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    • 2. 发明申请
    • INTERACTIVE CONTROLLER WITH AN INTEGRATED DISPLAY AND INTERFACE TO A SECOND CONTROLLER WITH STAND-ALONE DISPLAY
    • 具有集成显示的交互控制器和具有独立显示器的第二个控制器的接口
    • US20060205455A1
    • 2006-09-14
    • US10906811
    • 2005-03-08
    • Steven RehkemperNicholas GrisoliaKerry PhillipsLo Tak Kwong
    • Steven RehkemperNicholas GrisoliaKerry PhillipsLo Tak Kwong
    • A63F13/00
    • A63F13/26A63F13/00A63F13/235A63F13/92A63F2300/1031A63F2300/301A63F2300/403
    • The present invention provides for an interactive controller with an integrated display and with an interface to a second controller, that is in further communication with a stand-alone display. The interactive controller further includes a plurality of operation buttons positioned for manipulation by a user, a first electronic application stored in the interactive controller, a processor for generating control signals to control the first electronic application based upon input received from the operation buttons and for generating images on the display device in response thereto. The interactive controller includes a transmitter for transmitting wireless signals to the second controller. The second controller includes a receiver and is operatively connected to a stand-alone display. The second controller also includes a second electronic application and a processor for generating control signals to control the second electronic application based upon input received from the operation buttons and for generating images on the stand-alone display in response thereto.
    • 本发明提供一种具有集成显示器并具有与第二控制器的接口的交互式控制器,其与独立显示器进一步通信。 交互式控制器还包括多个操作按钮,用于操作用户,存储在交互式控制器中的第一电子应用程序,用于根据从操作按钮接收的输入产生控制信号以控制第一电子应用程序的处理器, 响应于显示设备上的图像。 交互式控制器包括用于向第二控制器发送无线信号的发射机。 第二控制器包括接收器并且可操作地连接到独立显示器。 第二控制器还包括第二电子应用和处理器,用于基于从操作按钮接收的输入产生控制信号以控制第二电子应用,并响应于此在独立显示器上生成图像。
    • 3. 发明申请
    • Control system for a flying vehicle
    • 飞行器控制系统
    • US20060157615A1
    • 2006-07-20
    • US11035606
    • 2005-01-14
    • Jeffrey RehkemperNicholas GrisoliaPeter Greenley
    • Jeffrey RehkemperNicholas GrisoliaPeter Greenley
    • B64C27/54
    • A63H30/00A63H27/12
    • In one embodiment of the present invention there is described a vehicle having a propeller mechanism for propelling the vehicle in a horizontal direction. The vehicle includes a transmitter positioned on the bottom of the vehicle for transmitting a signal from the vehicle downwardly away from the vehicle. A receiver is positioned on the bottom of the vehicle for receiving the signal as it is bounced off of a surface, defined as a bounced signal. A control system is also provided that automatically sets a speed of the propeller mechanism in response to the receiver. The control system sets the speed of the propeller mechanism to a first speed when the receiver receives the bounced signal and the control system sets the speed of the propeller mechanism to a second speed when the receiver does not receive the bounced signal. The first speed is predefined as a speed that causes the vehicle to gain altitude, while the second speed is predefined as a speed that causes the vehicle to lose altitude. When the vehicle reaches a predetermined distance away from the surface of the object, the vehicle will hover at the predetermined distance as the control system toggles between the first and second speeds.
    • 在本发明的一个实施例中,描述了具有用于在水平方向上推进车辆的螺旋桨机构的车辆。 车辆包括位于车辆底部的发射器,用于将来自车辆的信号向下远离车辆传输。 接收器位于车辆的底部,用于接收信号,当它被从表面反弹时,被定义为反弹信号。 还提供了一种响应于接收器自动设置螺旋桨机构的速度的控制系统。 当接收器接收到反弹信号时,控制系统将螺旋桨机构的速度设置为第一速度,并且当接收器未接收到反弹信号时,控制系统将螺旋桨机构的速度设定为第二速度。 第一速度被预先定义为导致车辆获得高度的速度,而第二速度被预先定义为导致车辆失去高度的速度。 当车辆距物体表面达到预定距离时,当控制系统在第一和第二速度之间切换时,车辆将以预定距离悬停。
    • 5. 发明授权
    • Propellers and propeller related vehicles
    • 螺旋桨和螺旋桨相关车辆
    • US06659395B2
    • 2003-12-09
    • US10189681
    • 2002-07-08
    • Jeffrey RehkemperKeith JohnsonNicholas Grisolia
    • Jeffrey RehkemperKeith JohnsonNicholas Grisolia
    • B64C2712
    • B64C27/32A63H27/12B64C27/52
    • A propeller related vehicle in accordance with one embodiment of the present invention is described as a helicopter having an airframe housing a motor mechanism for powering a main propeller attached to a main drive shaft that extends vertically through the airframe and for powering a tail rotor. The helicopter further includes a horizontal stabilizing mechanism attached between the main propeller and the main drive shaft, which permits the main propeller to freely pivot about the main drive shaft independently from the airframe. As such when the main propeller is rotating and the main propeller begins to pitch, the rotating main propeller has a centrifugal force created by the rotation thereof and will tend to pivot about the horizontal stabilizing mechanism in a manner that offsets the pitch such that the helicopter remains in a substantially horizontal position. In addition various main propeller configurations may be employed that provide additional self-stabilization.
    • 根据本发明的一个实施例的螺旋桨相关车辆被描述为具有机身的直升机,其具有容纳用于为主驱动轴连接的主螺旋桨供电的马达机构,所述主螺旋桨垂直延伸穿过机身并为尾部转子供电。 直升机还包括安装在主推进器和主驱动轴之间的水平稳定机构,其允许主螺旋桨独立于机身围绕主驱动轴自由枢转。 因此,当主螺旋桨旋转并且主螺旋桨开始俯仰时,旋转的主螺旋桨具有由其旋转产生的离心力,并且将趋向于以水平稳定机构的方式枢转,以偏移俯仰,使得直升机 保持在基本上水平的位置。 此外,可以采用提供额外的自稳定性的各种主要的螺旋桨结构。