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1. 发明申请

US20060040245A1 Interactive medical procedure training 审中-公开
标题翻译：互动医疗程序培训
公开(公告)号：US20060040245A1
公开(公告)日：2006-02-23
申请号：US10923353
申请日：2004-08-20
申请人： Christopher Airola , Peter Gruenbaum , Timothy Burnett , Janet Martinson , David Feiner Robison , Robert Sweet
发明人： Christopher Airola , Peter Gruenbaum , Timothy Burnett , Janet Martinson , David Feiner Robison , Robert Sweet
IPC分类号： G09B19/00 , G09B23/28
CPC分类号： G09B23/28 , G09B5/00 , G09B7/00
摘要： Apparatuses and methods are described that provide for selecting an actor to participate in an interactive simulation of a medical procedure within a graphical user interface. A medical instrument is identified that is to be used by the actor and an association is indicated between the medical instrument and the actor. A user plays the role of the actor.
摘要翻译：描述了提供用于选择演员参与图形用户界面内的医疗过程的交互式仿真的装置和方法。确定要由演员使用的医疗器械，并且在医疗器械和演员之间指示关联。用户扮演演员角色。

2. 发明授权

US06854164B2 Termination device for an aramid-based elevator rope 有权
标题翻译：用于基于芳纶的电梯绳索的终止装置
公开(公告)号：US06854164B2
公开(公告)日：2005-02-15
申请号：US10353139
申请日：2003-01-28
申请人： Patrick M. Bass , Robert Sweet
发明人： Patrick M. Bass , Robert Sweet
IPC分类号： B66B7/08 , F16G11/00 , F16G11/04
CPC分类号： B66B7/08 , F16G11/046 , Y10T24/3909 , Y10T24/3969 , Y10T24/3996 , Y10T403/4345
摘要： A termination device for an aramid-based elevator rope comprises a socket having a tapered internal passageway adapted to receive a wedge and a rope. The passageway has first and second semi-cylindrical rope engaging surfaces. The wedge has a peripheral groove having a variable radius of curvature. The device clamps the length of rope between linear portions of the wedge and the rope engaging surfaces of the socket with a substantially uniform application of force on the cross-section of the rope.
摘要翻译：用于基于芳族聚酰胺的电梯绳索的终端装置包括具有适于容纳楔形物和绳索的锥形内部通道的插座。通道具有第一和第二半圆柱形绳索接合表面。楔具有可变曲率半径的周向槽。该装置在绳索的横截面上基本均匀地施加力而将楔形物的线性部分与插座的绳索接合表面之间的绳索长度夹紧。

3. 发明授权

US09022316B2 System and method for failsafe operation of aircraft ground movement system 有权
标题翻译：飞机地面运动系统故障安全运行系统及方法
公开(公告)号：US09022316B2
公开(公告)日：2015-05-05
申请号：US13301498
申请日：2011-11-21
申请人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
发明人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
IPC分类号： B64C25/00 , B64C25/40
CPC分类号： B64C25/405 , Y02T50/823
摘要： A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.
摘要翻译：提供一种用于确保具有地面运动系统的飞机的安全操作以在地面独立地驱动飞机的故障安全系统和方法。该系统包括至少一个飞行器鼻部或主驱动轮，其由响应于感测到的飞行器和地面移动系统操作参数的车载驱动器驱动，以响应于正常限度内的参数继续操作，或者如果感测到的参数在正常限度之外，则防止继续操作并指示持续运作不安全。车载轮驱动器包括一个自动或手动响应的信号，该锁定组件响应于指示感测参数的信号，以根据地面移动系统的操作是否可以安全地继续操作将车载车轮驱动器锁定在激活状态或非激活状态。

4. 发明申请

US20120217339A1 System and Method for Failsafe Operation of Aircraft Ground Movement System 有权
标题翻译：飞机地面运动系统故障安全运行系统与方法
公开(公告)号：US20120217339A1
公开(公告)日：2012-08-30
申请号：US13301498
申请日：2011-11-21
申请人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
发明人： Neal Gilleran , Robert Sweet , Jonathan Edelson , Isaiah Watas Cox
IPC分类号： B64C25/50 , G08G5/06
CPC分类号： B64C25/405 , Y02T50/823
摘要： A failsafe system and method for ensuring the safe operation of an aircraft with a ground movement system to drive the aircraft independently on the ground is provided. The system includes at least one aircraft nose or main drive wheel powered by an onboard wheel driver responsive to sensed aircraft and ground movement system operating parameters to continue operation in response to parameters within normal limits or to prevent continued operation if sensed parameters are outside normal limits and indicate continued operation to be unsafe. The onboard wheel driver includes a locking assembly responsive automatically or manually to signals indicating sensed parameters to lock the onboard wheel driver in an activated or an inactivated condition, depending on whether operation of the ground movement system can be continued safely.
摘要翻译：提供一种用于确保具有地面运动系统的飞机的安全操作以在地面独立地驱动飞机的故障安全系统和方法。该系统包括至少一个飞行器鼻部或主驱动轮，其由响应于感测到的飞行器和地面移动系统操作参数的车载驱动器驱动，以响应于正常限度内的参数继续操作，或者如果感测到的参数在正常限度之外，则防止继续操作并指示持续运作不安全。车载轮驱动器包括一个自动或手动响应的信号，该锁定组件响应于指示感测参数的信号，以根据地面移动系统的操作是否可以安全地继续操作将车载车轮驱动器锁定在激活状态或非激活状态。

5. 发明授权

US09033273B2 Integrated aircraft ground navigation control system 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US09033273B2
公开(公告)日：2015-05-19
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/00 , B64C25/40 , G08G5/06
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torques and speeds.
摘要翻译：提供一种飞机地面控制系统，其在飞机着陆和起飞之间移动飞机，而不需要机场拖船或拖车的外部机械帮助，或依赖飞机发动机产生的推力。飞机地面控制系统只能与飞机辅助动力装置或其他飞机电源相连接，而与飞机系统无关。系统集成商和控制器连接驾驶舱控制器，其设计用于致动向系统组件传递电力，并且仅在预定条件下激活系统组件，其中选择性地激活驱动器与一个或多个飞行器轮驱动连接，以在选定的转矩下将飞机移动到地面上和速度。

6. 发明授权

US08833694B2 Split circumference aircraft wheel assembly with integrated drive motor assembly 有权
标题翻译：分体式飞轮组件与集成驱动电机组合
公开(公告)号：US08833694B2
公开(公告)日：2014-09-16
申请号：US13523865
申请日：2012-06-14
申请人： Neal Gilleran , Robert Sweet , Scott Perkins
发明人： Neal Gilleran , Robert Sweet , Scott Perkins
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , Y02T50/823
摘要： A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.
摘要翻译：为飞机着陆齿轮提供分体式圆周轮组件，其被配置为使起落架轮井内的空间最大化，以支撑具有驱动装置的马达驱动器组件，所述驱动装置驱动地面上的飞行器轮。分体式圆周轮组件包括可分离的内侧和外侧支撑壁，其间隔开最大距离的轴向间隔，使得电动机驱动器组件完全包含在限定的最大空间内。优选的车轮组件采用可拆卸的凸缘和锁定环，以将电动机驱动器组件整体地和可拆卸地支撑在最大化的车轮体积内以驱动一个或多个飞行器轮子并且独立地在地面上移动飞行器。这里描述的车轮和马达驱动器组件被设计成在现有飞行器轮中进行改装。

7. 发明申请

US20130056580A1 SPLIT CIRCUMFERENCE AIRCRAFT WHEEL ASSEMBLY WITH INTEGRATED DRIVE MOTOR ASSEMBLY 有权
标题翻译：具有集成驱动电机组件的分体循环飞行器车轮组件
公开(公告)号：US20130056580A1
公开(公告)日：2013-03-07
申请号：US13523865
申请日：2012-06-14
申请人： Neal Gilleran , Robert Sweet , Scott Perkins
发明人： Neal Gilleran , Robert Sweet , Scott Perkins
IPC分类号： B64C25/50 , B64C25/36
CPC分类号： B64C25/405 , Y02T50/823
摘要： A split circumference wheel assembly is provided for an aircraft landing gear wheel configured to maximize the space available within a landing gear wheel well to support a motor driver assembly with drive means that drives the aircraft wheel on the ground. The split circumference wheel assembly includes separable inboard and outboard support walls that are spaced axially apart a maximized distance so that the motor driver assembly is completely contained within the maximized space defined. A preferred wheel assembly employs a demountable flange and a locking ring to integrally and removably support the motor driver assembly within the maximized wheel volume to drive one or more aircraft wheels and move the aircraft independently on the ground. The wheel and motor driver assembly described herein are designed to be retrofitted in an existing aircraft wheel.
摘要翻译：为飞机着陆齿轮提供分体式圆周轮组件，其被配置为使起落架轮井内的空间最大化，以支撑具有驱动装置的马达驱动器组件，所述驱动装置驱动地面上的飞行器轮。分体式圆周轮组件包括可分离的内侧和外侧支撑壁，其间隔开最大距离的轴向间隔，使得电动机驱动器组件完全包含在限定的最大空间内。优选的车轮组件采用可拆卸的凸缘和锁定环，以将电动机驱动器组件整体地和可拆卸地支撑在最大化的车轮体积内以驱动一个或多个飞行器轮子并且独立地在地面上移动飞行器。这里描述的车轮和马达驱动器组件被设计成在现有飞行器轮中进行改装。

8. 发明申请

US20120168557A1 Integrated Aircraft Ground Navigation Control System 有权
标题翻译：综合飞机地面导航控制系统
公开(公告)号：US20120168557A1
公开(公告)日：2012-07-05
申请号：US13287115
申请日：2011-11-01
申请人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
发明人： Jonathan Edelson , Neal Gilleran , Isaiah Cox , Scott Perkins , Robert Sweet
IPC分类号： B64C25/50
CPC分类号： B64C25/405 , G08G5/065 , Y02T50/823
摘要： An aircraft ground control system that moves an aircraft on the ground between landing and take off without external mechanical assistance from airport tugs or tow vehicles or reliance on thrust produced by the aircraft's engines is provided. The aircraft ground control system interfaces only with an aircraft auxiliary power unit or other aircraft power supply, but otherwise operates independently of aircraft systems. A system integrator and controller links cockpit controls designed to actuate the transmission of power to system components and to activate system components only under predetermined conditions with selectively activatable drivers in driving connection with one or more aircraft wheels to move the aircraft on the ground at selected torques and speeds.
摘要翻译：提供一种飞机地面控制系统，其在飞机着陆和起飞之间移动飞机，而不需要机场拖船或拖车的外部机械帮助，或依赖飞机发动机产生的推力。飞机地面控制系统只能与飞机辅助动力装置或其他飞机电源相连接，而与飞机系统无关。系统集成商和控制器连接驾驶舱控制器，其设计用于致动向系统组件传递电力，并且仅在预定条件下激活系统组件，其中选择性地激活驱动器与一个或多个飞行器轮驱动连接，以在选定的转矩下将飞机移动到地面上和速度。

9. 发明申请

US20090208143A1 EFFICIENT AUTOMATED UROTHELIAL IMAGING USING AN ENDOSCOPE WITH TIP BENDING 审中-公开
标题翻译：使用胫骨弯曲的内窥镜进行有效的自动化尿路成像
公开(公告)号：US20090208143A1
公开(公告)日：2009-08-20
申请号：US12033826
申请日：2008-02-19
申请人： Woon Jong Yoon , Eric Seibel , Robert Sweet , Per Reinhall
发明人： Woon Jong Yoon , Eric Seibel , Robert Sweet , Per Reinhall
IPC分类号： G06K9/20
CPC分类号： A61B1/0058 , A61B1/00165 , A61B1/06 , A61B5/0062 , A61B5/0066 , A61B5/0084 , A61B5/065 , A61B5/411
摘要： A scanning fiber endoscope (SFE) disposed at the distal end of a flexible, small diameter imaging probe is inserted through a relatively small opening and into a larger volume, such as the bladder. Actuators disposed adjacent to the distal end of the imaging probe are selectively activated to bend the distal end of the imaging probe to assist in positioning and orienting the SFE at a plurality of points selected to image substantially all of at least a desired portion of the interior surface of the volume. The insertion depth, bending arc, and rotational position of the imaging probe can be manually and/or automatically controlled. The user can inspect the images to determine if a desired portion of the surface has been imaged and can thus ensure that a tumor or other characteristic of the surface is not overlooked due to a failure to image it.
摘要翻译：设置在柔性小直径成像探针的远端的扫描光纤内窥镜（SFE）通过相对小的开口插入诸如膀胱的较大体积中。被选择性地启动成像探头的远端设置的致动器，以弯曲成像探针的远端，以帮助定位和定向SFE在多个点上，所述多个点被选择为基本上全部至少部分内部的所需部分表面的体积。成像探头的插入深度，弯曲弧度和旋转位置可以手动和/或自动控制。用户可以检查图像以确定表面的所需部分是否已被成像，并且因此可以确保由于不能对其进行成像而使肿瘤或其他表面特征不被忽视。

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