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1. 发明授权

US06213442B1 Isolation system for isolation tables and the like 失效
标题翻译：隔离台隔离系统等
公开(公告)号：US06213442B1
公开(公告)日：2001-04-10
申请号：US09168545
申请日：1998-10-08
申请人： Douglas E. Ivers , Leslie P. Fowler , Russell E. Altieri , Stephen F. Buchner
发明人： Douglas E. Ivers , Leslie P. Fowler , Russell E. Altieri , Stephen F. Buchner
IPC分类号： F16M1300
CPC分类号： F16F15/03
摘要： An isolation system includes a housing that contains an electromagnet, a sensor and a controller. The housing is mounted underneath a table top of an isolation table (or other structure requiring isolation from a second body), and target elements, such as permanent magnets, are associated with the frame of the table in proximity to the housing. The sensor provides an input signal representative of motion of the table to the controller, which generates a control signal for the electromagnet to produce a force acting on the target element. The housing can be attached to the table top with magnets, which facilitate installation. The housing provides a unit that is simple to install, is unobtrusive, and advantageous for retrofitting existing isolation tables.
摘要翻译：隔离系统包括容纳电磁体，传感器和控制器的壳体。壳体安装在隔离台（或需要与第二主体隔离的其他结构）的桌面下方，并且目标元件（例如永久磁铁）与桌子的靠近壳体的框架相关联。传感器提供表示桌子运动的输入信号给控制器，该控制器产生用于电磁体产生作用在目标元件上的力的控制信号。外壳可以用磁铁安装在桌面上，便于安装。外壳提供了一个安装简单，不引人注意的单元，有利于改造现有的隔离台。

2. 发明授权

US08162606B2 Helicopter hub mounted vibration control and circular force generation systems for canceling vibrations 有权
标题翻译：直升机轮毂安装的振动控制和圆形力产生系统，用于消除振动
公开(公告)号：US08162606B2
公开(公告)日：2012-04-24
申请号：US12419775
申请日：2009-04-07
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： F04D29/26 , F01D5/26 , B64C11/00
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
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, and a distributed force generation data communications network link.
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，以及分布力产生数据通信网络链接。

3. 发明授权

US07925392B2 Aircraft vehicular propulsion system monitoring device and method 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US07925392B2
公开(公告)日：2011-04-12
申请号：US12099461
申请日：2008-04-08
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
IPC分类号： G01B7/24 , G01L3/00 , G06F15/00
CPC分类号： B64C29/005 , B64F5/60 , G01B7/31
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft 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 vertical propulsion 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 collar misalignment measuring system of the invention provide 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.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴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，其中垂直推进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对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。本发明的套环未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的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。

4. 发明授权

US06954685B2 Aircraft vehicular propulsion system monitoring device and method 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US06954685B2
公开(公告)日：2005-10-11
申请号：US10421325
申请日：2003-04-23
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
IPC分类号： B64C29/00 , B64D45/00 , B64F5/00 , G01B7/31 , G01M13/02
CPC分类号： G01B7/31 , B64C29/005 , B64F5/60
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft 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 vertical propulsion 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 collar misalignment measuring system of the invention provide 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.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴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，其中垂直推进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对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。本发明的套环未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的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。

5. 发明申请

US20120136533A1 HELICOPTER VIBRATION CONTROL SYSTEM AND CIRCULAR FORCE GENERATION SYSTEMS FOR CANCELING VIBRATIONS 有权
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：US20120136533A1
公开(公告)日：2012-05-31
申请号：US12971026
申请日：2010-12-17
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： G06F19/00 , G05D15/00 , B64C27/473 , G05D19/00 , F16F7/00 , F16F7/10
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
摘要： A rotary wing aircraft including a vehicle vibration control system. 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, 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 hub rotating 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，至少至少第一非旋转体圆周力产生器，至少第一非旋转体圆周力产生器，其与所述非旋转体固定连接，所述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，至少第一非旋转体振动传感器，主体圆形力发生器被控制以产生具有可控旋转力量级和可控旋转力相位的旋转力，可控旋转力量值从最小力量控制到最大力量值，并且可控旋转力相位被控制在参考旋转翼型飞行器构件传感器数据与旋转的旋转翼型轮毂相对于非旋转体相对旋转，其中由至少第一非旋转体振动传感器感测的振动减小。

6. 发明授权

US09073627B2 Helicopter vibration control system and circular force generation systems for canceling vibrations 有权
标题翻译：直升机振动控制系统和用于消除振动的圆形力产生系统
公开(公告)号：US09073627B2
公开(公告)日：2015-07-07
申请号：US12971026
申请日：2010-12-17
申请人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
发明人： Mark R. Jolly , Andrew D. Meyers , Daniel Mellinger , Douglas E. Ivers , Askari Badre-Alam , Douglas A. Swanson , Russell E. Altieri
IPC分类号： G06F19/00 , G05D15/00 , G05D19/00 , B64C27/00 , F16F15/22
CPC分类号： B64C27/001 , B64C2027/003 , F16F15/22 , G05D19/02 , Y10S416/50
摘要： A rotary wing aircraft including a vehicle vibration control system. 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, 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 hub rotating 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，至少至少第一非旋转体圆周力产生器，至少第一非旋转体圆周力产生器，其与所述非旋转体固定连接，所述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，至少第一非旋转体振动传感器，主体圆形力发生器被控制以产生具有可控旋转力量级和可控旋转力相位的旋转力，可控旋转力量值从最小力量控制到最大力量值，并且可控旋转力相位被控制在参考旋转翼型飞行器构件传感器数据与旋转的旋转翼型轮毂相对于非旋转体相对旋转，其中由至少第一非旋转体振动传感器感测的振动减小。

7. 发明申请

US20090055129A1 AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US20090055129A1
公开(公告)日：2009-02-26
申请号：US12099461
申请日：2008-04-08
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
IPC分类号： G01B7/24 , G06F15/00
CPC分类号： B64C29/005 , B64F5/60 , G01B7/31
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft 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 vertical propulsion 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 collar misalignment measuring system of the invention provide 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.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴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，其中垂直推进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对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。本发明的套环未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的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

US20110204882A1 AIRCRAFT VEHICULAR PROPULSION SYSTEM MONITORING DEVICE AND METHOD 审中-公开
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US20110204882A1
公开(公告)日：2011-08-25
申请号：US13083647
申请日：2011-04-11
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler , Matthew Ferguson
IPC分类号： G01R33/06
CPC分类号： B64C29/005 , B64F5/60 , G01B7/31
摘要： Methods/systems for monitoring an aircraft propulsion system is described. The measurement system/method provides for accurate and precise monitoring of rotating members in an aircraft vehicle propulsion system. The measuring system/method provides for a high reliability aircraft in which the propulsion dynamically rotating drive shaft system and couplings are monitored in real time. The vehicular 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 aircraft system. The relative position of the sensors is rigidly fixed externally from the rotating targets with a structural frame. The 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 an aircraft.
摘要翻译：描述了用于监视飞行器推进系统的方法/系统。测量系统/方法提供对飞行器车辆推进系统中的旋转构件的准确和精确的监测。测量系统/方法提供了一种高可靠性飞机，其中推进动态旋转驱动轴系统和联轴器被实时监控。车辆测量系统利用多个位置传感器来提供对航空器系统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。测量系统提供推进系统驱动轴柔性联轴器的不对中测量，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/系统提供用于监测旋转驱动轴系统并动态地测量飞行器中的旋转驱动轴联轴器。

9. 发明授权

US07389162B2 Aircraft vehicular propulsion system monitoring device and method 失效
标题翻译：飞机车辆推进系统监控装置及方法
公开(公告)号：US07389162B2
公开(公告)日：2008-06-17
申请号：US11224563
申请日：2005-09-12
申请人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
发明人： Russell E. Altieri , James F. Kuhn , Mark R. Jolly , Steve C. Southward , Askari Badre-Alam , Leslie P. Fowler
IPC分类号： G01B7/31 , G01M13/02 , G06F19/00
CPC分类号： G01B7/31 , B64C29/005 , B64F5/60
摘要： Methods and systems for monitoring rotating shaft shafts and couplings in an aircraft 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 vertical propulsion 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 collar misalignment measuring system of the invention provide 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.
摘要翻译：描述了用于监测飞行器推进系统中的旋转轴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，其中垂直推进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对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。本发明的套环未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的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. 发明授权

US08360728B2 Aircraft with transient-discriminating propeller balancing system 有权
标题翻译：具有瞬态辨别螺旋桨平衡系统的飞机
公开(公告)号：US08360728B2
公开(公告)日：2013-01-29
申请号：US11870891
申请日：2007-10-11
申请人： Steve F. Hildebrand , Russell E. Altieri , Wayne Winzenz
发明人： Steve F. Hildebrand , Russell E. Altieri , Wayne Winzenz
IPC分类号： B64C11/00 , G01M1/38
CPC分类号： B64C11/008 , G01M1/36
摘要： A system for balancing an aircraft propeller system receives a vibration signal from the aircraft propeller system and determines whether the vibration signal indicates a transient vibration condition. If it is determined that the vibration signal does not indicate a transient condition, the system enables a balance correction controller. The controller generates a balance correction signal based on the vibration signal, and balances the aircraft propeller system in response to the balance correction signal if the balance correction controller is enabled.
摘要翻译：用于平衡飞行器螺旋桨系统的系统从飞行器螺旋桨系统接收振动信号，并确定振动信号是否表示瞬时振动条件。如果确定振动信号不表示瞬态状态，则系统启用平衡校正控制器。控制器基于振动信号产生平衡校正信号，并且如果平衡校正控制器被使能，则平衡飞行器螺旋桨系统以响应平衡校正信号。

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