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    TRAILER FOR AUTONOMOUS VEHICLE
    171.
    发明申请
    TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
    自动车辆拖车

    公开(公告)号：WO2015038697A3

    公开(公告)日：2015-10-29

    申请号：PCT/US2014055075

    申请日：2014-09-11

    Applicant: SILICIS TECHNOLOGIES INC

    Inventor： STIGLER MICHAEL J ,  SETAR NICHOLAS JAMES

    IPC: B64F1/12

    CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    Abstract translation: 所公开的实施例包括用于由命令和控制接口控制的自主车辆的拖车。 拖车包括拖车主体，其构造成将自主车辆保持在未部署的构造中。 拖车还以部署的配置锚定自主车辆。 提供了系绳，其具有联接到拖车主体的第一端和被配置为联接到自主车辆的第二端。 使用绞盘来调节系绳的长度以在未部署的配置和部署配置之间移动自主车辆。 此外，通信系统与命令和控制界面以及自主车辆进行通信，以控制自动车辆在未部署配置和部署配置之间的移动。

    HYBRID VTOL VEHICLE
    172.
    发明申请
    HYBRID VTOL VEHICLE 审中-公开
    混合动力车

    公开(公告)号：WO2014210393A1

    公开(公告)日：2014-12-31

    申请号：PCT/US2014/044457

    申请日：2014-06-26

    Applicant: PLIMP, INC.

    Inventor： EGAN, James, C. ,  EGAN, Joel, D.

    IPC: B64B1/00

    CPC classification number: B64B1/20 ,  B64B1/14 ,  B64B1/22 ,  B64B1/28 ,  B64B1/30 ,  B64B1/34 ,  B64B1/38 ,  B64B1/58 ,  B64B1/60 ,  B64B1/70 ,  B64B2201/00 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/104

    Abstract: A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.

    Abstract translation: 一种具有被配置为提供静压浮力的封套的混合垂直起降车辆，附接到信封上的机身，并且具有从相对侧延伸的至少一对翼片，以产生通过运动的动力升降，以及每个机翼上的推力发生装置， 围绕围绕纵向轴线的侧壁的轴线旋转，以提供垂直起飞或着陆能力。 理想情况下，信封提供负静液压升力，以提高低速和地面的稳定性。

    LIGHTER-THAN-AIR SYSTEMS, METHODS, AND KITS FOR OBTAINING AERIAL IMAGES
    173.
    发明申请
    LIGHTER-THAN-AIR SYSTEMS, METHODS, AND KITS FOR OBTAINING AERIAL IMAGES 审中-公开
    用于获取空中图像的轻 - 空气系统，方法和套件

    公开(公告)号：WO2012118731A2

    公开(公告)日：2012-09-07

    申请号：PCT/US2012/026716

    申请日：2012-02-27

    Applicant: CIAMPA, John, A.

    Inventor： CIAMPA, John, A.

    IPC: B64B1/58

    CPC classification number: B64C39/024 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/146 ,  B64D47/08

    Abstract: Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various structural arrangements of lighter-than-air systems for accomplishing planned ascent, drift, and/or descent and obtaining aerial images are described.

    Abstract translation: 描述了用于获取航拍图像的比空中轻的系统，方法和套件。 例如，描述了用于确定轻于空气系统的计划上升，漂移和/或下降的各种方法。 另外，描述了用于完成计划上升，漂移和/或下降以及获得航拍图像的轻于空气系统的各种结构布置。

    AERIAL VEHICLE AND METHOD OF FLIGHT
    174.
    发明申请
    AERIAL VEHICLE AND METHOD OF FLIGHT 审中-公开
    空中客车和飞行方法

    公开(公告)号：WO2011117619A3

    公开(公告)日：2011-11-17

    申请号：PCT/GB2011050562

    申请日：2011-03-22

    Applicant: ATHENE WORKS LTD ,  DEAKIN NICHOLAS JAMES

    Inventor： DEAKIN NICHOLAS JAMES

    IPC: B64B1/00

    CPC classification number: B64B1/02 ,  B64B1/08 ,  B64B1/10 ,  B64B1/12 ,  B64B1/14 ,  B64B1/20 ,  B64B1/38 ,  B64B1/64 ,  B64B2201/00 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/167 ,  H01Q1/36 ,  H01Q9/27

    Abstract: An aerial vehicle is described which comprises: a first compartment (13) for holding a lighter than air gas; a second compartment (6, 4) for holding atmospheric air and having an inlet and an outlet; a solar panel (41) for converting sunlight into electricity; a compressor (242) for pumping atmospheric air through the inlet into the second compartment; control means (1,3) for controlling the pitch and yaw of the vehicle; and a controller (209) for controlling the buoyancy of the vehicle via the compressor and the outlet such that the vehicle is either lighter than the surrounding air and rising or heavier than the surrounding air and falling, and for controlling the control means such that the rising and falling motion includes a horizontal component. In another embodiment the solar panel is replaced by an engine and a fuel tank for storing fuel for the engine is also provided. The aerial vehicle can remain airborne for extended periods by using buoyancy propulsion. In the embodiments including a solar panel, a system including a light transmission station may be provided to supply energy to the solar panel from the light transmission station rather than relying on the incident sunlight alone. A method of flight using buoyancy propulsion is also described.

    Abstract translation: 描述了一种飞行器，其包括：用于保持比气体气体轻的第一隔室（13）; 用于保持大气空气并具有入口和出口的第二隔间（6,4）; 用于将太阳光转换成电的太阳能电池板（41） 压缩机（242），用于将大气通过所述入口排入所述第二隔室; 控制装置（1,3），用于控制车辆的俯仰和偏航; 以及用于经由压缩机和出口控制车辆的浮力的控制器（209），使得车辆比周围空气要轻，并且比周围空气上升或者重，并且为了控制控制装置， 上升和下降运动包括水平分量。 在另一个实施例中，太阳能电池板被发动机代替，并且还提供了用于储存用于发动机的燃料的燃料箱。 航空器可以通过使用浮力推进长时间保持空中。 在包括太阳能电池板的实施例中，可以提供包括光传输站的系统，以从光传输站向太阳能电池板提供能量，而不是仅依赖于入射的太阳光。 还描述了使用浮力推进的飞行方法。

    AIRSHIP AND METHOD OF OPERATION
    176.
    发明申请
    AIRSHIP AND METHOD OF OPERATION 审中-公开
    航空和操作方法

    公开(公告)号：WO2004000642A1

    公开(公告)日：2003-12-31

    申请号：PCT/CA2003/000945

    申请日：2003-06-25

    Applicant: 21ST CENTURY AIRSHIPS INC. ,  COLTING, Hokan

    Inventor： COLTING, Hokan

    IPC: B64B1/00

    CPC classification number: B64B1/34 ,  B64B1/02 ,  B64B1/32 ,  B64C21/02 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  Y02T50/166

    Abstract: An airship (20) has a generally spherical shape and has an internal envelope (24) for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system (36, 38) that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7 % full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module (180) that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors (44, 46) of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit (52) that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.

    Abstract translation: 飞艇（20）具有大致球形并且具有用于容纳诸如氦气或氢气的提升气体的内部封壳（24）。 飞艇有一个推进和控制系统（36,38），允许飞行到期望的游荡地点，并在该地点保持一段时间。 在一个实施例中，当内部信封充满提升气体的7％时，飞艇可以实现中性浮力，并且可以具有约6万英尺的服务天花板。飞艇具有可以包括通信设备 ，或监控设备，或两者兼而有之。 飞艇可以从地面站遥控。 飞艇具有太阳能电池阵列，推进和控制系统的电机（44,46）由阵列获得的功率驱动。 飞艇还具有可用于驱动电动机的辅助动力单元（52）。 飞艇可以有一个推动螺旋桨，有助于驾驶飞艇，还可以使球形飞艇进一步向后流动。 在一个实施例中，飞艇可以在高度加油以允许延长的游荡。

    레저 또는 인명구조용 날개없는 무인 비행체
    179.
    发明公开
    레저 또는 인명구조용 날개없는 무인 비행체 审中-实审
    Wingless无人机用于休闲或救生

    公开(公告)号：KR1020170115331A

    公开(公告)日：2017-10-17

    申请号：KR1020160042844

    申请日：2016-04-07

    Applicant: 하상균

    Inventor： 하상균

    IPC: B64C39/02 ,  B64C21/02 ,  B64D47/08 ,  B64D45/00 ,  B63C9/01

    CPC classification number: B64C39/024 ,  B63C9/01 ,  B64C21/02 ,  B64C2201/02 ,  B64C2201/042 ,  B64C2201/048 ,  B64C2201/10 ,  B64C2201/101 ,  B64C2201/16 ,  B64D45/00 ,  B64D47/08

    Abstract: 본발명은레저또는인명구조용날개없는무인비행체에관한것으로, 날개를사용하지않고비행하면서사람이탑승할수 있는레저용, 또는인명구조를위한구급용으로사용하기위한것이다. 이를위하여본 발명은, 사람이탈 수있도록중앙에개구부가형성되고단면형상이원통인케이스로이루어지는비행몸체부, 비행몸체부의케이스내부에구비되며모터와팬을케이스에내장하고팬에의해공기를유입및 토출시키는공기유입구와공기토출구를비행몸체부의케이스상부와하부에각각구비하여팬에의한상부공기의흡입과하부로의강제토출을통해비행몸체부에비행을위한추력을작용시키는추력발생부, 비행몸체부의케이스외측에구비되며사용자에의한키 조작을통해모터및 팬동작을제어하여추력발생부의추력을비행몸체부에작용시키거나정지시키는비행제어부, 및추력발생부와비행제어부및 시스템의각 부에동작전원을공급하는전원공급부를포함하는무인비행체를제공하여, 레저용또는인명구조를위한구급용으로사용가능하게한다.

    Abstract translation: 本发明的目的是用作急救拯救生命或休闲翼没有，尽管你可以不用翼人在船上或在救生员休闲无人看管的车辆飞行。 本发明的这一点，在中央具有开口，使得人们能逃脱被设置在壳体的内部由一个内置的和风扇电动机wapaen的情况下和飞行上的横截面的圆柱形壳体入口空气由形状的主体飞行体部形成 其通过在进气口和所述风扇的空气排出开口的上部空气的下部吸入或强制喷射到分别设置在壳体上部飞行体和推力的中部的动作为飞行下飞行体生成单元喷射力，飞行 每个飞行控制部，以及推力发生单元和飞行控制和系统的设置的情况下的主体的外部的推力产生部的动作由用户给子飞行体或止挡部，以控制通过键操作电机和风扇操作 提供无人驾驶飞行器，包括用于供应工作功率到被提供用于休闲或救生急救的电源。

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