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    • 1. 发明申请
    • Workspace lighting system
    • 工作区照明系统
    • US20070279895A1
    • 2007-12-06
    • US11432036
    • 2006-05-10
    • Walter ClarkDouglas BourneErik PageMichael SiminovitchKevin Gauna
    • Walter ClarkDouglas BourneErik PageMichael SiminovitchKevin Gauna
    • F21V33/00
    • F21S6/003F21S2/00F21V21/28F21Y2115/10
    • A modular lighting system for lighting a work area is disclosed. The system includes a power supply with power outlets for powering LED fixtures. The power supply preferably operates at or below a fixed power output level, such as to illuminate the work area using less than 0.2 Watts per square foot of energy. The lighting system also includes an occupancy sensor and/or a light level sensor for controlling lighting levels in the work area in response to detection of a person, ambient light levels and/or a combination thereof. The lighting system can also include computer unit with a micro-processor and a memory unit for running software or firmware the executes lighting programs, stores light usage histories and/or provides system reports to a remote computer by a wireless means and/or over a computer network.
    • 公开了一种用于照亮工作区域的模块化照明系统。 该系统包括一个电源,带有供电LED灯具的电源插座。 电源优选地在等于或低于固定功率输出电平的情况下操作,例如以每平方英尺能量小于0.2瓦的照明工作区域。 照明系统还包括占用传感器和/或光级传感器,用于响应于人的检测,环境光水平和/或其组合来控制工作区域中的照明水平。 照明系统还可以包括具有微处理器的计算机单元和用于运行软件或固件的存储单元,执行照明程序,存储光使用历史和/或通过无线装置和/或通过无线装置向远程计算机提供系统报告 计算机网络。
    • 4. 发明申请
    • SYSTEM AND METHOD FOR LANDING A TAILLESS AIRCRAFT IN A CROSSWIND
    • 用于在无人驾驶飞机上着陆的系统和方法
    • US20080017753A1
    • 2008-01-24
    • US11159472
    • 2005-06-23
    • Walter Clark
    • Walter Clark
    • B64C25/30
    • B64C39/10B64C25/50B64C25/60
    • The method of landing a flying wing type aircraft in a crosswind includes the steps of disengaging the nose landing wheel upon impact with the runway so that it is free to castor; and thereafter, engaging the nose wheel after a specific time period after the nose wheel impacts the runway such that the nose wheel is steerable. The system for landing a flying wing type aircraft in a crosswind on a runway includes a steering system for steering the nose wheel, the steering system having a first condition wherein it controls the angular position of nose wheel and a second condition wherein the wheel is free to castor. A control system for moving the steering system from the first condition to the second condition upon the wheel contacting the runway and to move the steering system back to the first condition after a specified time after the wheel contacts the runway.
    • 在侧风中着陆飞翼型飞机的方法包括以下步骤:在与跑道碰撞时使鼻子着陆轮脱离,使得其可以自由转脚; 之后,在前轮撞击跑道之后的特定时间段之后接合前轮,使得前轮是可操纵的。 用于在跑道上的侧风中着陆飞翼型飞机的系统包括用于转向前轮的转向系统,该转向系统具有第一状态,其中控制前轮的角位置以及第二状态,其中车轮是自由的 蓖麻 一种控制系统,用于在车轮接触跑道时将转向系统从第一状态移动到第二状态,并且在车轮接触跑道的指定时间之后将转向系统移回到第一状态。
    • 8. 发明申请
    • Control system for an aircraft
    • 飞机控制系统
    • US20060108472A1
    • 2006-05-25
    • US10993497
    • 2004-11-19
    • Walter Clark
    • Walter Clark
    • B64C9/00
    • B64C3/16B64C5/02B64C9/12
    • The invention is a system for controlling an aircraft, the aircraft having a longitudinal axis, vertical and horizontal axis and right and left wings and right and left ailerons mounted on the right and left wings. In detail, the system includes a right stabilizer mounted to the right wing, the right stabilizer canted from the right wing such that the outer end thereof is down and deflectable about an axis of rotation parallel to the span axis of the stabilizer. A left stabilizer is mounted to the left wing, the left stabilizer canted from the left wing such that the outer end thereof is down and deflectable about an axis of rotation parallel to the span axis of the stabilizer. A control system is provided to simultaneously deflect the right aileron and stabilizer downward and the left aileron and stabilizer upward to turn left and to deflect the right aileron and stabilizer upward and the left aileron and stabilizer downward to turn right.
    • 本发明是一种用于控制飞行器的系统,飞行器具有纵向轴线,垂直和水平轴线,以及安装在右翼和左翼上的左右翼和左右副翼。 详细地说,该系统包括一个安装在右翼上的右侧稳定器,右侧稳定器从右侧翼倾斜,使得其外端向下并可绕平行于稳定器跨度轴线的旋转轴偏转。 左稳定器安装到左翼,左稳定器从左翼倾斜,使得其外端向下并且可绕平行于稳定器的跨度轴线的旋转轴线偏转。 提供一种控制系统,同时使右副翼和稳定器向下偏转,左副翼和稳定器向上转动左转,并使右副翼和稳定器向上偏转,左副翼和稳定器向下偏转右转。