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164 条记录 (耗时 0.03 秒)

    Self tuning vibration isolation system
    132.
    发明授权
    Self tuning vibration isolation system 有权
    自调谐隔振系统

    公开(公告)号：US08731743B2

    公开(公告)日：2014-05-20

    申请号：US13444469

    申请日：2012-04-11

    申请人： Michael Seifert ,  Frank Bradley Stamps ,  Michael R. Smith ,  David E. Heverly

    发明人： Michael Seifert ,  Frank Bradley Stamps ,  Michael R. Smith ,  David E. Heverly

    IPC分类号： G06F17/00

    CPC分类号： B64C27/001 ,  B64C2027/002 ,  B64C2027/004 ,  F16F13/06 ,  F16F13/24 ,  F16F15/002 ,  F16F15/027

    摘要： A system and method to isolate vibrations from a vibrating structure. The system includes an adjustable vibration isolator that creates a reacting force matching the vibratory force of the vibrating structure. The method includes continuously monitoring the reacting force and vibratory force with a sensor system operably associated with a control unit having an algorithm to determine if adjustment of the vibration isolator is required. If required, the control unit commands a driver to selectively adjust the vibration isolator.

    摘要翻译： 将振动与振动结构隔离的系统和方法。 该系统包括可调节隔振器，其产生与振动结构的振动力相匹配的反作用力。 该方法包括使用与具有确定是否需要调节隔振器的算法的控制单元可操作地相关联的传感器系统连续地监测反作用力和振动力。 如果需要，控制单元命令驾驶员选择性地调节隔振器。

    Self Tuning Vibration Absorber
    133.
    发明申请
    Self Tuning Vibration Absorber 有权
    自调谐减振器

    公开(公告)号：US20130282204A1

    公开(公告)日：2013-10-24

    申请号：US13450060

    申请日：2012-04-18

    申请人： Michael Seifert ,  Frank B. Stamps ,  Michael R. Smith ,  David E. Heverly

    发明人： Michael Seifert ,  Frank B. Stamps ,  Michael R. Smith ,  David E. Heverly

    IPC分类号： B64C19/00 ,  F16F7/10

    CPC分类号： B64C27/001 ,  B64C2027/004 ,  F16F7/1005 ,  F16F15/00

    摘要： A system and method to adjustably create a reacting force in response to a vibrating force of a vibrating structure. The system includes an adjustable vibration absorber that creates a range of reacting forces. The method includes continuously monitoring the reacting force and the vibrating force with a sensor system operably associated with a control unit having an algorithm to determine if adjustment of the vibration absorber is required. If required, the control unit commands a driver to selectively adjust the vibration absorber such that the reacting force equals the vibrating force.

    摘要翻译： 一种响应于振动结构的振动力可调整地产生反作用力的系统和方法。 该系统包括可调节的振动吸收器，其产生一定范围的反作用力。 该方法包括使用与具有算法确定是否需要调节减振器的算法可操作地与控制单元可操作地相关联的传感器系统连续地监测反作用力和振动力。 如果需要，控制单元命令驾驶员选择性地调节振动吸收器，使得反作用力等于振动力。

    Method and system for including network security information in a frame
    134.
    发明授权
    Method and system for including network security information in a frame 有权
    在网络中包含网络安全信息的方法和系统

    公开(公告)号：US08561140B2

    公开(公告)日：2013-10-15

    申请号：US12779212

    申请日：2010-05-13

    申请人： Norman W. Finn ,  Michael R. Smith

    发明人： Norman W. Finn ,  Michael R. Smith

    IPC分类号： G06F7/04

    CPC分类号： H04L63/08 ,  H04L63/104

    摘要： A method and apparatus for including network security information in a frame is disclosed. Network security information is included in a secure portion of overhead of a frame. The network security information is configured to facilitate network security. A network device configured to process a frame is also disclosed. The frame includes frame security information and network security information. The frame security information is configured to facilitate securing a portion of overhead of the frame, and the network security information is located in the secure portion of the overhead of the frame and is configured to facilitate network security.

    摘要翻译： 公开了一种在网络中包含网络安全信息的方法和装置。 网络安全信息被包含在帧的开销的安全部分中。 网络安全信息被配置为便于网络安全。 还公开了一种被配置为处理帧的网络设备。 该帧包括帧安全信息和网络安全信息。 帧安全信息被配置为有助于保护帧的开销的一部分，并且网络安全信息位于帧的开销的安全部分中，并且被配置为便于网络安全性。

    Dual Frequency Damper for an Aircraft
    135.
    发明申请
    Dual Frequency Damper for an Aircraft 有权
    飞机双频阻尼器

    公开(公告)号：US20130241124A1

    公开(公告)日：2013-09-19

    申请号：US13421991

    申请日：2012-03-16

    申请人： Jeffrey Bosworth ,  Mithat Yuce ,  Frank B. Stamps ,  Michael R. Smith

    发明人： Jeffrey Bosworth ,  Mithat Yuce ,  Frank B. Stamps ,  Michael R. Smith

    IPC分类号： B64C27/51 ,  F16F13/08

    CPC分类号： B64C27/51

    摘要： A dual frequency damper includes a liquid inertia vibration eliminator (LIVE) portion and a fluid damper portion. LIVE portion and fluid damper portion operate in series and function so that dual frequency damper is optimized in both stiffness and damping at multiple frequencies. LIVE portion acts as a frequency dependent switch to selectively cause low frequency oscillatory forces to be treated primarily by the high spring rate and high damping rate characteristics of the fluid damper portion, and also to select high frequency oscillatory forces to be primarily treated by the low spring rate and low damping rate characteristics of the LIVE unit portion.

    摘要翻译： 双频阻尼器包括液体惯性减振器（LIVE）部分和流体阻尼器部分。 LIVE部分和流体阻尼器部分串联操作并且起作用，使得双频阻尼器在多个频率下的刚度和阻尼都被优化。 LIVE部分用作频率相关开关，以选择性地引起低频振荡力主要由流体阻尼器部分的高弹簧速率和高阻尼率特性来处理，并且还选择要被主要处理的低频振荡力 LIVE单元部分的弹簧刚度和低阻尼率特性。

    Aircraft occupant protection system
    137.
    发明授权
    Aircraft occupant protection system 有权
    飞机乘员保护系统

    公开(公告)号：US08474753B2

    公开(公告)日：2013-07-02

    申请号：US13125884

    申请日：2009-07-27

    申请人： Andrew T. Hill ,  Michael R. Smith ,  Zi Lu ,  Cheng-Ho Tho

    发明人： Andrew T. Hill ,  Michael R. Smith ,  Zi Lu ,  Cheng-Ho Tho

    IPC分类号： B64C25/56

    CPC分类号： B64D25/00 ,  B64C27/04 ,  B64D2201/00

    摘要： A crash attenuation system for an aircraft includes an airbag carried by the aircraft that is inflatable generally adjacent an exterior of the aircraft. The airbag is in fluid communication with at least one vent passage for channeling gas from within the interior of the airbag to a region external to the airbag that allows the gas to escape without being obstructed by the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag. A vent valve is provided within the vent passage for controlling a flow of gas through the vent passage, thereby controlling deflation of the airbag. The vent valve is continuously adjustable to and between an open state, a closed state, and any number of partially open states.

    摘要翻译： 用于飞行器的碰撞衰减系统包括由飞机携带的气囊，该气囊大体上邻近飞行器的外部可充气。 气囊与至少一个通气通道流体连通，用于将气体从气囊的内部引导到气囊外部的区域，允许气体逸出而不被气囊阻挡。 气体源与气囊的内部流体连通，以使气囊膨胀。 在排气通道内设有排气阀，用于控制通过通气通道的气体流，从而控制气囊的放气。 排气阀可连续调节到打开状态，关闭状态和任何数量的部分打开状态之间。

    Virtual service domains
    138.
    发明授权
    Virtual service domains 有权
    虚拟服务域

    公开(公告)号：US08442041B2

    公开(公告)日：2013-05-14

    申请号：US13557673

    申请日：2012-07-25

    申请人： Srinivas Sardar ,  Udayakumar Srinivasan ,  Shankar Ramachandran ,  Chidambareswaran Raman ,  Ajit Sanzgiri ,  Michael R. Smith

    发明人： Srinivas Sardar ,  Udayakumar Srinivasan ,  Shankar Ramachandran ,  Chidambareswaran Raman ,  Ajit Sanzgiri ,  Michael R. Smith

    IPC分类号： H04L12/50

    CPC分类号： H04L67/1097 ,  H04L45/04 ,  H04L67/327 ,  H04L69/12

    摘要： In one embodiment, ports of a network device are assigned to virtual service domains (VSDs). The ports are coupled to a virtual Ethernet module (VEM) of the network device. Each VSD is associated with one or more virtual service engines (VSEs) in a particular order. Each VSE is configured to apply a particular service to traffic traversing the VSE. Traffic received at a virtual Ethernet module (VEM) of the network device that is destined for a particular VSD, and is received on a port that has not been assigned to the particular VSD, is forwarded to the particular VSD via the one or more VSEs associated with the particular VSD such that the traffic traverses the one or more VSEs in the particular order.

    摘要翻译： 在一个实施例中，网络设备的端口被分配给虚拟服务域（VSD）。 端口耦合到网络设备的虚拟以太网模块（VEM）。 每个VSD以特定顺序与一个或多个虚拟服务引擎（VSE）相关联。 每个VSE被配置为将特定服务应用于遍历VSE的流量。 在发往特定VSD的网络设备的虚拟以太网模块（VEM）上接收的并且未被分配给特定VSD的端口上接收的流量经由一个或多个VSE被转发到特定的VSD 与特定VSD相关联，使得业务以特定顺序遍历一个或多个VSE。

    Crash attenuation system for aircraft
    139.
    发明授权
    Crash attenuation system for aircraft 有权
    飞机衰减衰减系统

    公开(公告)号：US08418957B2

    公开(公告)日：2013-04-16

    申请号：US13110607

    申请日：2011-05-18

    申请人： Michael R. Smith ,  Cheng-Ho Tho ,  Somen Chowdhury

    发明人： Michael R. Smith ,  Cheng-Ho Tho ,  Somen Chowdhury

    IPC分类号： B64C25/56

    CPC分类号： B64D25/00 ,  B64C27/04 ,  B64D2201/00

    摘要： A crash attenuation system for an aircraft, the system having an airbag carried by the aircraft and inflatable generally adjacent an exterior of the aircraft. The airbag has at least one vent for releasing gas from the interior of the airbag. A gas source is in fluid communication with the interior of the airbag for inflating the airbag with gas generated provided by the gas source. A vent valve is provided for controlling a flow of gas through each vent, each vent valve being selectively configurable between an open state, in which gas can pass through the associated vent from the interior of the airbag, and a closed state, in which gas is retained within the interior of the airbag. The gas source is provided for at least partially re-inflating the airbag after venting of gas through the at least one vent.

    摘要翻译： 一种用于飞行器的碰撞衰减系统，该系统具有由飞机携带并且大体上邻近飞机外部充气的气囊。 气囊具有至少一个用于从气囊的内部释放气体的通气口。 气体源与气囊的内部流体连通，用气体源产生的气体使气囊充气。 提供排气阀以控制通过每个通气口的气体流动，每个排气阀可选择性地配置在打开状态之间，气体可以从气囊的内部通过相关联的通气口，而关闭状态，气体 保持在气囊的内部。 气源被提供用于在通过至少一个排气口排出气体之后至少部分地重新充气气囊。