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    • 1. 发明授权
    • Secure over-the-air modification of automotive vehicular options
    • 确保汽车车辆选项的空中修改
    • US07926091B2
    • 2011-04-12
    • US11945860
    • 2007-11-27
    • Ansaf I. AlrabadyHoward J. CarverSalvatore G. Trupiano
    • Ansaf I. AlrabadyHoward J. CarverSalvatore G. Trupiano
    • G06F7/04H04L29/06
    • G06F21/6209G06F21/31G06F21/64H04L63/08H04L63/12H04W4/046H04W12/06H04W12/10
    • A method and system are provided for secure over-the-air modification of vehicular options by a vehicle user. The system includes a vehicle and a secure server. The vehicle includes receiver circuitry for receiving and demodulating wireless signals and a controller coupled to the receiver. The secure server is accessible by the vehicle user and generates a vehicular option modification package for provision to the vehicle by generating option parameter modification instructions in response to user parameter modification requests from the vehicle owner and generating authentication information in response to unique server authentication information associated with the secure server. The vehicle's receiver demodulates received wireless signals to generate the vehicular option modification package and the vehicle's controller authenticates the vehicular option modification package and, when the vehicular option modification package is authenticated, modifies the vehicular options of the vehicle in response to the parameter modification instructions.
    • 提供了一种方法和系统,用于由车辆用户对车辆选项进行安全的空中改装。 该系统包括车辆和安全服务器。 车辆包括用于接收和解调无线信号的接收机电路和耦合到接收机的控制器。 安全服务器可由车辆用户访问,并且通过响应于来自车主的用户参数修改请求生成选项参数修改指令并且响应于相关联的唯一服务器认证信息而生成认证信息来生成用于提供给车辆的车辆选项修改包 与安全服务器。 车辆的接收机解调接收到的无线信号以产生车辆选项修改包,并且车辆控制器认证车辆选项修改包,并且当车辆选项修改包被认证时,响应于参数修改指令来修改车辆的车辆选项。
    • 3. 发明授权
    • Vertical-lift and horizontal flight aircraft
    • 垂直升降机和水平飞行飞机
    • US06575401B1
    • 2003-06-10
    • US09925069
    • 2001-08-07
    • Howard J. Carver
    • Howard J. Carver
    • B64C2900
    • B64D27/24B64C27/20B64C29/0008B64C29/0025Y02T50/44Y02T50/64
    • A vertical-lift and horizontal flight aircraft, which can be operated in a horizontal flight mode, as soon as ground clearance is made. And, because of its unique design is very stable in flight, is very light, has a low drag resistance factor and is versatile in the configurations that can be made from a basic platform. The aircraft is primarily disk shaped with the aircraft body in the center surrounded by a lift assembly housing, an outer body lift surface and a propulsion thrust unit mounted aft of the central body compartment. The lift assembly housing is parallel with the aircraft body and contains an inner drive ring, with attached lift blades, facing inward toward the body compartment and an outer drive ring, with attached lift blades, facing outward toward the outer body lift surface. Electromagnetic motors power each drive ring. The inner and outer lift assemblies are composed of a drive ring; lift blades, a drive ring guide-way and electromagnetic motors. The inner and outer drive rings counter-rotate to alleviate any possible torque effect. Each drive ring is controlled independently, and synchronized to achieve positive directional control. As the drive rings rotate, the attached lift blades move through the air to create lift. The pitch of the lift blades can be fixed or variable. Once the aircraft is airborne and the forward motion is attained, air moving over the outer body lift surface provides the lift for horizontal flight. An electric control mechanism will synchronize the speed of the two counter-rotating lift assembly drive rings for flight control purposes. This will allow the body to rotate, or maintain a steady course. Flight directional flaps will control the direction of the aircraft.
    • 一个垂直升降机和水平飞行器,可以在水平飞行模式下操作,一旦进行离地间隙。 而且,由于其独特的设计在飞行中非常稳定,非常轻,具有较低的阻力系数,并且在基本平台可配置上具有通用性。 飞机主要是盘形的,飞机主体在中心处被包围的升降机组件外壳,外部主体提升表面和推动推力单元安装在中心体隔室的后面。 升降组件壳体与飞行器主体平行并且包含内部驱动环,附接的提升叶片朝向身体隔室向内,外部驱动环具有附接的提升叶片,朝向外部主体提升面向外。 电磁电机为每个驱动环供电。 内外升降组件由驱动环组成; 提升叶片,驱动环导轨和电磁马达。 内部和外部驱动环反向旋转以减轻任何可能的扭矩效应。 每个驱动环是独立控制的,并且同步以实现正方向控制。 当驱动环旋转时,附接的提升叶片通过空气移动以产生升力。 提升叶片的间距可以是固定的或可变的。 一旦飞机机载并且达到向前的运动,在外部机体提升表面上移动的空气提供了用于水平飞行的升降机。 电动控制机构将使两个反向旋转提升组件驱动环的速度同步以进行飞行控制。 这将允许身体旋转,或保持稳定的过程。 飞行方向襟翼将控制飞机的方向。
    • 4. 发明授权
    • Method and system for verifying an embedded module of a mobile vehicle
    • 用于验证移动车辆的嵌入式模块的方法和系统
    • US07194372B2
    • 2007-03-20
    • US10996635
    • 2004-11-23
    • Howard J. CarverSteven D. ScottJohn L. Dale
    • Howard J. CarverSteven D. ScottJohn L. Dale
    • G01R21/28
    • G06F11/263
    • A method and system for verifying an embedded module of a mobile vehicle. The method includes the steps of providing a validation test plan including a plurality of test keywords indexed to a requirement in a spread sheet format, receiving a validation test plan request including at least one requirement, determining the test keywords of the validation test plan based on the requirement according to a test keyword definition, and sending the test keywords from a call center to the embedded module based on correspondence between the requirement and test keywords. A computer usable medium with suitable computer program code is employed for verifying an embedded module of a mobile vehicle.
    • 一种用于验证移动车辆的嵌入式模块的方法和系统。 该方法包括以下步骤:提供验证测试计划,该验证测试计划包括以扩展表格格式的要求索引的多个测试关键字,接收包括至少一个需求的验证测试计划请求,基于以下步骤确定验证测试计划的测试关键字: 根据测试关键字定义的要求,并根据需求和测试关键字之间的对应关系,将测试关键字从呼叫中心发送到嵌入式模块。 采用具有合适的计算机程序代码的计算机可用介质来验证移动车辆的嵌入式模块。