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    • 5. 发明申请
    • BALANCING DEVICE FOR A ROTATING MEMBER AND ASSOCIATED METHODS
    • 用于旋转成员的平衡装置及相关方法
    • WO2003042650A1
    • 2003-05-22
    • PCT/US2002/036595
    • 2002-11-13
    • LORD CORPORATION
    • ALTIERI, Russell, E.SCHULTE, Thomas, E.SHARP, JeffryHACKETT, Brian, K.
    • G01M1/36
    • G01M1/36F16F15/36Y10T74/2114Y10T74/2127
    • A balancing device (10) including a positionable member (14) associated with a rotating member (12) having an axis (26), wherein the positionable member (14) has a substantially constant mass, and wherein the positionable member (14) is disposed at a first position (14') about the axis (26) of the rotating member (14''). The balancing device (10) also including an actuation device (16) disposed at a distance from the positionable member (14), wherein the actuation device (16) is operable for selectively generating a force, and wherein the force is operable for moving the positionable member (14) from the first position (14') to a second position (14'') about the axis (26) of the rotating member (12), thereby balancing the rotating member (12).
    • 一种平衡装置(10),包括与具有轴线(26)的旋转构件(12)相关联的可定位构件(14),其中所述可定位构件(14)具有基本恒定的质量,并且其中所述可定位构件 设置在围绕旋转构件(14“)的轴线(26)的第一位置(14')处。 所述平衡装置(10)还包括设置在距所述可定位构件(14)一定距离处的致动装置(16),其中所述致动装置(16)可操作以选择性地产生力,并且其中所述力可操作以使 从所述第一位置(14')到所述旋转构件(12)的轴线(26)的第二位置(14“)定位构件(14),从而平衡所述旋转构件(12)。
    • 6. 发明申请
    • CIRCULAR FORCE GENERATOR (CFG) DEVICES, SYSTEMS, AND METHODS HAVING INDIRECTLY DRIVEN IMBALANCED ROTORS
    • 具有独立驱动的不平衡转子的循环发电机(CFG)装置,系统和方法
    • WO2015031768A1
    • 2015-03-05
    • PCT/US2014/053431
    • 2014-08-29
    • LORD CORPORATION
    • HUNTER, Anthony, G.ALTIERI, Russell, E.BRANNAN, Warren, F.JOLLY, Mark, R.
    • B64C27/00F16F15/10F16F15/14F16F15/30
    • F16F15/1464B64C27/001B64C2027/003B64C2027/004F16F7/1005F16F15/30
    • Circular force generator (CFG) devices, systems, and methods are disclosed having indirectly driven imbalanced rotors for generating vibrations and/or imparting vibration control. A CFG device (10) includes a first set of imbalanced rotors (12) disposed about a center point and a second set of imbalanced rotors (12) disposed about the center point. The first set of imbalanced rotors is configured to co-rotate synchronously. The second set of imbalanced rotors is configured to co-rotate synchronously. The first and second sets of imbalanced rotors are configured to create a controllable rotating force vector having a controllable magnitude and phase about the center point. A CFG system includes a controller and one or more CFG devices configured to receive control commands from the controller. A method of generating a force via a CFG device includes receiving a force command and generating a force in response to receiving the force command.
    • 公开了具有用于产生振动和/或施加振动控制的间接驱动的不平衡转子的圆形力发生器(CFG)装置,系统和方法。 CFG装置(10)包括围绕中心点设置的第一组不平衡转子(12)和围绕中心点设置的第二组不平衡转子(12)。 第一组不平衡转子被配置为同步共旋转。 第二组不平衡转子被配置为同步共旋转。 第一组和第二组不平衡转子被配置成产生具有围绕中心点的可控大小和相位的可控旋转力矢量。 CFG系统包括控制器和配置成从控制器接收控制命令的一个或多个CFG设备。 通过CFG装置产生力的方法包括接收力指令并响应于接收到力命令产生力。
    • 7. 发明申请
    • AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD
    • 飞机车辆推进系统监控装置及方法
    • WO2005019030A2
    • 2005-03-03
    • PCT/US2004/007331
    • 2004-03-10
    • LORD CORPORATION
    • ALTIERI, Russell, E.KUHN, James, F.JOLLY, Mark, R.SOUTHWARD, Steve, C.BADRE-ALAM, AskariFOWLER, Leslie, P.
    • B64D
    • G01B7/31B64C29/005B64F5/60
    • Methods and systems for monitoring rotating shafts and couplings in an aircraft vehicle propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vehicle’s dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The misalignment measuring system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
    • 描述了用于监视飞行器车辆推进系统中的旋转轴和联轴器的方法和系统。 测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。 测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机,其中车辆的动态旋转驱动轴系统和联轴器被实时监控。 车轴联轴器未对准测量系统利用多个位置传感器来提供推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。 传感器的相对位置通过结构框架从旋转目标的外部刚性固定。 不对准测量系统驱动轴柔性联轴器涉及飞机车辆操作中旋转轴联轴器的关键性能。 该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。
    • 8. 发明申请
    • AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD
    • 飞机车辆推进系统监控装置及方法
    • WO2004094954A2
    • 2004-11-04
    • PCT/US2004/012477
    • 2004-04-21
    • LORD CORPORATION
    • ALTIERI, Russell, E.KUHN, James, F.JOLLY, Mark, R.SOUTHWARD, Steve, C.BADRE-ALAM, AskariFOWLER, Leslie, P.
    • G01D
    • G01B7/31B64C29/005B64F5/60
    • Methods and systems for monitoring rotating shafts and couplings in an aircraft vehicle propulsion system is described. The measurement system/method provides for accurate and precise monitoring of a rotating shaft flexible coupling in a fixed wing aircraft vehicle propulsion system. The measuring system/method provides for a high reliability short take off vertical landing fixed wing aircraft in which the vehicle's dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular shaft coupling misalignment measuring system utilizes multiple positional sensors to provide highly reliable and precise determination of the dynamic characteristics of the rotating sensor target components of the propulsion system drive shaft. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The misalignment measuring system provides a misalignment measurement of the propulsion system drive shaft flexible coupling which relates to a critical performance of rotating shaft coupling in the operation of an aircraft vehicle. The method/system provides for monitoring a rotating drive shaft system and dynamically measuring a rotating drive shaft coupling in a fixed wing aircraft propulsion system.
    • 描述了用于监视飞行器车辆推进系统中的旋转轴和联轴器的方法和系统。 测量系统/方法可以精确和精确地监测固定翼飞机车辆推进系统中的旋转轴柔性联轴器。 测量系统/方法提供了一种高可靠性的短距离垂直着陆固定翼飞机,其中车辆的动态旋转驱动轴系统和联轴器被实时监控。 车轴联轴器未对准测量系统利用多个位置传感器来提供推进系统驱动轴的旋转传感器目标部件的动态特性的高度可靠和精确的确定。 传感器的相对位置通过结构框架从旋转目标的外部刚性固定。 不对准测量系统提供了推进系统驱动轴柔性联轴器的不对准测量,其涉及在飞行器车辆的操作中旋转轴联轴器的关键性能。 该方法/系统提供用于监视旋转驱动轴系统并动态地测量固定翼飞机推进系统中的旋转驱动轴联轴器。
    • 10. 发明申请
    • HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS
    • 直升机振动控制系统和消除振动的循环发电系统
    • WO2009126608A2
    • 2009-10-15
    • PCT/US2009/039745
    • 2009-04-07
    • LORD CORPORATIONJOLLY, Mark, R.MEYERS, Andrew, D.MELLINGER, DanielIVERS, Douglas, E.BADRE-ALAM, AskariSWANSON, Douglas, A.ALTIERI, Russell, E.
    • JOLLY, Mark, R.MEYERS, Andrew, D.MELLINGER, DanielIVERS, Douglas, E.BADRE-ALAM, AskariSWANSON, Douglas, A.ALTIERI, Russell, E.
    • B64C27/00
    • B64C27/001B64C2027/004
    • A vehicle a nonrotating vehicle body, a rotating machine member, and including a vehicle vibration control system, the vehicle vibration control system including a vehicle vibration control system controller, a vehicle rotating machine member sensor for inputting vehicle rotating machine member data correlating to the relative rotation of the vehicle rotating machine member rotating relative to the nonrotating vehicle body into the vehicle vibration control system controller, at least a first nonrotating vehicle body vibration sensor, the at least first nonrotating vehicle body vibration sensor inputting at least first nonrotating vehicle body vibration sensor data correlating to vehicle vibrations into the vehicle vibration control system controller, at least a first nonrotating vehicle body circular force generator, the at least a first nonrotating vehicle body circular force generator fixedly coupled with the nonrotating vehicle body, the at least first nonrotating vehicle body circular force generator controlled to produce a rotating force with a controllable rotating force magnitude and a controllable rotating force phase, the controllable rotating force magnitude controlled from a minimal force magnitude up to a maximum force magnitude, and with the controllable rotating force phase controlled in reference to the vehicle rotating machine member sensor data correlating to the relative rotation of the vehicle rotating machine member rotating relative to the nonrotating vehicle body wherein the vehicle vibration sensed by the at least first nonrotating vehicle body vibration sensor is reduced.
    • 一种车辆非旋转车体,旋转机械构件,并且包括车辆振动控制系统,所述车辆振动控制系统包括车辆振动控制系统控制器,用于输入与所述相对的相关联的车辆旋转机器构件数据的车辆旋转机构构件传感器 至少第一非旋转车体振动传感器,至少第一非旋转车身振动传感器,其至少输入第一非旋转车体振动传感器,所述至少第一非旋转车体振动传感器 与车辆振动相关的数据与车辆振动控制系统控制器相关联的至少第一非旋转车体圆周力产生器,至少第一非旋转车体圆周力产生器,与非转动车身固定连接,所述至少第一非旋转车体 保监会 受控制的小型力发生器产生具有可控旋转力量级和可控旋转力相位的旋转力,可控旋转力量值由最小力量值直到最大力量值控制,并且可控旋转力相位受控参考 涉及与所述车辆旋转机械构件相对于所述非旋转车体旋转的相对旋转相关联的所述车辆旋转机构传感器数据,其中,所述至少第一非旋转车身振动传感器感测到的车辆振动减小。