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    • 87. 发明申请
    • ENERGY CELL REGENERATIVE SYSTEM FOR ELECTRICALLY POWERED AIRCRAFT
    • 用于电动飞机的能源电池再生系统
    • WO2015195856A1
    • 2015-12-23
    • PCT/US2015/036332
    • 2015-06-18
    • ELECTRONAIR LLC
    • WALTER-ROBINSON, Dale Martin
    • B60L11/12B64D41/00
    • B64D27/24B64D41/00B64D41/007B64D2027/026H02J7/0068H02J7/32H02J7/345H02K7/1823H02K53/00H02P4/00Y02T50/53Y02T50/54Y02T50/64Y10S74/09
    • A system for providing regenerative power for an aircraft to sustain flight includes multiple energy cells disposed within the aircraft, the energy cells being configured to supply power to a propulsion motor and electronics of the aircraft, a fan generator harnessing propeller blast created by an aircraft propeller and converting kinetic energy of the propeller blast into electrical energy, a charger receiving the electrical energy generated by the fan generator and using the electrical energy to recharge one or more of the energy cells, and a power transfer switch selectively connecting one of the energy cells to the propulsion motor and electronics of the aircraft, such that the energy cells are rotated one at a time to power the propulsion motor and electronics. During recharging, the one or more of the energy cells are disconnected by the power transfer switch.
    • 用于为飞行器提供再生能量以维持飞行的系统包括设置在飞行器内的多个能量单元,所述能量单元被配置为向飞行器的推进马达和电子设备供电,风力发电机利用由飞行器螺旋桨产生的螺旋桨 并且将所述螺旋桨鼓风的动能转换成电能;充电器,接收由所述风扇发生器产生的电能并且使用所述电能对所述能量单元中的一个或多个进行再充电;以及功率传输开关,其选择性地连接所述能量单元 到飞机的推进马达和电子设备,使得能量单元一次一个旋转以为推进电机和电子设备供电。 在再充电期间,一个或多个能量单元由电力转换开关断开。
    • 88. 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
    • WO2015168320A1
    • 2015-11-05
    • PCT/US2015/028345
    • 2015-04-29
    • ALAKAI TECHNOLOGIES CORPORATION
    • MORRISON, Brian, D.
    • B64C27/08B64C27/32B64C27/68
    • 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 这可能导致失去控制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。