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    Active chaff
    3.
    发明授权
    Active chaff 有权
    活动谷壳

    公开(公告)号：US08537048B2

    公开(公告)日：2013-09-17

    申请号：US12239434

    申请日：2008-09-26

    申请人： Michael J. Dunn ,  Brian Kenneth Kormanyos ,  Thomas H. Friddell

    发明人： Michael J. Dunn ,  Brian Kenneth Kormanyos ,  Thomas H. Friddell

    IPC分类号： G01S7/38

    CPC分类号： F42B12/382 ,  G01S7/38 ,  G01S7/495 ,  H01Q1/22 ,  H01Q1/28

    摘要： An active chaff may be released by an aircraft to assist the aircraft in evading at least one of radar detection and a missile. The active chaff may include a signal generator, a signal spreading device, a microprocessor, a power source, and a substantially high-drag aerodynamic envelope. The signal generator may emit a signal to assist the aircraft in evading radar detection and/or a missile. The signal spreading device may spread the generated signal. The microprocessor may control the signal generator and the signal spreading device. The power source may power the signal generator and the microprocessor. Each of the signal generator, signal spreading device, microprocessor, and power source may be located on or within the substantially high-drag aerodynamic envelope.

    摘要翻译： 飞机可以释放一个活动的糠壳，以协助飞机逃避雷达检测和导弹中的至少一个。 活动谷壳可以包括信号发生器，信号扩展装置，微处理器，电源和基本上高阻力的空气动力学外壳。 信号发生器可以发出信号以帮助飞机逃避雷达检测和/或导弹。 信号扩展装置可以扩展生成的信号。 微处理器可以控制信号发生器和信号扩展装置。 电源可以为信号发生器和微处理器供电。 信号发生器，信号扩展装置，微处理器和电源中的每一个可以位于基本上高阻力的空气动力学外壳上或内部。

    Two-wheel drive two-wheeled vehicle
    4.
    发明授权
    Two-wheel drive two-wheeled vehicle 失效
    两轮驱动两轮车

    公开(公告)号：US08056693B2

    公开(公告)日：2011-11-15

    申请号：US12356665

    申请日：2009-01-21

    申请人： Steven J. Christini ,  Michael J. Dunn

    发明人： Steven J. Christini ,  Michael J. Dunn

    IPC分类号： F16D41/24 ,  F16D21/00

    CPC分类号： B62M23/00 ,  B62M17/00

    摘要： A two-wheel drive motorcycle having a drive train that supplies power to the front wheel and includes a series of rigid shafts or other internalized drive systems. The front wheel drive consists of components located on the axis of steering within the head tube and positioned symmetrically in a counterbalancing fashion within the front fork in order to counteract the torque reactions from the rotating front wheel drive while providing a full range of steering. The front wheel drive lengthens and shortens in parallel with the shock-absorbing front fork. An engagement clutch, a one-way hub, and torque limiting clutch operatively engaged with the front wheel drive are also disclosed.

    摘要翻译： 具有向前轮供电并包括一系列刚性轴或其他内部驱动系统的传动系的两轮驱动摩托车。 前轮驱动器由位于头管内的转向轴上的部件组成，并且在前叉内以对称的方式对准，以便在提供全范围的转向时抵消来自旋转的前轮驱动的扭矩反作用。 前轮驱动器与减震前叉平行延长并缩短。 还公开了与前轮驱动器可操作地接合的接合离合器，单向轮毂和扭矩限制离合器。

    Systems and methods for tracing aircraft vortices
    6.
    发明申请
    Systems and methods for tracing aircraft vortices 有权
    跟踪飞机旋涡的系统和方法

    公开(公告)号：US20080035789A1

    公开(公告)日：2008-02-14

    申请号：US11647063

    申请日：2006-12-27

    申请人： Michael S. Lewis ,  Jere S. Meserole ,  Michael J. Dunn ,  Brian J. Tillotson

    发明人： Michael S. Lewis ,  Jere S. Meserole ,  Michael J. Dunn ,  Brian J. Tillotson

    IPC分类号： B64D47/00

    CPC分类号： G08G5/0013 ,  G01P5/001 ,  G08G5/0008 ,  G08G5/0091

    摘要： Systems and methods for tracing aircraft vortices are disclosed. One method includes directing a tracer from a first aircraft into a vortical flow generated by the first aircraft. The method can further include detecting a characteristic corresponding to the presence of the tracer directed into the vortical flow. Based at least in part on the detected characteristic, the method can include directing the flight of the first aircraft, or a second aircraft following the first aircraft, or both.

    摘要翻译： 公开了跟踪飞机旋涡的系统和方法。 一种方法包括将示踪器从第一飞行器引导到由第一飞行器产生的涡流中。 该方法还可以包括检测对应于引导到涡流中的示踪物的存在的特征。 至少部分地基于检测到的特征，该方法可以包括指导第一飞行器或第一飞机之后的第二飞机或两者的飞行。

    Method and system for determining the position of a mobile receiver
    7.
    发明授权
    Method and system for determining the position of a mobile receiver 失效
    用于确定移动接收机的位置的方法和系统

    公开(公告)号：US5600706A

    公开(公告)日：1997-02-04

    申请号：US240070

    申请日：1994-05-09

    申请人： Michael J. Dunn ,  Don H. Atherly ,  Douglas O. J. Reudink ,  Martin J. Feuerstein ,  Ronald E. Foerster ,  Ching Chuang ,  Dino J. Vendetti

    发明人： Michael J. Dunn ,  Don H. Atherly ,  Douglas O. J. Reudink ,  Martin J. Feuerstein ,  Ronald E. Foerster ,  Ching Chuang ,  Dino J. Vendetti

    IPC分类号： G01S5/10 ,  G01S5/14 ,  G01S19/48 ,  H04W4/02 ,  H04W4/24 ,  H04W60/00 ,  H04W64/00 ,  H04M11/00 ,  G01S3/02 ,  H04B7/185

    CPC分类号： G01S5/14 ,  G01S5/10 ,  H04M15/8033 ,  H04M15/8083 ,  H04W4/24 ,  H04W60/00 ,  H04M2215/0184 ,  H04M2215/32 ,  H04M2215/7435 ,  H04W4/02 ,  H04W64/00

    摘要： A position system and method utilizes a plurality of range transceivers located at known fixed locations and which are adapted to transmit approximately synchronized digital range signals for receipt by both a primary receiver and a supplemental receiver, the former disposed at a known location and the latter disposed at an unknown location. The range transceivers are adapted to transmit pulse sequences which include an error portion corresponding to the approximate synchronization error of each range signal. This error portion is constantly updated in accordance with the last determined synchronization errors of the corresponding range signals received by a secondary transceiver. In an alternative embodiment employing Code Division Multiple Access (CDMA) technology, the range transceiver time stamp on transmitted range signals may be adjusted to account for the measured timing error for a given range transceiver. The supplemental receiver receives the range signals and uses the same in accordance with known time of arrival or time difference of arrival calculation techniques to determine the position of the supplemental receiver.

    摘要翻译： 位置系统和方法利用位于已知固定位置处的多个范围收发器，并且其适于发送近似同步的数字范围信号，以便由主接收机和辅助接收机两者接收，前者设置在已知位置，后者设置在 在一个未知的位置。 范围收发器适于发送包括对应于每个范围信号的近似同步误差的误差部分的脉冲序列。 根据由次级收发器接收到的相应范围信号的最后确定的同步误差来不断更新该误差部分。 在采用码分多址（CDMA）技术的替代实施例中，传输范围信号上的范围收发器时间戳可以被调整以考虑给定范围收发器的测量定时误差。 补充接收机接收范围信号并根据已知的到达时间或到达时间差计算技术使用相同的信号来确定补充接收机的位置。

    Wound retraction apparatus and method
    8.
    发明授权
    Wound retraction apparatus and method 有权
    伤口收缩装置及方法

    公开(公告)号：US08388526B2

    公开(公告)日：2013-03-05

    申请号：US12108400

    申请日：2008-04-23

    申请人： Richard C. Ewers ,  John R. Brustad ,  Edward D. Pingleton ,  Nabil Hilal ,  Payam Adlparvar ,  Scott V. Taylor ,  Gary R. Dulak ,  Michael J. Dunn ,  Norman L. Morales ,  Charles C. Hart ,  Robert R. Bowes

    发明人： Richard C. Ewers ,  John R. Brustad ,  Edward D. Pingleton ,  Nabil Hilal ,  Payam Adlparvar ,  Scott V. Taylor ,  Gary R. Dulak ,  Michael J. Dunn ,  Norman L. Morales ,  Charles C. Hart ,  Robert R. Bowes

    IPC分类号： A61B17/02

    CPC分类号： A61B1/32 ,  A61B17/0293 ,  A61B17/3423 ,  A61B17/3431 ,  A61B2017/3484

    摘要： A surgical wound retractor is adapted to dilate a wound stretchable to a desired diameter, the retractor includes a first ring having a diameter greater than that desired for the wound and being adapted for disposition interiorly of the wound. A second ring has a diameter greater than that desired for the wound and is adapted for disposition exteriorly of the wound. A plurality of retraction elements are disposed in a generally cylindrical relationship to each other, between the first ring and the second ring. These elements extend through the wound to exert a radial retraction force on the wound which is dependent on the distance separating the first ring and the second ring. Retraction elements, both distensible and non-distensible are contemplated with appropriate attachment means at the rings to provide for variations in the retraction force. With a suitable retraction sleeve, a third ring can be provided to form a circumferential retainer to vary the retraction force. Rings can also be made inflatable or self-expanding to vary the retraction force. An associated method includes the step of rolling the second ring circumferentially of the third ring to form the circumferential retainer.

    摘要翻译： 外科伤口牵开器适于将可拉伸至期望直径的伤口扩张，牵开器包括直径大于伤口所需直径的第一环，并适于在伤口内部配置。 第二环的直径大于伤口所需的直径，并且适于在伤口的外部配置。 多个退回元件在第一环和第二环之间以大致圆柱形的关系设置。 这些元件延伸穿过伤口以在伤口上施加径向缩回力，这取决于分离第一环和第二环的距离。 缩回元件，可扩张和不扩张两者都可以在环上使用适当的附接装置来设计，以提供收缩力的变化。 利用合适的缩回套筒，可以提供第三环以形成圆周保持器以改变收回力。 环也可以制成充气或自膨胀以改变收缩力。 相关联的方法包括在第三环周向滚动第二环以形成周向保持器的步骤。

    Systems and methods for tracing aircraft vortices
    9.
    发明授权
    Systems and methods for tracing aircraft vortices 有权
    跟踪飞机旋涡的系统和方法

    公开(公告)号：US07874522B2

    公开(公告)日：2011-01-25

    申请号：US12625460

    申请日：2009-11-24

    申请人： Michael S. Lewis ,  Jere S. Meserole ,  Michael J. Dunn ,  Brian J. Tillotson

    发明人： Michael S. Lewis ,  Jere S. Meserole ,  Michael J. Dunn ,  Brian J. Tillotson

    IPC分类号： G05D1/08

    CPC分类号： G08G5/0013 ,  G01P5/001 ,  G08G5/0008 ,  G08G5/0091

    摘要： Systems and methods for tracing aircraft vortices. One method includes directing a tracer from a first aircraft into a vortical flow generated by the first aircraft. The method can further include detecting a characteristic corresponding to the presence of the tracer directed into the vortical flow. Based at least in part on the detected characteristic, the method can include directing the flight of the first aircraft, or a second aircraft following the first aircraft, or both.

    摘要翻译： 跟踪飞机旋涡的系统和方法。 一种方法包括将示踪器从第一飞行器引导到由第一飞行器产生的涡流中。 该方法还可以包括检测对应于引导到涡流中的示踪物的存在的特征。 至少部分地基于检测到的特征，该方法可以包括指导第一飞行器或第一飞机之后的第二飞机或两者的飞行。

    Stable maritime platform
    10.
    发明授权
    Stable maritime platform 有权
    稳定的海上平台

    公开(公告)号：US07703407B2

    公开(公告)日：2010-04-27

    申请号：US11944922

    申请日：2007-11-26

    申请人： Michael J. Dunn

    发明人： Michael J. Dunn

    IPC分类号： B63B35/50 ,  B63B35/44

    CPC分类号： B63B35/50

    摘要： Systems and methods for a stable maritime helicopter platform are disclosed. In one embodiment, a ship that may be converted into a spar buoy includes a flipping mechanism to convert the ship to the spar buoy, a takeoff and landing platform for helicopters and other VTOL vehicles, and an actuation and balance system to deploy the platform.

    摘要翻译： 公布了稳定的海上直升机平台的系统和方法。 在一个实施例中，可以转换成翼梁浮标的船包括翻转机构，用于将船转换成翼梁浮标，用于直升机和其它垂直起落架的起飞和着陆平台以及用于部署该平台的致动和平衡系统。