTRUMENTED MOTION CONTROL FLUID DEVICE 有权
标题翻译：飞机旋转运动控制和仪器运动控制流体装置
公开(公告)号：US20120256055A1
公开(公告)日：2012-10-11
申请号：US13439980
申请日：2012-04-05
申请人： Mark R. Jolly , Zachary Fuhrer , Robert E. Fogle , David M. Catanzarite
发明人： Mark R. Jolly , Zachary Fuhrer , Robert E. Fogle , David M. Catanzarite
IPC分类号： B64C13/20 , F04D29/32
CPC分类号： B64C27/51 , B64D2045/0085
摘要： An aircraft rotary wing motion control fluid device providing motion control and with wireless sensing of at least one fluid property inside the fluid device is provided. The wireless sensing system is integrated with at least one of the first and second aircraft rotary wing motion control fluid device bodies. The wireless sensing system includes at least one fluid property sensor in sensing proximity to the at least one fluid chamber and a communications device for wirelessly conveying a measurement made by the at least one fluid property sensor to a remote location.
摘要翻译：提供一种提供运动控制并且在流体装置内部具有至少一种流体特性的无线感测的飞行器旋转翼运动控制流体装置。该无线感测系统与第一和第二飞行器旋转翼运动控制流体装置主体中的至少一个集成。无线感测系统包括至少一个感测与至少一个流体室接近的流体特性传感器和用于将由至少一个流体特性传感器制成的测量无线传送到远程位置的通信装置。

3. 发明申请

US20080069695A1 ROTARY WING AIRCRAFT ROTARY LEAD LAG DAMPER 有权
标题翻译：旋转翼飞机旋转导杆拉杆阻尼器
公开(公告)号：US20080069695A1
公开(公告)日：2008-03-20
申请号：US11754673
申请日：2007-05-29
申请人： Peter Jones , Zachary Fuhrer
发明人： Peter Jones , Zachary Fuhrer
IPC分类号： B64C27/54
CPC分类号： B64C27/51 , F16F9/145
摘要： The invention provides a rotary damper for controlling helicopter motions. The rotary damper includes an outer canister with an inner paddle wheel receiving cavity which receives an inner paddle wheel with upper and lower elastomeric tubular intermediate members between the inner paddle wheel and the outer canister. The canister and inner paddle wheel form neighboring variable volume chambers in liquid communication through liquid damping conduits. A clockwise rotation of the inner paddle wheel about the center of rotation axis relative to the outer canister pumps damper liquid from a second variable volume chamber through a first liquid conduit towards a first variable volume chamber, and a counterclockwise rotation of the paddle wheel relative to the outer canister pumps the damper liquid from the first variable volume chamber through the first liquid conduit towards the second variable volume chamber with the elastomeric tubular intermediate members providing for the relative rotation and containing the damper liquid in the damper.
摘要翻译：本发明提供一种用于控制直升机运动的旋转阻尼器。旋转阻尼器包括具有内桨轮容纳腔的外筒，其在内桨叶轮和外筒之间接收具有上和下弹性体管状中间构件的内桨轮。罐和内桨轮通过液体阻尼管道形成液体连通的相邻可变容积室。内侧叶轮围绕旋转轴线的中心相对于外部罐泵顺时针旋转，将来自第二可变容积室的液体通过第一液体导管朝向第一可变容积室进行阻尼，并且相对于桨叶的逆时针旋转外罐将来自第一可变体积室的阻尼液从第一液体导管朝向第二可变容积室泵送，弹性体管状中间构件提供相对旋转并将阻尼液体容纳在阻尼器中。

4. 发明授权

US08356977B2 Rotary wing aircraft rotary lead lag damper 有权
标题翻译：旋翼飞机旋转牵引阻尼器
公开(公告)号：US08356977B2
公开(公告)日：2013-01-22
申请号：US11754673
申请日：2007-05-29
申请人： Peter J. Jones , Zachary Fuhrer
发明人： Peter J. Jones , Zachary Fuhrer
IPC分类号： B64C27/51 , F16F9/14
CPC分类号： B64C27/51 , F16F9/145
摘要： The rotary damper for controlling helicopter motions includes an outer canister with an inner paddle wheel receiving cavity which receives an inner paddle wheel with upper and lower elastomeric tubular intermediate members between the inner paddle wheel and the outer canister. The canister and inner paddle wheel form neighboring variable volume chambers in liquid communication through liquid damping conduits. A clockwise rotation of the inner paddle wheel about the center of rotation axis relative to the outer canister pumps damper liquid from a second variable volume chamber through a first liquid conduit towards a first variable volume chamber, and a counterclockwise rotation of the paddle wheel relative to the outer canister pumps the damper liquid from the first variable volume chamber through the first liquid conduit towards the second variable volume chamber with the elastomeric tubular intermediate members providing for the relative rotation and containing the damper liquid in the damper.
摘要翻译：用于控制直升机运动的旋转阻尼器包括具有内桨轮容纳腔的外筒，其接纳内桨轮，其具有在内桨轮和外筒之间的上弹性体管管中间构件和下弹性体管状中间构件。罐和内桨轮通过液体阻尼管道形成液体连通的相邻可变容积室。内侧叶轮围绕旋转轴线的中心相对于外部罐泵顺时针旋转，将来自第二可变容积室的液体通过第一液体导管朝向第一可变容积室进行阻尼，并且相对于桨叶的逆时针旋转外罐将来自第一可变体积室的阻尼液从第一液体导管朝向第二可变容积室泵送，弹性体管状中间构件提供相对旋转并将阻尼液体容纳在阻尼器中。

5. 发明申请

US20150198201A1 ROTARY WING AIRCRAFT BEARING FOR ROTARY WING AIRCRAFT MOTIONS 有权
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：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。

6. 发明授权

US09068621B1 Rotary wing aircraft bearing for rotary wing aircraft motions 有权
标题翻译：旋翼飞机轴承用于旋翼飞机运动
公开(公告)号：US09068621B1
公开(公告)日：2015-06-30
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： F16F7/00 , F16F1/40 , F16F1/36 , F16C41/00
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。

7. 发明申请

US20120257847A1 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：US20120257847A1
公开(公告)日：2012-10-11
申请号：US13439913
申请日：2012-04-05
申请人： Charles J. Allred , Marshall W. Downing , Zachary Fuhrer , Mark R. Jolly , Matthew A. Smith
发明人： Charles J. Allred , Marshall W. Downing , Zachary Fuhrer , Mark R. Jolly , Matthew A. Smith
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。

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