公开(公告)号：WO2013148916A1

公开(公告)日：2013-10-03

申请号：PCT/US2013/034219

申请日：2013-03-28

Applicant: BOREALIS TECHNICAL LIMITED ,  EDELSON, Jonathan, Sidney ,  PERKINS, Scott ,  SWEET, Robert, M. ,  COX, Isaiah, W.

Inventor： EDELSON, Jonathan, Sidney ,  PERKINS, Scott ,  SWEET, Robert, M. ,  COX, Isaiah, W.

IPC: G01M17/00 ,  G01L3/00

CPC classification number: G01M17/013 ,  G01L5/26 ,  G01L5/28 ,  G01M17/0074 ,  G01N3/00

Abstract: A wheel testing system and method are provided that simulates realistically conditions likely to be encountered during operation of vehicle wheels, especially powered drive wheels and wheel-connected structures. The system may include an integral support frame designed to adjustably mount wheels or wheel-connected structures to be tested, a load motor drivingly connected to an inertial load, and an adjustable mounting sled configured to adjustably mount a test wheel or a wheel-connected structure with an hydraulic system actuatable to adjust the location of the test wheel relative to the inertial load to vary or fix the load on the test wheel desired. Speed of the test wheel can be varied or fixed by controlling the speed of the load motor. System measurement and data collection electronics measure a range of selected wheel parameters and gather data for transmission to a processor or non-transitory storage medium for processing and evaluation.

Abstract translation: 提供了一种车轮测试系统和方法，其模拟在车辆车轮，特别是动力驱动轮和轮子连接结构的操作期间可能遇到的现实条件。 该系统可以包括设计成可调节地安装待测试的轮子或车轮连接结构的整体支撑框架，驱动地连接到惯性负载的负载电动机和可调节安装滑车，其被配置成可调节地安装测试轮或轮子连接结构 液压系统可致动以调节测试轮相对于惯性负载的位置，以便将负载改变或固定在所需的测试轮上。 通过控制负载电机的速度可以改变或固定测试轮的速度。 系统测量和数据采集电子测量一系列选定的车轮参数，并收集数据以传输到处理器或非暂时性存储介质进行处理和评估。

公开(公告)号：WO2012162444A1

公开(公告)日：2012-11-29

申请号：PCT/US2012/039227

申请日：2012-05-24

Applicant: BOREALIS TECHNICAL LIMITED ,  SWEET, Robert, M. ,  EDELSON, Jonathan, Sidney

Inventor： SWEET, Robert, M. ,  EDELSON, Jonathan, Sidney

IPC: B64C25/36

CPC classification number: B64C25/34 ,  B60K7/0007 ,  B60L3/0061 ,  B60L15/2045 ,  B60L2200/10 ,  B60L2200/26 ,  B60L2220/44 ,  B60L2240/36 ,  B60L2240/421 ,  B60L2240/423 ,  B64C25/405 ,  F16H1/46 ,  H02K7/116 ,  Y02T10/641 ,  Y02T10/645 ,  Y02T10/72 ,  Y02T10/7283 ,  Y02T50/823

Abstract: A compact in-wheel vehicle motor and gearing system designed to meet high power and torque requirements for driving a vehicle on the ground independently of other power sources is provided. The motor and gearing system includes a motor assembly with an outside rotor element mounted for rotation about an inside stator element and a gear assembly with a plurality of gear stages mounted inside the stator and drivingly connected to the motor assembly. The motor assembly and gear assembly are mounted interiorly of the wheel and completely within a space defined by the internal dimensions of the wheel. This motor and gearing system can be effectively installed in an existing aircraft wheel without changes to other components to produce a drive wheel with the torque and power required to move the aircraft independently on the ground.

Abstract translation: 提供了紧凑的轮内车辆电动机和齿轮系统，其被设计为满足用于独立于其它动力源的在地面上驾驶车辆的高功率和扭矩要求。 电动机和齿轮系统包括具有外部转子元件的电动机组件，外部转子元件安装成用于围绕内部定子元件旋转;以及齿轮组件，其具有安装在定子内并驱动地连接到电动机组件的多个齿轮级。 马达组件和齿轮组件安装在车轮的内部并完全在由车轮的内部尺寸限定的空间内。 该电动机和齿轮系统可以有效地安装在现有的飞机车轮中，而不改变其他部件以产生驱动轮，其具有在飞机上独立地移动飞机所需的扭矩和功率。

公开(公告)号：WO2012061532A1

公开(公告)日：2012-05-10

申请号：PCT/US2011/059021

申请日：2011-11-02

Applicant: BOREALIS TECHNICAL LIMITED ,  EDELSON, Jonathan ,  GILLERAN, Neal ,  COX, Isaiah, Watas ,  PERKINS, Scott ,  SWEET, Robert, M.

Inventor： EDELSON, Jonathan ,  GILLERAN, Neal ,  COX, Isaiah, Watas ,  PERKINS, Scott ,  SWEET, Robert, M.

IPC: B64C25/50

CPC classification number: B64C25/405 ,  G08G5/065 ,  Y02T50/823

Abstract: 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 torgues and speeds.

Abstract translation: 提供一种飞机地面控制系统，其在飞机着陆和起飞之间在地面上移动，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。 飞机地面控制系统仅与飞机辅助动力单元或其他飞机电源接口，但是与飞机系统无关。 系统集成商和控制器连接驾驶舱控制器，其被设计成致动向系统部件传递动力，并且仅在预定条件下激活系统部件，并且可选地可激活的驱动器与一个或多个飞行器轮驱动连接，以使飞机在所选择的torgues上在地面上移动 和速度。

公开(公告)号：WO2013165529A2

公开(公告)日：2013-11-07

申请号：PCT/US2013/026933

申请日：2013-02-20

Applicant: PONIATOWSKI, Lauren H. ,  SWEET, Robert M. ,  REIHSEN, Troy E. ,  ROTTY, Vincent ,  HANANEL, David ,  STUBBS, Jack B. ,  SIE, Astrini ,  WINEK, Michael ,  KOWALEWSKI, Timothy M.

Inventor： PONIATOWSKI, Lauren H. ,  SWEET, Robert M. ,  REIHSEN, Troy E. ,  ROTTY, Vincent ,  HANANEL, David ,  STUBBS, Jack B. ,  SIE, Astrini ,  WINEK, Michael ,  KOWALEWSKI, Timothy M.

IPC: G09B23/28

CPC classification number: G09B23/30 ,  G06T7/0014 ,  G06T2207/20092 ,  G06T2207/30004 ,  G09B23/28

Abstract: A system for assessing performance of a procedure comprises a tissue model or a tool comprising assessment indicators applied thereto, one or more image-capturing devices for capturing one or more assessment images of the assessment indicators while or after a user performs the medical procedure, and a processor configured to analyze the assessment indicators in the one or more assessment images and provide feedback to the user. A system can also comprise a tissue model, one or more image-capturing devices each configured to capture one or more images of the tissue model, and a processor configured to analyze the one or more images from the one or more image-capturing devices to determine a deformation of the tissue model and determine a force exerted on the tissue model based on the determined deformation of the tissue model.

Abstract translation: 用于评估程序的性能的系统包括组织模型或包括应用于其的评估指示器的工具，用于在用户执行医疗程序期间或之后捕获评估指示符的一个或多个评估图像的一个或多个图像捕获装置，以及 处理器，其被配置为分析所述一个或多个评估图像中的评估指示符，并向所述用户提供反馈。 系统还可以包括组织模型，每个被配置为捕获组织模型的一个或多个图像的一个或多个图像捕获装置，以及被配置为将一个或多个图像从一个或多个图像捕获装置分析到 确定组织模型的变形并且基于所确定的组织模型的变形来确定施加在组织模型上的力。

公开(公告)号：WO2013165529A3

公开(公告)日：2014-02-20

申请号：PCT/US2013026933

申请日：2013-02-20

Applicant: PONIATOWSKI LAUREN H ,  SWEET ROBERT M ,  REIHSEN TROY E ,  ROTTY VINCENT ,  HANANEL DAVID ,  STUBBS JACK B ,  SIE ASTRINI ,  WINEK MICHAEL ,  KOWALEWSKI TIMOTHY M

Inventor： PONIATOWSKI LAUREN H ,  SWEET ROBERT M ,  REIHSEN TROY E ,  ROTTY VINCENT ,  HANANEL DAVID ,  STUBBS JACK B ,  SIE ASTRINI ,  WINEK MICHAEL ,  KOWALEWSKI TIMOTHY M

IPC: G09B23/28

CPC classification number: G09B23/30 ,  G06T7/0014 ,  G06T2207/20092 ,  G06T2207/30004 ,  G09B23/28

Abstract: A system for assessing performance of a procedure comprises a tissue model or a tool comprising assessment indicators applied thereto, one or more image-capturing devices for capturing one or more assessment images of the assessment indicators while or after a user performs the medical procedure, and a processor configured to analyze the assessment indicators in the one or more assessment images and provide feedback to the user. A system can also comprise a tissue model, one or more image-capturing devices each configured to capture one or more images of the tissue model, and a processor configured to analyze the one or more images from the one or more image-capturing devices to determine a deformation of the tissue model and determine a force exerted on the tissue model based on the determined deformation of the tissue model.

Abstract translation: 用于评估程序的性能的系统包括组织模型或包括应用于其的评估指示器的工具，用于在用户执行医疗程序期间或之后捕获评估指示符的一个或多个评估图像的一个或多个图像捕获装置，以及 处理器，其被配置为分析所述一个或多个评估图像中的评估指示符，并向所述用户提供反馈。 系统还可以包括组织模型，每个被配置为捕获组织模型的一个或多个图像的一个或多个图像捕获装置，以及被配置为将一个或多个图像从一个或多个图像捕获装置分析到 确定组织模型的变形并且基于所确定的组织模型的变形来确定施加在组织模型上的力。

公开(公告)号：WO2012071456A3

公开(公告)日：2013-07-25

申请号：PCT/US2011061928

申请日：2011-11-22

Applicant: BOREALIS TECH LTD ,  GILLERAN NEAL ,  SWEET ROBERT M ,  EDELSON JONATHAN ,  COX ISAIAH WATAS

Inventor： GILLERAN NEAL ,  SWEET ROBERT M ,  EDELSON JONATHAN ,  COX ISAIAH WATAS

IPC: B64C25/50

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：WO2006023224A3

公开(公告)日：2006-03-02

申请号：PCT/US2005/026621

申请日：2005-07-27

Applicant: RED LLAMA INC. ,  GRUENBAUM, Peter E. ,  AIROLA, Christopher A. ,  BURNETT, Timothy R. ,  MARTINSON, Janet M. ,  ROBISON, David F.W. ,  SWEET, Robert M.

Inventor： GRUENBAUM, Peter E. ,  AIROLA, Christopher A. ,  BURNETT, Timothy R. ,  MARTINSON, Janet M. ,  ROBISON, David F.W. ,  SWEET, Robert M.

IPC: G09B23/28

Abstract: 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.

公开(公告)号：WO2012071456A2

公开(公告)日：2012-05-31

申请号：PCT/US2011/061928

申请日：2011-11-22

Applicant: BOREALIS TECHNICAL LIMITED ,  GILLERAN, Neal ,  SWEET, Robert, M. ,  EDELSON, Jonathan ,  COX, Isaiah, Watas

Inventor： GILLERAN, Neal ,  SWEET, Robert, M. ,  EDELSON, Jonathan ,  COX, Isaiah, Watas

IPC: B64C19/02

CPC classification number: B64C25/405 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：WO2012174306A3

公开(公告)日：2014-05-01

申请号：PCT/US2012042547

申请日：2012-06-14

Applicant: BOREALIS TECH LTD ,  GILLERAN NEAL ,  SWEET ROBERT M ,  PERKINS SCOTT

Inventor： GILLERAN NEAL ,  SWEET ROBERT M ,  PERKINS SCOTT

IPC: B64C25/36

CPC classification number: B64C25/405 ,  B60B25/002 ,  B60B25/04 ,  Y02T10/82 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。

公开(公告)号：WO2012174306A2

公开(公告)日：2012-12-20

申请号：PCT/US2012/042547

申请日：2012-06-14

Applicant: BOREALIS TECHNICAL LIMITED ,  GILLERAN, Neal ,  SWEET, Robert, M. ,  PERKINS, Scott

Inventor： GILLERAN, Neal ,  SWEET, Robert, M. ,  PERKINS, Scott

IPC: H02J4/00 ,  H01L31/052 ,  H01L31/0236 ,  G06F17/50

CPC classification number: B64C25/405 ,  B60B25/002 ,  B60B25/04 ,  Y02T10/82 ,  Y02T50/823

Abstract: 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.

Abstract translation: 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。