公开(公告)号：US20140261443A1

公开(公告)日：2014-09-18

申请号：US14067158

申请日：2013-10-30

申请人： STEPHEN JAY LOWENSTEIN ,  KEITH RUBIN ,  KEN SOLOVAY ,  TIMOTHY VANDERMEY ,  KLAUS LESSNAU ,  MICHAEL R. COLE

发明人： STEPHEN JAY LOWENSTEIN ,  KEITH RUBIN ,  KEN SOLOVAY ,  TIMOTHY VANDERMEY ,  KLAUS LESSNAU ,  MICHAEL R. COLE

IPC分类号： A61M16/00 ,  A61M16/04

CPC分类号： A61M16/044 ,  A61M2205/3341 ,  A61M2205/505 ,  A61M2205/8212

摘要： A system and accompanying assembly, of integrated or modular construction, for inflating and monitoring pressure within a retaining cuff including a housing having a pressure chamber connected in fluid communication with a fluid pressure source and a fluid communicating connection with the retaining cuff. Associated control circuitry includes a pressure sensor disposable in fluid communication with the pressure chamber and the retaining cuff, via the fluid communicating connection and structured to concurrently determine and monitor pressure within the pressure chamber and the retaining cuff. The control circuitry is cooperatively structured with the pressure sensor and other operative components to establish dynamic multilevel sampling capabilities, calibration parameters stored within the control circuitry prior to use and limited or single use capabilities of the assembly.

摘要翻译： 一种用于对保持箍内的压力进行充气和监测的系统和伴随组件，包括具有与流体压力源流体连通的压力室和与保持箍的流体连通连接的压力室的壳体。 相关控制电路包括经由流体连通连接与压力室和保持箍一起流体连通并且被构造成同时确定和监测压力室和保持箍内的压力的压力传感器。 控制电路与压力传感器和其他可操作部件协同地构成，以在使用之前建立动态多级采样能力，存储在控制电路内的校准参数以及组件的有限或单一使用能力。

公开(公告)号：US07159817B2

公开(公告)日：2007-01-09

申请号：US11035263

申请日：2005-01-13

申请人： Timothy VanderMey ,  Josiah VanderMey

发明人： Timothy VanderMey ,  Josiah VanderMey

IPC分类号： B64C15/00 ,  B64C29/00

CPC分类号： B64C39/062 ,  B64C29/0016 ,  B64C39/068 ,  B64C39/08

摘要： An aircraft having a vertical take-off and landing (VTOL) propulsion system. The aircraft includes a fuselage, the VTOL propulsion system, at least one forward thruster, a power source used for both the VTOL propulsion system and forward thruster, fore and aft wings and a plurality of spars attached to and spanning the space between the two wings. The VTOL propulsion system includes a plurality of VTOL cells (including a motor, motor controller, and propeller) attached in a spaced relation along each spar. The VTOL cells are used exclusively for vertical flight or hovering and are powered down as the aircraft develops forward flight velocity and corresponding wing lift. During forward flight the VTOL propellers are articulated to allow the aircraft to take on a low drag configuration. The present invention is suitable for use in manned or un-manned aircraft of any scale.

摘要翻译： 具有垂直起降（VTOL）推进系统的飞机。 飞机包括机身，垂直起降推进系统，至少一个前推进器，用于垂直起降推进系统和前推进器，前后翼的动力源和连接到两翼之间的空间的多个翼梁 。 VTOL推进系统包括沿着每个翼梁以间隔的关系附接的多个VTOL单元（包括马达，马达控制器和螺旋桨）。 垂直起落架单元专门用于垂直飞行或悬停，并随着飞机发展向前飞行速度和相应的机翼升力而断电。 在向前飞行期间，垂直起落架螺旋桨被铰接以允许飞机采取低阻力配置。 本发明适用于任何规模的载人或无人驾驶飞机。

公开(公告)号：US20060256881A1

公开(公告)日：2006-11-16

申请号：US11127401

申请日：2005-05-12

申请人： Lawrence Yonge ,  Timothy Vandermey

发明人： Lawrence Yonge ,  Timothy Vandermey

IPC分类号： H04K1/10

CPC分类号： H04L27/2608 ,  H04L27/2602

摘要： A method for generating a signal is presented. The method includes selecting a first set of carrier frequencies that are integral multiples of a first frequency interval, and selecting a second set of carrier frequencies that are integral multiples of a second frequency interval. The second frequency interval is an integral multiple of the first frequency interval and the second set is a subset of the first set. The method includes, for each of one or more signal carrier frequencies in the second set, selecting a plurality of associated carrier frequencies in the first set including a peak carrier frequency having substantially the same value as the signal carrier frequency, and modulating waveform frequency components at each of the selected plurality of associated carrier frequencies according to the same data value.

公开(公告)号：US20070025398A1

公开(公告)日：2007-02-01

申请号：US11339293

申请日：2006-01-24

申请人： Lawrence Yonge ,  Srinivas Katar ,  Timothy Vandermey ,  James Petranovich ,  Neal Riedel ,  George Peponides ,  Sherman Gavette

发明人： Lawrence Yonge ,  Srinivas Katar ,  Timothy Vandermey ,  James Petranovich ,  Neal Riedel ,  George Peponides ,  Sherman Gavette

IPC分类号： H04J3/06 ,  H04L7/00

CPC分类号： H04J3/0655 ,  H04B3/54 ,  H04B2203/5408 ,  H04B2203/5412 ,  H04B2203/5416

摘要： A method and corresponding system for communicating between stations in a network is presented. The method includes providing repeated beacon transmissions from a coordinator station for coordinating transmissions among the stations; transmitting a signal from a first station and receiving the signal at a second station; and performing one or both of: generating the signal based on a local clock at the first station and time adjustment information in a beacon transmission received by the first station, and sampling the signal at sample times based on a local clock at the second station and time adjustment information in a beacon transmission received by the second station.

摘要翻译： 提出了一种用于在网络中的站之间进行通信的方法和对应系统。 该方法包括提供来自协调站的重复信标传输，用于协调站间的传输; 从第一站发送信号并在第二站接收信号; 并且执行以下中的一个或两个：基于第一站处的本地时钟生成信号和由第一站接收的信标发送中的时间调整信息，以及基于第二站处的本地时钟在采样时间采样信号，以及 由第二站接收的信标发送中的时间调整信息。

公开(公告)号：US20060256883A1

公开(公告)日：2006-11-16

申请号：US11347002

申请日：2006-02-03

申请人： Lawrence Yonge ,  Timothy VanderMey

发明人： Lawrence Yonge ,  Timothy VanderMey

IPC分类号： H04K1/10

CPC分类号： H04L27/2602 ,  H04L27/2608

摘要： A method and system for transmitting signals between communication nodes is presented. The method includes generating a first waveform that includes a shaped portion; generating a second waveform that includes a shaped portion; and combining the first and second waveforms including overlapping the shaped portion of the first waveform with the shaped portion of the second waveform and adding the overlapped portions of the waveforms. The method includes generating a signal including the combined first and second waveforms. At least one of the first and second waveforms includes a characteristic signature configured for synchronizing with the signal.

摘要翻译： 提出了一种在通信节点之间传输信号的方法和系统。 该方法包括产生包括成形部分的第一波形; 产生包括成形部分的第二波形; 以及将包括与第一波形的成形部分重叠的第一和第二波形与第二波形的成形部分组合，并且将波形的重叠部分相加。 该方法包括产生包括组合的第一和第二波形的信号。 第一波形和第二波形中的至少一个波形包括被配置为与该信号同步的特征签名。

公开(公告)号：US20060151666A1

公开(公告)日：2006-07-13

申请号：US11035263

申请日：2005-01-13

申请人： Timothy VanderMey ,  Josiah VanderMey

发明人： Timothy VanderMey ,  Josiah VanderMey

IPC分类号： B64C29/00

CPC分类号： B64C39/062 ,  B64C29/0016 ,  B64C39/068 ,  B64C39/08

摘要： An aircraft having a vertical take-off and landing (VTOL) propulsion system. The aircraft includes a fuselage, the VTOL propulsion system, at least one forward thruster, a power source used for both the VTOL propulsion system and forward thruster, fore and aft wings and a plurality of spars attached to and spanning the space between the two wings. The VTOL propulsion system includes a plurality of VTOL cells (including a motor, motor controller, and propeller) attached in a spaced relation along each spar. The VTOL cells are used exclusively for vertical flight or hovering and are powered down as the aircraft develops forward flight velocity and corresponding wing lift. During forward flight the VTOL propellers are articulated to allow the aircraft to take on a low drag configuration. The present invention is suitable for use in manned or un-manned aircraft of any scale.

摘要翻译： 具有垂直起降（VTOL）推进系统的飞机。 飞机包括机身，垂直起降推进系统，至少一个前推进器，用于垂直起降推进系统和前推进器，前后翼的动力源和连接到两翼之间的空间的多个翼梁 。 VTOL推进系统包括沿着每个翼梁以间隔的关系附接的多个VTOL单元（包括马达，马达控制器和螺旋桨）。 垂直起落架单元专门用于垂直飞行或悬停，并随着飞机发展向前飞行速度和相应的机翼升力而断电。 在向前飞行期间，垂直起落架螺旋桨被铰接以允许飞机采取低阻力配置。 本发明适用于任何规模的载人或无人驾驶飞机。