AMPHIBIOUS VERTICAL TAKEOFF AND LANDING UNMANNED SYSTEM AND FLYING CAR WITH MULTIPLE AERIAL AND AQUATIC FLIGHT MODES FOR CAPTURING PANORAMIC VIRTUAL REALITY VIEWS, INTERACTIVE VIDEO AND TRANSPORTATION WITH MOBILE AND WEARABLE APPLICATION
    211.
    发明申请
    AMPHIBIOUS VERTICAL TAKEOFF AND LANDING UNMANNED SYSTEM AND FLYING CAR WITH MULTIPLE AERIAL AND AQUATIC FLIGHT MODES FOR CAPTURING PANORAMIC VIRTUAL REALITY VIEWS, INTERACTIVE VIDEO AND TRANSPORTATION WITH MOBILE AND WEARABLE APPLICATION 审中-公开
    两侧垂直起飞和着陆无人系统和飞行汽车与多个空中和水上飞行模式捕捉全景虚拟现实视图,交互式视频和交通与移动和可穿戴应用程序

    公开(公告)号:WO2017081668A1

    公开(公告)日:2017-05-18

    申请号:PCT/IB2016/056829

    申请日:2016-11-12

    Abstract: An amphibious vertical takeoff and landing unmanned device comprises a modular and expandable waterproof body (802), a chassis (804), an outer body shell (806), a propulsion system, a propeller protection system, a surface skidding material platform, a landing system, control surfaces, a ballast, an onboard air compressor, an onboard electrolysis system, a waterproof through-body wire or antenna feed-through, a single or multiple-axis tilt-motor device (1025), a tilt fuselage device, a tilt wing device (1015), a battery, a power distribution board, a Global Positioning System module, a lost model alert, a cooling device (1041), a detachable impact absorbing skin or shell, vision aiding and orientative lights, hatches, quick connect payloads, a lap counter for racing, a flat or inclined launch platform or footing, claws, an apparatus for externally attaching and internally housing a cargo, a charging station, a partial vacuum device, a manually or automatically deployable parachute (1130), and an onboard or ground station electricity generator. A video capture, realtime broadcast, and video downlink system for an amphibious VTOL unmanned device and a collision avoidance, flight stabilization, and multi-rotor control system for an amphibious VTOL unmanned device are also provided.

    Abstract translation: 一种水陆两用垂直起降无人装置,包括模块化且可扩展的防水体(802),底盘(804),外体壳体(806),推进系统,推进器保护系统, 表面打滑材料平台,着陆系统,控制表面,镇流器,车载空气压缩机,车载电解系统,防水通体电线或天线馈通,单轴或多轴倾斜马达装置(1025 ),倾斜机身装置,倾斜翼装置(1015),电池,配电板,全球定位系统模块,遗失模型警报,冷却装置(1041),可拆卸的冲击吸收表皮或外壳,视觉 辅助和定位灯,舱口盖,快速连接有效载荷,用于比赛的圈数计数器,平坦或倾斜的发射平台或基座,爪,用于外部附接和内部容纳货物的装置,充电站,部分真空装置,手动 或自动部署 降落伞(1130)以及机载或地面站发电机。 还提供了用于两栖垂直起降无人设备的视频捕获,实时广播和视频下行链路系统,以及用于两栖垂直起降无人设备的避撞,飞行稳定和多旋翼控制系统。

    LUFTFAHRZEUG MIT IM RUMPF EINGEROLLTEN AUFBLASBAREN TRAGFLÄCHEN
    212.
    发明申请
    LUFTFAHRZEUG MIT IM RUMPF EINGEROLLTEN AUFBLASBAREN TRAGFLÄCHEN 审中-公开
    具有充气膨胀表面的飞机

    公开(公告)号:WO2017076498A1

    公开(公告)日:2017-05-11

    申请号:PCT/EP2016/001822

    申请日:2016-11-03

    Applicant: DAIMLER AG

    Abstract: Die Erfindung betrifft ein Luftfahrzeug (1), umfassend eine Rumpfeinheit (2) und zumindest eine aufblasbare Tragflächeneinheit (3), welche im nicht aufgeblasenen Zustand in der Rumpfeinheit (2) angeordnet ist und durch Aufblasen aus der Rumpfeinheit (2) heraus in eine Tragflächenstellung positionierbar ist. Erfindungsgemäß ist die zumindest eine Tragflächeneinheit (3) im nicht aufgeblasenen Zustand in die Rumpfeinheit (2) eingerollt und durch Aufblasen aus der Rumpfeinheit (2) ausrollbar.

    Abstract translation:

    本发明涉及一种飞行器(1),其包括主体部(2)和至少一个可充气水翼BEAR单位面积(3),其被布置在躯干单元(2)的收缩状态和通过膨胀 从机身单元(2)可以定位在Tragl @ chenstellung外。 发明Ä大街 所述至少一个翼型单元(3)在收缩状态下被卷入机身单元(2)中并且可以通过充气而从机身单元(2)中滚出。

    UNMANNED GLIDER SYSTEM FOR PAYLOAD DISPERSION
    213.
    发明申请
    UNMANNED GLIDER SYSTEM FOR PAYLOAD DISPERSION 审中-公开
    不间断的GLIDER系统用于PAYLOAD分配

    公开(公告)号:WO2016024276A1

    公开(公告)日:2016-02-18

    申请号:PCT/IL2015/050820

    申请日:2015-08-11

    Abstract: A disposable unmanned aerial glider (UAG) with pre-determined UAG flight capabilities. The UAG comprises a flight module comprising at least one aerodynamic arrangement; and a fuselage module comprising a container configured for storing therein a payload and having structural integrity. The container is pressurized so as to maintain structural integrity thereof at least during flight, so that the UAG flight capabilities are provided only when the container is pressurized.

    Abstract translation: 具有预定UAG飞行能力的一次性无人驾驶滑翔机(UAG)。 UAG包括飞行模块,其包括至少一个空气动力学装置; 以及机身模块,其包括被配置为在其中存储有效载荷并具有结构完整性的容器。 容器被加压以至少在飞行期间保持其结构完整性,使得仅当容器被加压时才提供UAG飞行能力。

    STOWABLE AND DEPLOYABLE UNMANNED AERIAL VEHICLE
    214.
    发明申请
    STOWABLE AND DEPLOYABLE UNMANNED AERIAL VEHICLE 审中-公开
    可持续和可配置的无人机

    公开(公告)号:WO2015123004A1

    公开(公告)日:2015-08-20

    申请号:PCT/US2015/012417

    申请日:2015-01-22

    Abstract: An unmanned aerial vehicle (UAV) can be deployed from a small stowed package for flight and stowed back into the package after the flight is complete is disclosed. The UAV is retracted to a volume that is less than half of its fully deployed volume. This allows the UAV to be transported to any desired field position on a truck or other convenient transportation. The UAV may also be launched from a ship deck. In a further aspect, the flexible deployment of the UAV will allow a single UAV to be used in place of multiple types of UAVs.

    Abstract translation: 飞行完成后,可以从一个小型收起的包装中部署无人驾驶飞行器(UAV)并收回包装。 UAV被缩回到小于其完全部署卷的一半的卷。 这样可以将无人机运送到卡车上的任何所需的现场位置或其他方便的交通工具。 无人机也可以从船甲板上发射。 在另一方面,UAV的灵活部署将允许使用单个UAV来代替多种类型的UAV。

    AIRCRAFT
    215.
    发明申请
    AIRCRAFT 审中-公开
    飞机

    公开(公告)号:WO2007021011A3

    公开(公告)日:2014-01-23

    申请号:PCT/JP2006316271

    申请日:2006-08-18

    Abstract: [PROBLEMS] An aircraft that can be transported in a small space and has high performance. [MEANS FOR SOLVING PROBLEMS] An aircraft in which a kite wing (300) is attached to an aircraft body (100) via struts (210, 220) and a propeller (500) is rotatably supported by a shaft. A propeller guard section (120) for guarding the outer circumference of the propeller (500) is provided at the aircraft body (100). The struts (210, 220) can be fixed to the propeller guard section (120).

    Abstract translation: [问题]可在小空间内运输,性能高的飞机。 用于解决问题的手段通过支柱(210,220)和螺旋桨(500)将风筝翼(300)附接到飞行器主体(100)的飞行器由轴可旋转地支撑。 用于防护螺旋桨(500)的外周的螺旋桨防护部(120)设置在飞行器主体(100)处。 支柱(210,220)可以固定到螺旋桨保护部分(120)。

    FOLDING CONFIGURATION FOR AIR VEHICLE
    216.
    发明申请
    FOLDING CONFIGURATION FOR AIR VEHICLE 审中-公开
    空中车辆的折叠配置

    公开(公告)号:WO2013172992A1

    公开(公告)日:2013-11-21

    申请号:PCT/US2013/035267

    申请日:2013-04-04

    CPC classification number: B64C3/56 B64C39/024 B64C2201/102 F42B10/16 Y02T50/14

    Abstract: An air vehicle, as well as a method for folding an air vehicle for storage, may include a fuselage and a wing connected to the fuselage. The wing may include two ends positioned opposite from each other, and the wing may be substantially perpendicular to the fuselage. At least one of the ends may define a space therebetween the fuselage and the wing. The space may be sized to receive a potion of the wing when the wing is wrapped around the fuselage.

    Abstract translation: 一种空中飞行器以及用于折叠用于存储的空中飞行器的方法可以包括机身和连接到机身的机翼。 机翼可以包括彼此相对定位的两个端部,并且机翼可以基本上垂直于机身。 端部中的至少一个可以限定机身和机翼之间的空间。 当机翼围绕机身缠绕时,该空间的大小可以接收机翼的一部分。

    MORPHING AIRCRAFT
    217.
    发明申请
    MORPHING AIRCRAFT 审中-公开
    MORPHING飞机

    公开(公告)号:WO2010027801A3

    公开(公告)日:2010-05-27

    申请号:PCT/US2009054917

    申请日:2009-08-25

    Abstract: A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

    Abstract translation: 实现多模式位置和伪装用于有效载荷的变形飞机变形飞机包括基本上圆柱形的机身,其包括被配置为具有第一端和第二端的包装容器的形状。一组翼结合到机身。该组 的翼部包括第一位置,其中所述一组翼从机身向外延伸,并且第二位置,其中该组翼向内朝向机身A缩回。尾部联接到圆柱形机身的第二端。尾部包括第一位置 其中尾部从机身向外延伸,而第二位置则尾部朝向机身向内缩进。螺旋桨安装在机身的第一端。发动机机械地联接到螺旋桨发动机被封闭在机身内并且动力 螺旋桨

    MORPHING AIRCRAFT
    218.
    发明申请
    MORPHING AIRCRAFT 审中-公开
    变形飞机

    公开(公告)号:WO2010027801A2

    公开(公告)日:2010-03-11

    申请号:PCT/US2009/054917

    申请日:2009-08-25

    Abstract: A morphing aircraft that is achieves multi- modality location and camouflage for payload emplacement The morphing aircraft includes a substantially cylindrical fuselage including a shape configured as a packaging container with a first end and a second end A set of wings is coupled to the fuselage The set of wings includes a first position where the set of wings is extended outwards from the fuselage and a second position where the set of wings is retracted inwards towards the fuselage A tail is coupled to the second end of the cylindrical fuselage The tail includes a first position where the tail is extended outward from the fuselage and a second position where the tail is retracted inward towards the fuselage A propeller is mounted to the first end of the fuselage An engine is mechanically coupled to the propeller The engine is enclosed within the fuselage and powers the propeller.

    Abstract translation: 实现用于有效载荷安置的多模式位置和伪装的变形飞行器变体飞机包括基本上圆柱形的机身,该机身包括被配置为包装容器的形状,该包装容器具有第一端和第二端, 机翼被耦合到机身。该组机翼包括第一位置和第二位置,其中该组机翼从机身向外延伸,在第二位置该组机翼朝向机身A向内缩回。尾部耦合到机身的第二端 圆柱形机身尾部包括尾部从机身向外延伸的第一位置和尾部朝着机身向内缩回的第二位置。螺旋桨安装到机身的第一端。发动机机械地耦合到螺旋桨上。 发动机封闭在机身内并为螺旋桨提供动力。

    METHODS AND APPARATUS FOR ADJUSTABLE SURFACES
    220.
    发明申请
    METHODS AND APPARATUS FOR ADJUSTABLE SURFACES 审中-公开
    可调表面的方法和装置

    公开(公告)号:WO2009096967A1

    公开(公告)日:2009-08-06

    申请号:PCT/US2008/052570

    申请日:2008-01-31

    Abstract: Methods and apparatus for systems having deployable elements according to various aspects of the present invention comprise a system including a deployable surface and an adaptive actuator including a polymer foam. In one embodiment, the system comprises a vehicle including a deployable wing comprising an exterior surface. The exterior surface may be adjusted by adjusting the shape, size, position, and/or orientation of the adaptive actuator.

    Abstract translation: 根据本发明的各个方面的具有可展开元件的系统的方法和装置包括包括可展开表面和包括聚合物泡沫的自适应致动器的系统。 在一个实施例中,系统包括包括可展开的机翼的车辆,其包括外表面。 可以通过调节自适应致动器的形状,尺寸,位置和/或取向来调节外表面。

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