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1. 发明申请

WO2013152300A2 MOTION CONTROLLED HELICOPTER AND ROTATION RATE SWITCHED FLUID LEAD LAG DAMPER 审中-公开
标题翻译：运动控制直升机和旋转速率切换流体导管拉杆阻尼器
公开(公告)号：WO2013152300A2
公开(公告)日：2013-10-10
申请号：PCT/US2013/035468
申请日：2013-04-05
申请人： LORD CORPORATION , FUHRER, Zachary , JOLLY, Mark , MARR, Conor
发明人： FUHRER, Zachary , JOLLY, Mark , MARR, Conor
IPC分类号： B64C27/51
CPC分类号： B64C27/51 , B64C27/32 , F16F9/064 , F16F9/20 , F16F9/504 , F16F13/08 , F16F2230/16
摘要： A method and centrifugal force switching dampers are disclosed for controlling helicopter ground resonance motions and air resonance motions. The helicopter lead-lag damper has a first ground resonance motion damping rate stage and a second air resonance motion damping rate stage. The damper includes a centrifugal force switch. The damper is oriented relative to the rotary wing rotation axis and helicopter blade. An in-flight rotation rate of the centrifugal force switching damper actuates the centrifugal force switch with the damper switching from the ground resonance motion damping rate stage to the second air resonance motion damping rate stage.
摘要翻译：公开了用于控制直升机地面共振运动和空气共振运动的方法和离心力切换阻尼器。直升机牵引滞后阻尼器具有第一接地共振运动阻尼速率级和第二空气谐振运动阻尼速率级。阻尼器包括离心力开关。阻尼器相对于旋转翼旋转轴和直升机叶片定向。离心力切换阻尼器的飞行中旋转速度致动离心力开关，其中阻尼器从地面共振运动阻尼速率级切换到第二空气共振运动阻尼速率级。

2. 发明申请

WO2012021202A2 REAL TIME ACTIVE HELICOPTER VIBRATION CONTROL AND ROTOR TRACK AND BALANCE SYSTEMS 审中-公开
标题翻译：实时有效的直升机振动控制和转子跟踪和平衡系统
公开(公告)号：WO2012021202A2
公开(公告)日：2012-02-16
申请号：PCT/US2011/038043
申请日：2011-05-26
申请人： LORD CORPORATION , JOLLY, Mark , MILLER, Lane , BADRE-ALAM, Askari
发明人： JOLLY, Mark , MILLER, Lane , BADRE-ALAM, Askari
IPC分类号： B64C27/80
CPC分类号： B64C27/001 , B64C27/008 , B64C2027/004
摘要： Rotary wing aircraft electronic control system including a tachometer and a plurality of nonrotating body vibration control sensors outputting at least first nonrotating body vibration sensor data correlating to vibrations. The system includes a plurality of nonrotating body force generators to input a vibration control force into said nonrotating aerostructure body. The system includes a data communications network link linking together the nonrotating body force generators the tachometer sensor, the vibration control sensors, and an actuating force generator rotor track balance electronic controller, the actuating force generator rotor track balance electronic controller including at least a first computer processor with the actuating force generator rotor track controller controlling the nonrotating body force generators to input vibration control forces into the nonrotating aerostructure body and computing a rotor track solution for aircraft rotor blades.
摘要翻译：旋转翼飞行器电子控制系统包括转速计和多个非旋转体振动控制传感器，其输出与振动相关的至少第一非旋转体振动传感器数据。该系统包括多个非旋转体力发生器，用于将振动控制力输入到所述非旋转航空结构体中。该系统包括将非旋转体力发生器，转速计传感器，振动控制传感器和致动力发生器转子轨道平衡电子控制器连接在一起的数据通信网络链路，致动力发生器转子轨道平衡电子控制器至少包括第一计算机处理器，其具有致动力发生器转子轨道控制器，其控制非旋转体力发生器以将振动控制力输入到非旋转航空结构体中并计算用于飞行器转子叶片的转子轨道解决方案。

3. 发明申请

WO2006135405A2 HELICOPTER VIBRATION CONTROL SYSTEM AND ROTARY FORCE GENERATOR FOR CANCELING VIBRATIONS 审中-公开
标题翻译：直升机振动控制系统和旋转发电机取消振动
公开(公告)号：WO2006135405A2
公开(公告)日：2006-12-21
申请号：PCT/US2005/030909
申请日：2005-08-30
申请人： LORD CORPORATION , JOLLY, Mark , HILDEBRAND, Stephen , ALTIERI, Russell , IVERS, Douglas , FERGUSON, Matthew
发明人： JOLLY, Mark , HILDEBRAND, Stephen , ALTIERI, Russell , IVERS, Douglas , FERGUSON, Matthew
IPC分类号： B64C27/00
CPC分类号： F16F15/265 , B64C27/001 , B64C2027/003 , F16F15/22 , F16F15/267
摘要： A helicopter rotating hub mounted vibration control system for a helicopter rotary wing hub having a periodic vibration while rotating at a helicopter operational rotation frequency. The helicopter rotating hub mounted vibration control system includes an annular ring rotary housing attachable to the helicopter rotary wing hub and rotating with the helicopter rotary wing hub at the helicopter operational rotation frequency. The annular ring housing is centered about the rotary wing hub axis of rotation and has an electronics housing cavity subsystem and preferably an adjacent coaxial rotor housing cavity subsystem. The rotor housing cavity subsystem contains a first coaxial frameless AC ring motor having a first rotor with a first imbalance mass and a second coaxial frameless AC ring motor having a second rotor with a second imbalance mass. The electronics housing cavity subsystem contains an electronics control system which receives sensor outputs and electrically controls and drives the first coaxial frameless AC ring motor and the second coaxial frameless AC ring motor such that the first imbalance mass and the second imbalance mass are directly driven at a vibration canceling rotation frequency greater than the helicopter operational rotation frequency wherein the helicopter rotary wing hub periodic vibration is reduced.
摘要翻译：一种直升机旋转轮毂安装的用于直升机旋转翼片的振动控制系统，其具有以直升机操作旋转频率旋转的周期性振动。直升机旋转轮毂安装的振动控制系统包括环形环旋转壳体，其可连接到直升机旋转翼毂并且以直升机操作旋转频率与直升机旋转翼毂一起旋转。环形环壳体围绕旋转翼轮毂旋转轴线居中，并且具有电子器件壳体腔子系统，并且优选地是相邻的同轴转子壳体腔子系统。转子壳体空腔子系统包括具有第一不平衡质量的第一转子和具有第二不平衡质量的第二转子的第二同轴无框架AC环形电动机的第一同轴无框架AC环形电动机。电子设备壳体子系统包含电子控制系统，其接收传感器输出并电控制并驱动第一同轴无框架AC环形电动机和第二同轴无框架AC环形电动机，使得第一不平衡质量块和第二不平衡质量块直接在减振旋转频率大于直升机操作旋转频率，其中直升机旋翼轮毂周期性振动减小。

4. 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。

5. 发明申请

WO2012075236A1 FREQUENCY-DEPENDENT DAMPER AND ROTARY WING SYSTEM 审中-公开
标题翻译：频率依赖阻尼器和旋转摆动系统
公开(公告)号：WO2012075236A1
公开(公告)日：2012-06-07
申请号：PCT/US2011/062806
申请日：2011-12-01
申请人： LORD CORPORATION , FUHRER, Zachary , JOLLY, Mark
发明人： FUHRER, Zachary , JOLLY, Mark
IPC分类号： B64C27/51 , F16F9/20
CPC分类号： B64C27/51 , F16F1/3814 , F16F1/3835 , F16F1/50 , F16F9/0209 , F16F9/064 , F16F9/20 , F16F9/3415 , F16F9/43 , F16F9/5126 , F16F9/54 , F16F13/16 , F16F2228/04 , Y10T29/494 , Y10T29/49615
摘要： A frequency- dependent damper (10) for creating a damping force in response to a variable - frequency disturbance includes an outer damper body (12) having an internal cavity (16), an inner damper body (14) for receiving the variable - frequency disturbance extending into the internal cavity, a first fluid chamber (46) and a second fluid chamber (48) defined inside the internal cavity, a piston (44) separating the first and second fluid chambers, a selected orifice ( 39 ) for transferring fluid between the first and second fluid chambers, and a selected spring element (54) arranged serially between the piston and the inner damper body such that the piston can move relative to the inner damper body through deformation of the spring element.
摘要翻译：用于响应于可变频率干扰产生阻尼力的频率相关阻尼器（10）包括具有内部空腔（16）的外部阻尼器体（12），用于接收可变频率的内部阻尼器本体（14）干扰延伸到内腔中，限定在内腔内部的第一流体室（46）和第二流体室（48），分隔第一和第二流体室的活塞（44），用于输送流体的选定孔在第一和第二流体室之间，以及选定的弹簧元件（54），其串联地布置在活塞和内部阻尼器主体之间，使得活塞可以通过弹簧元件的变形相对于内部阻尼器主体移动。

6. 发明申请

WO2011143377A1 LAND VEHICLES AND SYSTEMS WITH CONTROLLABLE SUSPENSION SYSTEMS 审中-公开
标题翻译：具有可控悬挂系统的陆地车辆和系统
公开(公告)号：WO2011143377A1
公开(公告)日：2011-11-17
申请号：PCT/US2011/036176
申请日：2011-05-12
申请人： LORD CORPORATION , JOLLY, Mark
发明人： JOLLY, Mark
IPC分类号： B60G17/016 , B60G17/08 , B60W50/08 , B60W40/10 , B60W30/04 , G08B21/02 , B60W50/04 , B60W50/02 , B60W40/12 , F16F9/53 , B60G17/0195
CPC分类号： B60G17/0195 , B60G17/0152 , B60G17/0165 , B60G17/0185 , B60G2300/07 , B60G2300/36 , B60G2400/0521 , B60G2400/104 , B60G2400/204 , B60G2400/252 , B60G2400/41 , B60G2400/61 , B60G2401/28 , B60G2500/10 , B60G2600/02 , B60G2600/042 , B60G2600/044 , B60G2600/08 , B60G2600/70 , B60G2800/0124 , B60G2800/24 , B60G2800/704 , B60G2800/9124 , B60W10/22 , B60W30/04 , B60W40/105 , B60W40/109 , B60W50/14 , F16F9/535
摘要： The land vehicle includes a body, a controllable suspension system, the controllable suspension system for controlling suspension movements between the body and land engagers. The land vehicle includes a computer system and suspension sensors located proximate the land engagers for measuring suspension parameters representative of suspension movements between the body and the land engagers and outputting a plurality of suspension sensor measurement output signals. The land vehicle includes controllable force suspension members located proximate the land engagers and the suspension sensors, the controllable force suspension members applying suspension travel forces between the body and the land engagers to control the suspension movements. The land vehicle computer system includes controllable suspension system algorithms for controlling the controllable force suspension members to control vehicle body motion and the suspension movements between the body and the land engagers and inhibit the driver from crossing into an identified impending driver vehicle safety margin.
摘要翻译：陆地车辆包括一个主体，一个可控制的悬挂系统，用于控制车身和地面接地装置之间的悬挂运动的可控悬架系统。陆地车辆包括计算机系统和位于陆地接地装置附近的悬架传感器，用于测量表示车身和陆地接合器之间悬架运动的悬架参数，并输出多个悬架传感器测量输出信号。陆地车辆包括位于陆地接合器和悬架传感器附近的可控力悬挂构件，可控力悬挂构件在身体和陆地接合器之间施加悬挂行程力以控制悬架运动。陆上车辆计算机系统包括用于控制可控力悬挂构件以控制车体运动的控制悬架系统算法和身体与陆地接合器之间的悬挂运动，并且禁止驾驶员进入识别的即将到来的驾驶员车辆安全距离。

7. 发明申请

WO2011137417A2 HELICOPTER HUB MOUNTED VIBRATION CONTROL AND CIRCULAR FORCE GENERATION SYSTEMS FOR CANCELING VIBRATIONS 审中-公开
标题翻译：直升机HUB安装振动控制和循环振动系统取消振动
公开(公告)号：WO2011137417A2
公开(公告)日：2011-11-03
申请号：PCT/US2011/034719
申请日：2011-05-02
申请人： JOLLY, Mark , BLACK, Paul , LORD CORPORATION
发明人： JOLLY, Mark , BLACK, Paul
IPC分类号： B64C27/00
CPC分类号： B64C27/001 , B64C2027/003 , B64C2027/004
摘要： A rotary wing aircraft vehicle vibration control system includes a hub mounted vibration control system mounted to the rotary wing hub with the hub mounted vibration control system rotating with the rotary wing hub driven to rotate about a rotating hub center Z-axis with a transmission. The system includes a sensor for outputting data correlating to relative rotation of the rotating rotary wing hub rotating about the Z axis relative to the nonrotating body, first nonrotating body vibration sensor outputting first nonrotating body vibration sensor data correlating to vibrations. The system includes first/second nonrotating body force generators fixedly coupled with the helicopter body proximate the transmission and oriented relative to the Z-axis, and a link linking together the force generators and the hub mounted vibration control system wherein such are controlled to produce forces wherein the vibration sensed by the first nonrotating body vibration sensor is reduced.
摘要翻译：旋翼飞机车辆振动控制系统包括安装在旋转翼毂上的轮毂安装的振动控制系统，轮毂安装的振动控制系统随着旋转翼毂被驱动以围绕转动的轮毂中心Z轴旋转。该系统包括：传感器，用于输出与绕相对于非旋转体旋转的Z轴旋转的旋转翼片的相对旋转相关的数据;第一非旋转体振动传感器，输出与振动相关的第一非旋转体振动传感器数据。该系统包括第一/第二非旋转体力发生器，其与直升机主体固定地相邻于传动装置并相对于Z轴定向;以及将力发生器和轮毂安装的振动控制系统连接在一起的连杆，其中，其中由所述第一非旋转体振动传感器感测到的振动减小。

8. 发明申请

WO2012138830A1 AIRCRAFT ROTARY WING MOTION CONTROL AND INSTRUMENTED MOTION CONTROL FLUID DEVICE 审中-公开
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：WO2012138830A1
公开(公告)日：2012-10-11
申请号：PCT/US2012/032271
申请日：2012-04-05
申请人： LORD CORPORATION , JOLLY, Mark , FUHRER, Zachary , FOGLE, Robert , CATANZARITE, David
发明人： JOLLY, Mark , FUHRER, Zachary , FOGLE, Robert , CATANZARITE, David
IPC分类号： B64C27/51
CPC分类号： B64C27/51 , B64D2045/0085
摘要： An aircraft rotary wing motion control fluid device (200) providing motion control and with wireless sensing (260) of at least one fluid property inside the fluid device (200) is provided. The wireless sensing system (260) is integrated with at least one of the first (212) and second (214) aircraft rotary wing motion control fluid device bodies. The wireless sensing system (260) includes at least one fluid property sensor (105) in sensing proximity to the at least one fluid chamber (239) and a communications device for wirelessly conveying a measurement made by the at least one fluid property sensor (105) to a remote location.
摘要翻译：提供了提供运动控制和在流体装置（200）内部具有至少一种流体特性的无线感测（260）的飞行器旋转翼运动控制流体装置（200）。无线感测系统（260）与第一（212）和第二（214）飞机旋转翼运动控制流体设备主体中的至少一个集成。无线感测系统（260）包括至少一个感测到至少一个流体室（239）附近的流体特性传感器（105）和用于无线地传送由至少一个流体特性传感器（105））到远程位置。

9. 发明申请

WO2011140016A1 COMPUTER SYSTEM AND PROGRAM PRODUCT FOR BALANCING ROTATING MACHINES 审中-公开
标题翻译：用于平衡旋转机器的计算机系统和程序产品
公开(公告)号：WO2011140016A1
公开(公告)日：2011-11-10
申请号：PCT/US2011/034895
申请日：2011-05-03
申请人： LORD CORPORATION , JOLLY, Mark , OWENS, Jonathan , MILLER, Scott
发明人： JOLLY, Mark , OWENS, Jonathan , MILLER, Scott
IPC分类号： G01M1/30
CPC分类号： G01M1/36 , G01H1/003 , G05B2219/37349 , G05B2219/49177
摘要： Method/system to control a rotating assembly balance control system with at least a first imbalance mass concentration for a rotating assembly having a problematic imbalance while rotating at an operational rotation frequency about a rotation axis. The method includes positioning the imbalance mass concentration around the rotation axis to a balanced rest angular position with the imbalance mass concentration rested at the balanced rest angular position with the rested first imbalance mass concentration at the balance rest angular position providing a counter acting imbalance mass concentration to counter the imbalance. The method includes monitoring at least a first rotating machinery performance health characteristic to diagnose a machine health problem and outputting a machine health problem signal when a machine health problem is diagnosed.
摘要翻译：用于控制具有至少第一不平衡质量浓度的旋转组件平衡控制系统的方法/系统，所述旋转组件在具有围绕旋转轴的操作旋转频率旋转时具有有问题的不平衡。该方法包括将不平衡质量集中在旋转轴周围定位到平衡静止角位置，其中不平衡质量浓度在平衡静止角位置处停止，而在平衡静止角位置处的静止的第一不平衡质量浓度提供反作用的不平衡质量浓度以抵消不平衡。该方法包括至少监视第一旋转机械性能健康特征以诊断机器健康问题并在诊断机器健康问题时输出机器健康问题信号。

10. 发明申请

WO2018195053A1 METHODS AND SYSTEMS FOR MEASURING PARAMETERS OF ROTATING SHAFTS AND COUPLINGS 审中-公开
公开(公告)号：WO2018195053A1
公开(公告)日：2018-10-25
申请号：PCT/US2018/027933
申请日：2018-04-17
申请人： LORD CORPORATION
发明人： KAKALEY, Daniel , ALTIERI, Russell , JOLLY, Mark , ZACCARDO, Victor
IPC分类号： G01D5/14 , G01D5/347 , G01B21/24 , G01B21/26 , G01L3/10 , G01L3/12 , G01B7/31 , G01B7/312
摘要： Systems and methods for measuring displacement parameters of rotating shafts and couplings are disclosed. In some aspects, a measurement system includes a shaft extended in a longitudinal direction and a target wheel configured to rotate with the shaft. The target wheel includes sensor targets circumferentially distributed around the target wheel. Some of the targets are slanted in the longitudinal direction and some of the targets are parallel to the longitudinal direction. The measurement system includes a sensor array including at least three sensors mounted radially around the shaft and configured to detect the sensor targets as the target wheel rotates with the shaft. The measurement system includes a controller configured to receive sensor signals from the sensors and determine, based on the sensor signals, at least an axial displacement measurement of the shaft in the longitudinal direction and a radial displacement measurement of the shaft.

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