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1. 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。

2. 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。

3. 发明申请

WO2009055007A2 DISTRIBUTED ACTIVE VIBRATION CONTROL SYSTEMS AND ROTARY WING AIRCRAFT WITH SUPPRESSED VIBRATIONS 审中-公开
标题翻译：分布式主动振动控制系统和具有抑制振动的旋转式飞机
公开(公告)号：WO2009055007A2
公开(公告)日：2009-04-30
申请号：PCT/US2008012081
申请日：2008-10-24
申请人： LORD CORP , MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
发明人： MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： An aircraft with at least one rotating machine creating troublesome vibrations, the aircraft comprised of an aerostructure, the aircraft including: a power source, the power source outputting a plurality of electromagnetic force generator power outputs, the aerostructure including a plurality of distributed actiye vibration control system sites, at least a first distributed active vibration electromagnetic force generator, the first distributed active vibration electromagnetic force generator including a first distributed electronic control system and a first electromagnetically driven mass, the first distributed active vibration electromagnetic force generator fixed to the aerostructure at a first distributed active vibration control system site, at least a second distributed active vibration electromagnetic force generator, the second distributed active vibration electromagnetic force generator including a second distributed electronic control system and a second electromagnetically driven mass, the second distributed active vibration electromagnetic force generator fixed to the aerostructure at a second distributed active vibration control system site, a plurality of electrical power distribution lines, the electrical power distribution lines connecting the electromagnetic force generators with the power source with the electromagnetic force generator power outputs outputted to the electromagnetic force generators, a distributed force generator data communications network, the distributed force generator data communications system network linking together the at least first and second distributed electronic control systems wherein the distributed electronic control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.
摘要翻译：一种具有至少一个旋转机器的飞机产生麻烦的振动，该飞行器由航空结构组成，飞行器包括：电源，电源输出多个电磁力发生器功率输出，该航空结构包括多个分布式动力学振动控制系统站点，至少第一分布式主动振动电磁力发生器，所述第一分布式主动振动电磁力发生器包括第一分布式电子控制系统和第一电磁驱动质量块，所述第一分布式主动振动电磁力发生器固定在所述空气结构第一分布式主动振动控制系统现场，至少第二分布式主动振动电磁力发生器，所述第二分布式主动振动电磁力发生器包括第二分布式电子控制系统和第二电磁第二分布式主动振动电磁力发生器在第二分布式主动振动控制系统现场固定到航空结构，多个电力分配线，电力分配线将电磁力发生器与电源连接，电磁输出到电磁力发生器的力发电机功率输出，分布式力发生器数据通信网络，分布式力发生器数据通信系统网络将至少第一和第二分布式电子控制系统连接在一起，其中分布式电子控制系统将力发电机振动控制数据通过分布式力发生器数据通信网络独立于电力配电线路，以尽量减少麻烦的振动。

4. 发明申请

WO2009055007A3 DISTRIBUTED ACTIVE VIBRATION CONTROL SYSTEMS AND ROTARY WING AIRCRAFT WITH SUPPRESSED VIBRATIONS 审中-公开
标题翻译：分布式主动振动控制系统和具有抑制振动的旋转式飞机
公开(公告)号：WO2009055007A3
公开(公告)日：2009-07-30
申请号：PCT/US2008012081
申请日：2008-10-24
申请人： LORD CORP , MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
发明人： MARK R JOLLY , BADRE-ALAM ASKARI , ALTIERI RUSSELL , MEYERS ANDREW D
IPC分类号： B64C27/00
CPC分类号： B64C27/001 , B64C2027/004 , B64C2027/005 , F16F15/002 , F16F15/223
摘要： An aircraft (20) with at least one rotating machine (22) including: a power source (26), outputting a plurality of electromagnetic force generator power outputs, an aerostructure (24) including a plurality of distributed actiye vibration control system sites, at least a first distributed active vibration electromagnetic force generator (30), including a first distributed electronic control system (32) and a first electromagnetically driven mass (34), the first force generator fixed to the aerostructure at a first site (28), at least a second distributed active vibration electromagnetic force generator including a second distributed electronic control system and a second electromagnetically driven mass, the second force generator fixed to the aerostructure at a second site, a plurality of electrical power distribution lines (40), connecting the electromagnetic force generators with the power source-with the power outputs outputted to the electromagnetic force generators, a distributed force generator data communications network (50) linking together the at least first. and second distributed electronic control systems wherein the control systems communicate force generator vibration control data through the distributed force generator data communications network independently of the electrical power distribution lines to minimize the troublesome vibrations.
摘要翻译：一种具有至少一个旋转机器（22）的飞机（20），包括：输出多个电磁力发生器功率输出的电源（26），包括多个分布式活动振动控制系统位置的航空结构（24），至少一个第一分布式主动振动电磁力发生器（30），其包括第一分布式电子控制系统（32）和第一电磁驱动质量块（34），所述第一力发生器在第一位置（28）处固定到所述航空结构，至少一个第二分布式主动振动电磁力发生器，其包括第二分布式电子控制系统和第二电磁驱动质量块，所述第二力发生器固定在第二场所的航空结构，多个配电线路（40）具有电源的力发生器 - 输出到电磁力发生器的功率输出，分布式f 所述发电机数据通信网络（50）至少连接在一起。以及第二分布式电子控制系统，其中控制系统通过分布式力发生器数据通信网络与电力分配线路独立地传递力发生器振动控制数据，以最小化麻烦的振动。

5. 发明申请

WO2015195664A3 ACTIVE TORSIONAL DAMPER FOR ROTATING SHAFTS 审中-公开
标题翻译：主动扭矩阻尼器
公开(公告)号：WO2015195664A3
公开(公告)日：2016-03-10
申请号：PCT/US2015036029
申请日：2015-06-16
申请人： LORD CORP
发明人： NORRIS MARK A , BADRE-ALAM ASKARI , EDEAL DAVID , O'NEIL DANIEL , MEYERS ANDREW D
IPC分类号： F16F15/00 , B60K1/00 , B60P3/00 , E21B43/26 , F16F15/18
CPC分类号： E21B43/26 , E21B17/073 , E21B47/00 , F04B11/00 , F04B19/22 , F04B23/00 , F04B49/065 , F16F15/002 , F16F15/18
摘要： Systems and methods are disclosed herein that include providing an active torsion damper control system that includes a rotatable component (206) and a rotatable measurement interface (302) disposed on the rotatable component, the rotatable measurement interface having at least one torsional strain gauge configured to measure a strain of the rotatable component, a torque management (306) computer configured to determine a resonant frequency of the rotatable component and a corrective torque needed to be applied to the rotatable component to excite the resonant frequency as a function of the measured strain, and a correction motor (308) configured to impart the corrective torque on the rotatable component.
摘要翻译：本文公开的系统和方法包括提供主动扭力阻尼器控制系统，其包括可旋转部件（206）和设置在可旋转部件上的可旋转测量接口（302），所述可旋转测量接口具有至少一个扭转应变计，其被配置为测量可旋转部件的应变;扭矩管理（306）计算机，其被配置为确定可旋转部件的共振频率以及需要施加到可旋转部件以根据所测量的应变激发谐振频率的校正扭矩，以及校正马达（308），其被配置为将所述校正扭矩赋予所述可旋转部件。

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