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    • 13. 发明申请
    • CLEAN FUEL ELECTRIC MULTIROTOR AIRCRAFT FOR PERSONAL AIR TRANSPORTATION AND MANNED OR UNMANNED OPERATION
    • 用于个人空运和清洁或无人操作的清洁燃料电动多功能飞机
    • US20160200421A1
    • 2016-07-14
    • US14699945
    • 2015-04-29
    • Alakai Technologies Corporation
    • Brian D. Morrison
    • B64C13/18B64C27/08
    • B64C13/18B64C27/08B64D27/24B64D2027/026B64D2041/005G01C23/00G05D1/0077Y02T50/44Y02T50/54Y02T50/64Y02T90/36
    • Methods and systems for a full-scale vertical takeoff and landing manned or unmanned aircraft, having an all-electric, low-emission or zero-emission lift and propulsion system, an integrated ‘highway in the sky’ avionics system for navigation and guidance, a tablet-based motion command, or mission planning system to provide the operator with ‘drive by wire’ style direction control, and automatic on-board-capability to provide traffic awareness, weather display and collision avoidance. Automatic computer monitoring by a programmed triple-redundant digital autopilot computer controls each motor-controller and motor to produce pitch, bank, yaw and elevation, while simultaneously restricting the flight regime that the pilot can command, to protect the pilot from inadvertent potentially harmful acts that might lead to loss of control, or loss of vehicle stability. By using the results of the state measurements to inform motor control commands, the methods and systems contribute to the operational simplicity, reliability and safety of the vehicle.
    • 具有全电动,低排放或零排放的电梯和推进系统的全尺寸垂直起飞和着陆载人或无人飞机的方法和系统,“天空高速公路”导航和指导航空电子系统, 基于平板电脑的运动指令或任务规划系统,为操作员提供“电线驱动”风格方向控制,以及自动车载功能,提供交通意识,天气显示和避免碰撞。 通过编程的三重冗余数字自动驾驶仪计算机进行的自动计算机监控可控制每个电机控制器和电机产生俯仰,跳跃和偏航,同时限制飞行员可以指挥的飞行状态,以保护驾驶员免于潜在的有害行为 这可能导致控制失控或车辆稳定性的损失。 通过使用状态测量的结果来通知电机控制命令,这些方法和系统有助于车辆的操作简单性,可靠性和安全性。
    • 20. 发明申请
    • ALL-ELECTRIC MULTIROTOR FULL-SCALE AIRCRAFT FOR COMMUTING, PERSONAL TRANSPORTATION, AND SECURITY/SURVEILLANCE
    • 全电动多用途飞机全面规范,个人运输和安全/监控
    • US20150353192A1
    • 2015-12-10
    • US14452245
    • 2014-08-05
    • Alakai Technologies Corporation
    • Brian D. Morrison
    • B64C27/08B64C27/32
    • B64C27/08B64C27/32B64C27/56B64C27/57B64D27/24B64D31/04B64D31/06B64D43/00G01C23/005Y02T50/54Y02T50/62
    • Methods and systems for a full-scale vertical takeoff and landing manned or unmanned electric aircraft, having an all-electric, non-hydrocarbon-powered lift and propulsion system, an integrated avionics system for navigation and guidance, and simple joystick and throttle controls to provide the operator with ‘drive by wire’ style direction control. The vehicle employs counter-rotating sets of propellers and lift is provided by multiple pairs of small electric motors driving directly-connected, counter-rotating sets of propellers. Automatic computer monitoring by one or a plurality of programmed redundant digital motor management computer or autopilot controls each motor-controller and motor to produce pitch, bank and elevation, while simultaneously restricting the flight regime that the pilot can command. Sensed multi-axis information and parameter values about vehicle state are used to provide stable vehicle control and to detect when stable vehicle operating limits are about to be exceeded.
    • 具有全电动,非碳氢化合物驱动的电梯和推进系统的全尺寸垂直起飞和着陆载人或无人电动飞机的方法和系统,用于导航和引导的集成航空电子系统,以及简单的操纵杆和节气门控制 为操作员提供“通过线驱动”式方向控制。 车辆采用反旋转螺旋桨组,升降机由多对小型电动马达提供,这些小型电动机驱动直接连接,反向旋转的螺旋桨组。 由一个或多个编程的冗余数字电机管理计算机或自动驾驶仪进行的自动计算机监视控制每个电动机控制器和电动机以产生音调,组合和高程,同时限制驾驶员可以指挥的飞行状态。 用于检测车辆状态的多轴信息和参数值用于提供稳定的车辆控制,并检测何时将要超出稳定的车辆运行极限。