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1. 发明申请

WO2015089404A2 REDUNDANT ACTIVE VIBRATION AND NOISE CONTROL SYSTEMS AND METHODS 审中-公开
标题翻译：冗余有源振动和噪声控制系统和方法
公开(公告)号：WO2015089404A2
公开(公告)日：2015-06-18
申请号：PCT/US2014070034
申请日：2014-12-12
申请人： LORD CORP
发明人： SWANSON DOUGLAS A
IPC分类号： B64D27/26
CPC分类号： F16F15/002 , B06B1/16 , B64C27/001 , B64C2027/004 , G05B15/02
摘要： Redundant active vibration and noise control systems and methods are provided, which include safety-critical systems and methods. In one embodiment, a safety-critical active vibration control system (SCAVCS) is provided, which includes a plurality of digital buses, a force generator, at least one sensor and at least one system parameter. The at least one force generator is in electronic communication with at least two digital buses. The force generator includes a pair of unbalanced masses, at least one motor, at least one microprocessor, at least one speed sensor, at least one accelerometer, and at least one power input. The at least one sensor is in electronic communication with each of the digital buses and with each of the microprocessors. The at least one system parameter is in electronic communication with each of the digital buses and each of the microprocessors.
摘要翻译：提供冗余主动振动和噪声控制系统和方法，其中包括安全关键系统和方法。在一个实施例中，提供了安全关键的主动振动控制系统（SCAVCS），其包括多个数字总线，力生成器，至少一个传感器和至少一个系统参数。该至少一个力发生器与至少两个数字总线进行电子通信。力发生器包括一对不平衡质量块，至少一个电动机，至少一个微处理器，至少一个速度传感器，至少一个加速度计和至少一个功率输入。至少一个传感器与每个数字总线和每个微处理器进行电子通信。该至少一个系统参数与每个数字总线和每个微处理器进行电子通信。

2. 发明申请

WO2009126608A3 HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEM FOR CANCELING VIBRATIONS 审中-公开
标题翻译：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
申请人： LORD CORP , JOLLY MARK R , MEYERS ANDREW D , MELLINGER DANIEL , IVERS DOUGLAS E , BADRE-ALAM ASKARI , SWANSON DOUGLAS A , ALTIERI RUSSELL E
发明人： JOLLY MARK R , MEYERS ANDREW D , MELLINGER DANIEL , IVERS DOUGLAS E , BADRE-ALAM ASKARI , SWANSON DOUGLAS A , ALTIERI RUSSELL E
IPC分类号： B64C27/00
CPC分类号： B64C27/001 , B64C2027/004
摘要： 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.
摘要翻译：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。

3. 发明申请

WO2009126626A2 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
申请人： LORD CORP , JOLLY MARK R , MEYERS ANDREW D , MELLINGER DANIEL , IVERS DOUGLAS E , BADRE-ALAM ASKARI , SWANSON DOUGLAS A , ALTIERI RUSSEL E
发明人： JOLLY MARK R , MEYERS ANDREW D , MELLINGER DANIEL , IVERS DOUGLAS E , BADRE-ALAM ASKARI , SWANSON DOUGLAS A , ALTIERI RUSSEL E
IPC分类号： B64C27/00
CPC分类号： B64C27/001 , B64C2027/003 , B64C2027/005
摘要： 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.
摘要翻译：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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