HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS
    1.
    发明申请
    HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS 审中-公开
    直升机振动控制系统和消除振动的循环发电系统

    公开(公告)号:WO2009126608A3

    公开(公告)日:2009-12-17

    申请号:PCT/US2009039745

    申请日:2009-04-07

    CPC classification number: B64C27/001 B64C2027/004

    Abstract: A vehicle (520) a nonrotating vehicle body (524), a rotating machine member (522), and including a vehicle vibration control system (409), the vehicle vibration control system including a controller (411), a vehicle rotating machine member sensor (552) 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 (554), for inputting at least first nonrotating vehicle body vibration sensor data correlating to vehicle vibrations into the controller, at least a first nonrotating vehicle body circular force generator (530), fixedly coupled with the nonrotating vehicle body and controlled to produce a rotating force with a controllable rotating force magnitude and a controllable rotating force phase, wherein the vehicle vibration sensed by the at least first nonrotating vehicle body vibration sensor is reduced.

    Abstract translation: 车辆(520),非旋转车体(524),旋转机械部件(522),并且包括车辆振动控制系统(409),所述车辆振动控制系统包括控制器(411),车辆旋转机构传感器 (552),用于将与所述车辆旋转机构相对于所述非旋转动力车身旋转的相对旋转相关的车辆旋转机构部件数据输入到所述车辆振动控制系统控制器中,至少第一非旋转车体振动传感器(554),其用于 将与车辆振动相关的至少第一非旋转车身振动传感器数据输入到所述控制器中,至少第一非旋转车体圆周力产生器(530),其与所述非旋转车体固定地联接并被控制以产生具有可控旋转的旋转力 力大小和可控旋转力相位,其中由至少第一非线性感测的车辆振动 车身振动传感器减少。

    HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS
    2.
    发明申请
    HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS 审中-公开
    直升机振动控制系统和消除振动的循环发电系统

    公开(公告)号:WO2009126608A2

    公开(公告)日:2009-10-15

    申请号:PCT/US2009/039745

    申请日:2009-04-07

    CPC classification number: B64C27/001 B64C2027/004

    Abstract: 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.

    Abstract translation: 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。

    HELICOPTER HUB MOUNTED VIBRATION CONTROL AND CIRCULAR FORCE GENERATION SYSTEMS FOR CANCELING VIBRATIONS
    4.
    发明申请
    HELICOPTER HUB MOUNTED VIBRATION CONTROL AND CIRCULAR FORCE GENERATION SYSTEMS FOR CANCELING VIBRATIONS 审中-公开
    直升机HUB安装振动控制和循环发电系统取消振动

    公开(公告)号:WO2009126626A2

    公开(公告)日:2009-10-15

    申请号:PCT/US2009039773

    申请日:2009-04-07

    CPC classification number: B64C27/001 B64C2027/003 B64C2027/005

    Abstract: A rotary wing aircraft including a vehicle vibration control system. The vehicle vibration control system includes a rotating hub mounted vibration control system, the rotating hub mounted vibration control system mounted to the rotating rotary wing hub with the rotating hub mounted vibration control system rotating with the rotating rotary wing hub. The vehicle vibration control system includes a rotary wing aircraft member sensor for outputting rotary wing aircraft member data correlating to the relative rotation of the rotating rotary wing hub member rotating relative to the nonrotating body, at least a first nonrotating body vibration sensor, the at least first nonrotating body vibration sensor outputting at least first nonrotating body vibration sensor data correlating to vibrations, at least a first nonrotating body circular force generator, the at least a first nonrotating body circular force generator fixedly coupled with the nonrotating body, a distributed force generation data communications network link, the distributed force generation data communications system network link linking together at least the first nonrotating body circular force generator and the rotating hub mounted vibration control system wherein the rotating hub mounted vibration control system and the first nonrotating body circular force generator communicate force generation vibration control data through the distributed force generation data communications network, the at least first nonrotating 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 rotary wing aircraft member sensor data correlating to the relative rotation of the rotating rotary wing hubrotating relative to the nonrotating body wherein the vibration sensed by the at least first nonrotating body vibration sensor is reduced.

    Abstract translation: 一种包括车辆振动控制系统的旋翼飞机。 车辆振动控制系统包括旋转轮毂安装的振动控制系统,旋转轮毂安装的振动控制系统安装到旋转的旋翼轮毂上,旋转轮毂安装的振动控制系统与旋转的旋翼轮毂一起旋转。 车辆振动控制系统包括旋转翼飞行器构件传感器,用于输出与旋转的旋翼轮毂构件相对于非旋转体相对旋转相关的旋转翼飞行器构件数据,至少第一非旋转体振动传感器,至少 第一非旋转体振动传感器,至少输出与振动相关的第一非旋转体振动传感器数据,至少第一非旋转体圆周力产生器,与所述非旋转体固定连接的所述至少第一非旋转体圆周力产生器,分布力产生数据 通信网络链路,分布式力产生数据通信系统网络链路至少连接在第一非旋转体圆周力产生器和旋转轮毂安装的振动控制系统之间,其中旋转毂安装的振动控制系统和第一非旋转体圆周力产生器com 通过分布式力产生数据通信网络发出振动控制数据,所述至少第一非旋转体圆周力产生器被控制以产生具有可控旋转力大小和可控旋转力相位的旋转力,所述可控旋转力幅度由 相对于与旋转的旋转旋翼相对于非旋转体的旋转旋翼相对旋转的旋转翼飞行器构件传感器数据来控制可控旋转力相位,其中由 所述至少第一非旋转体振动传感器被减小。

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