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    Aerial unit and method for elevating payloads
    3.
    发明授权
    Aerial unit and method for elevating payloads 有权
    提升有效载荷的空中单元和方法

    公开(公告)号：US09260202B2

    公开(公告)日：2016-02-16

    申请号：US13847583

    申请日：2013-03-20

    申请人： Gabriel Shachor ,  Shy Cohen ,  Ronen Keidar

    发明人： Gabriel Shachor ,  Shy Cohen ,  Ronen Keidar

    IPC分类号： B64C27/08 ,  B64C27/20 ,  B64F1/12 ,  B64C39/02 ,  B64C29/04 ,  B64C27/04 ,  B64F1/00

    CPC分类号： B64F1/12 ,  B64C27/04 ,  B64C27/08 ,  B64C29/04 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/148 ,  B64F1/007 ,  B64F1/125

    摘要： A system that includes a ground unit that includes: a takeoff and landing platform; a landing and takeoff assisting module; and a housing. The takeoff and landing platform is arranged to hold and support an aerial unit during a first part of a landing process of the aerial unit and a first part of takeoff process of the aerial unit. The aerial unit is coupled to the ground unit via a connecting element. The effective length of the connecting element increases during the takeoff process and decreases during the landing process. The landing and takeoff assisting module is coupled to the takeoff and landing platform and is arranged to (a) lower the takeoff and landing platform into the housing during a second part of the landing process and (b) elevate the takeoff and landing platform during a second part of the takeoff process.

    摘要翻译： 一种包括地面单元的系统，包括：起降平台; 着陆和起飞辅助模块; 和住房。 起飞和着陆平台布置成在天线单元的着陆过程的第一部分和天线单元的起飞过程的第一部分期间保持和支撑天线单元。 天线单元通过连接元件耦合到接地单元。 连接元件的有效长度在起飞过程中增加，在着陆过程中减小。 着陆和起飞辅助模块耦合到起飞和着陆平台，并且被布置成（a）在着陆过程的第二部分期间将起飞和着陆平台降低到壳体中，并且（b）在起飞和着陆平台期间提升起飞和着陆平台 起飞过程的第二部分。

    Systems and methods for controlling an aerial unit
    4.
    发明授权
    Systems and methods for controlling an aerial unit 有权
    用于控制天线单元的系统和方法

    公开(公告)号：US09056687B2

    公开(公告)日：2015-06-16

    申请号：US13759084

    申请日：2013-02-05

    申请人： Gabriel Shachor ,  Shy Cohen ,  Ronen Keidar ,  Zvi Yaniv

    发明人： Gabriel Shachor ,  Shy Cohen ,  Ronen Keidar ,  Zvi Yaniv

    IPC分类号： B64C27/00 ,  B64C27/08 ,  B64F1/12 ,  B64C39/02 ,  B64C29/04 ,  B64C27/04

    CPC分类号： B64F1/12 ,  B64C27/04 ,  B64C27/08 ,  B64C29/04 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/148 ,  B64F1/007 ,  B64F1/125

    摘要： An aerial unit, a method and a system are provide, the system includes a ground unit; an aerial unit and a connecting element arranged to connect the ground unit to the aerial unit. The ground unit may include a connecting element manipulator, a ground unit controller for controlling the connecting element manipulator; and a ground unit location sensor arranged to generate ground unit location information indicative of a location of the ground unit. The wherein the aerial unit may include a first propeller, a frame, a first propeller motor, at least one steering element; and an aerial unit location sensor arranged to generate aerial unit location information indicative of a location of the aerial unit. At least one of the ground unit and the aerial unit includes a controller that is arranged to control, at least in response to a relationship between the aerial unit location information and the ground unit location information, at least one of the first propeller motor and the at least one steering element to affect at least one of the location of the aerial unit and an orientation of the aerial unit.

    摘要翻译： 提供一种天线单元，方法和系统，该系统包括接地单元; 天线单元和布置成将地面单元连接到天线单元的连接元件。 接地单元可以包括连接元件操纵器，用于控制连接元件操纵器的接地单元控制器; 以及地面单元位置传感器，布置成产生指示地面单元的位置的地面单元位置信息。 其中，所述天线单元可以包括第一螺旋桨，框架，第一螺旋桨电动机，至少一个操纵元件; 以及天线单元位置传感器，布置成产生指示天线单元的位置的天线单元位置信息。 地面单元和天线单元中的至少一个包括控制器，其被布置为至少响应于天线单元位置信息和地面单元位置信息之间的关系来控制第一螺旋桨电动机和 至少一个操纵元件，以影响天线单元的位置和天线单元的定向中的至少一个。

    Personal flight vehicle and system
    6.
    发明申请
    Personal flight vehicle and system 失效
    个人飞行器和系统

    公开(公告)号：US20040089763A1

    公开(公告)日：2004-05-13

    申请号：US10293826

    申请日：2002-11-12

    发明人： Scott D. Redmond

    IPC分类号： B64C027/22 ,  B64C039/00

    CPC分类号： B64C39/026 ,  B64C29/04 ,  B64C39/00 ,  B64C39/001 ,  B64D27/24 ,  Y02T50/44 ,  Y02T50/62

    摘要： Various methods, apparatuses, and systems in which an electric-energy lifting panel levitates a user secured to the electric-energy lifting panel. The electric-energy lifting panel includes a first capacitive plate and a second capacitive plate having different geometric dimensions to generate a net-directional force. An ion conditioner ion enhances air around the first capacitive plate and the second capacitive plate.

    摘要翻译： 其中电能提升面板使固定在电能提升面板上的使用者浮起的各种方法，装置和系统。 电能提升面板包括具有不同几何尺寸的第一电容板和第二电容板，以产生网络力。 离子调节剂离子增强了第一电容板和第二电容板周围的空气。

    Levity aircraft design
    7.
    发明授权
    Levity aircraft design 失效
    利空飞机设计

    公开(公告)号：US5881970A

    公开(公告)日：1999-03-16

    申请号：US434981

    申请日：1995-05-04

    申请人： Carl Wayne Whitesides

    发明人： Carl Wayne Whitesides

    IPC分类号： B64B1/02 ,  B64B1/36 ,  B64C1/34 ,  B64C29/04 ,  B64C15/02

    CPC分类号： B64C29/04 ,  B64B1/02 ,  B64B1/36 ,  B64C1/34

    摘要： An aircraft with automated means to transport. Spherical or one of its segments, without airfoils for lift or guidance. Means for flight are housed within the aircraft. The outer-most sureface is configured to disrupt the air-flow, over its surfaces, in flight. This, to reduce skin-friction and drag coefficients, and mollify heat build-up on the skins outer surfaces as speeds increase to and beyond mach 1. The weight of gas per unit volume, with temperature variations, is the means to reduce the gross-weight and adjust for temperature and weight changes during flight. Propulsion, within the propulsion component, is provided by turbojet engines. They are secured within an inner compression pod and an outer combustion pod. The compression pod and the attached vertical-air-duct, rotate through three hundred sixty degrees, as the means for directional guidance and direct thrust. Augmented power-thrust-tubes extend outward from the combustion pod to the mid-horizontal circumference of the aircraft. Control baffles, on each thrust-tube, check, deflect and regulate the engines' thrust to control the motivity of the aircraft. Struts retract for flight and are extended for landing. These electro-hydraulic struts, level, raise and lower the aircraft for direct ground level support operations. The aircraft has the means to maintain a horizontal flight attitude. For flight aptness the aircraft has an internal, mechanical and scientific means, for vertical ascent and vertical descent without horizontal motivity, to hover and maintain a position and altitude. And during horizontal flight, climb and descend, and perform heading changes. These flight means are all performed in the aircrafts' horizontal attitude.

    摘要翻译： 一架具有自动化装置的飞机。 球形或其中一个段，没有用于升降或引导的翼型。 飞机的方式安置在飞机内。 最外面的表面配置为在飞行中破坏其表面上的空气流。 这是为了减少皮肤摩擦和阻力系数，并且随着速度增加到超过马赫1，在皮肤外表面上的热积累变得虚弱。每单位体积的气体重量与温度变化是减少毛重 重量，并适应飞行过程中的温度和重量变化。 在推进组件内的推进由涡轮喷气发动机提供。 它们固定在内部压缩舱和外部燃烧舱内。 压缩舱和连接的垂直风道，旋转三百六十度，作为定向导向和直接推力的手段。 增强的动力推力管从燃烧舱向外延伸到飞行器的中部水平周边。 控制挡板，在每个推力管上，检查，偏转和调节发动机的推力以控制飞机的动力。 Struts撤回飞行，并延长着陆。 这些电动液压支柱，水平，升高和降低飞机直接地面水平支持操作。 飞机有维持水平飞行姿态的手段。 对于飞行适应性，飞机具有内部，机械和科学的手段，用于垂直上升和垂直下降，没有水平动力，可以悬停并保持位置和高度。 在水平飞行中，爬升和下降，并执行航向变化。 这些飞行手段都是以飞机的横向姿态进行的。

    Multi-Propulsion Design for Unmanned Aerial Systems
    10.
    发明申请
    Multi-Propulsion Design for Unmanned Aerial Systems 审中-公开
    无人空中系统的多推进设计

    公开(公告)号：US20170015417A1

    公开(公告)日：2017-01-19

    申请号：US14839960

    申请日：2015-08-29

    申请人： Reference Technologies Inc

    发明人： Allen Paul Bishop

    IPC分类号： B64C39/02 ,  B64C27/82 ,  B64C29/04

    CPC分类号： B64C39/024 ,  B64C27/20 ,  B64C27/82 ,  B64C29/04 ,  B64C2027/8227 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/108 ,  B64D2027/026

    摘要： A propulsion system for a ducted fan vertical takeoff and landing aircraft (VTOL) powered by multiple electric motors with two, counter rotating electric motors comprising the primary thrust generation within a ducted fan component and 3 or more external electric motors providing lift, stability and directional control of the aircraft. Through the use of counter rotating ducted fans, the aircraft does not require the need for internal stators—either fixed or adjustable angle. Power to the electric motors is sourced by either onboard batteries, a ground based power source via a ground to aircraft tether, or an on board fuel cell or combustion engine driving an alternator.

    摘要翻译： 一种用于由具有两个逆向旋转电动机的多个电动机驱动的管道风扇垂直起降飞机（VTOL）的推进系统，其包括在管道风扇部件内的主要推力产生和提供升力，稳定性和定向的3个或更多个外部电动马达 控制飞机。 通过使用反向旋转管道风扇，飞机不需要内部定子 - 固定或可调角度。 电动机的功率来自车载电池，地面电源通过地面到飞机系绳，或车载燃料电池或驱动交流发电机的内燃机。