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    INTELLIGENT NOISE MONITORING DEVICE AND NOISE MONITORING METHOD USING THE SAME
    252.
    发明申请
    INTELLIGENT NOISE MONITORING DEVICE AND NOISE MONITORING METHOD USING THE SAME 审中-公开
    智能噪声监测装置和噪声监测方法

    公开(公告)号：US20160025551A1

    公开(公告)日：2016-01-28

    申请号：US14805730

    申请日：2015-07-22

    Applicant: DOOSAN HEAVY INDUSTRIES CONSTRUCTION CO., LTD.

    Inventor： Sang Jin LEE

    IPC: G01H3/04 ,  G08G5/00 ,  G01H3/10 ,  G05D1/12

    CPC classification number: G01H3/04 ,  B64C2201/027 ,  B64C2201/123 ,  G01H3/00 ,  G01H3/10 ,  G08G5/003

    Abstract: An intelligent noise monitoring device includes a self-flying moving module, a noise measurement module equipped in the moving module to measure noise of a target to be detected, a control module configured to control the moving module and the noise measurement module; and a communication module configured to communicate with a ground control center, wherein the intelligent noise monitoring device flies to a location to be detected to measure the noise of the location to be detected so as to determine whether or not the measured noise is in an abnormal state.

    Abstract translation: 一种智能噪声监测装置，包括：自动移动模块，安置在移动模块中的噪声测量模块，用于测量待检测目标的噪声;控制模块，被配置为控制移动模块和噪声测量模块; 以及通信模块，被配置为与地面控制中心进行通信，其中所述智能噪声监测装置飞行到要检测的位置，以测量待检测位置的噪声，以便确定所测量的噪声是否处于异常状态 州。

    PAYLOAD SHROUD FOR AIR VEHICLE
    253.
    发明申请
    PAYLOAD SHROUD FOR AIR VEHICLE 有权
    空中交通工具

    公开(公告)号：US20160009371A1

    公开(公告)日：2016-01-14

    申请号：US14105988

    申请日：2013-12-13

    Applicant: AAI Corporation

    Inventor： MONICA ATZERT ,  Jason Wallace ,  Robert Hurn ,  Doug Deardorff ,  Terry Zeleny

    IPC: B64C7/00 ,  B64C39/02 ,  B64D47/08

    CPC classification number: B64C7/00 ,  B64C1/36 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64D1/08 ,  B64D47/08

    Abstract: A UAV includes a body. The body defines a payload opening 14. The payload opening is circular, but any shape may be used. A payload of the UAV is arranged in the payload opening. The payload may be a camera, sensors, a package, etc. A payload shroud may be installed which prohibits or reduced ingress of foreign material via payload opening. A payload shroud may include a diverter. The diverter may act as a barrier wall preventing the water or debris from entering the body of the UAV. The diverter should fit flush with the payload opening in the body of the UAV.

    Abstract translation: 无人机包括一个身体。 主体限定有效载荷开口14.有效载荷开口是圆形的，但是可以使用任何形状。 无人机的有效载荷被布置在有效载荷开口中。 有效载荷可以是相机，传感器，包装等。可以安装有效载荷罩，其可以通过有效载荷打开来禁止或减少外来物质的进入。 有效载荷罩可以包括转向器。 分流器可以用作防止水或碎屑进入无人机身体的障碍壁。 转向器应与无人机身体的有效载荷齐平。

    UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING
    256.
    发明申请
    UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING 审中-公开
    无人驾驶的空中客车和起飞方法

    公开(公告)号：US20150183520A1

    公开(公告)日：2015-07-02

    申请号：US14416035

    申请日：2013-07-19

    Applicant: Andrew Charles ELSON

    Inventor： Andrew Charles Elson

    IPC: B64D5/00 ,  B64C39/02

    CPC classification number: B64D5/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/104 ,  B64C2201/122 ,  B64C2201/123 ,  B64C2201/162 ,  B64C2201/187

    Abstract: A method of launching a powered unmanned aerial vehicle, the method comprising lifting the vehicle by attachment to a lighter-than-air carrier from a substantially ground-level location to an elevated altitude, wherein the vehicle is prevented from entering its flight mode during ascent, causing the vehicle to detach from the carrier while the velocity of the vehicle relative to the carrier is substantially zero, the vehicle thereafter decreasing in altitude as it accelerates to a velocity where it is capable of preventing any further descent and can begin independent sustained flight.

    Abstract translation: 一种发射有功无人驾驶飞行器的方法，该方法包括通过从基本上地平面位置到高架高度附接到比轻空载体提升车辆，其中在上升期间车辆被阻止进入其飞行模式 ，当车辆相对于承运人的速度基本上为零时，导致车辆从载体上脱离，随后车辆随着其高度减小到能够防止任何进一步下降并能够开始独立持续飞行的速度 。

    Aerial photogrammetry and aerial photogrammetric system
    259.
    发明授权
    Aerial photogrammetry and aerial photogrammetric system 有权
    空中摄影测量和航空摄影测量系统

    公开(公告)号：US08953933B2

    公开(公告)日：2015-02-10

    申请号：US14059784

    申请日：2013-10-22

    Applicant: Kabushiki Kaisha TOPCON

    Inventor： Fumio Ohtomo ,  Hitoshi Otani ,  Kazuki Osaragi ,  Tetsuji Anai

    IPC: G03B39/00 ,  G01C11/00 ,  G01C11/02

    CPC classification number: G01C11/00 ,  A01B79/005 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/127 ,  G01C11/025 ,  G05D1/0094 ,  G05D1/104

    Abstract: Aerial photogrammetry is provided by using two or more flying vehicles, each equipped with a GPS device and an image pickup unit. This method comprises setting up two or more photographing points and setting up a photographing point area, respectively, with each of the photographing points as the center, measuring a position of the flying vehicle by the GPS device, a step where each of the flying vehicle reaches each corresponding photographing point area and maintains the position of the photographing point area, acquiring a time when the flying vehicle finally reaches the photographing point area, setting up a shutter timing time after a predetermined time from the moment when the flying vehicle has finally reached the photographing point area, and taking aerial photographs by the two or more flying vehicles at the shutter timing time.

    Abstract translation: 通过使用两个或更多个飞行器，每个配备有GPS装置和图像拾取单元来提供空中摄影测量。 该方法包括以每个拍摄点为中心分别设置两个或更多个拍摄点和设置拍摄点区域，通过GPS装置测量飞行器的位置，其中每个飞行器 到达每个对应的拍摄点区域并保持拍摄点区域的位置，获取飞行时间最终到达拍摄点区域的时间，在从飞行器最终到达之后的预定时间之后设置快门定时时间 拍摄点区域，并且在快门定时时间由两个或更多个飞行车辆拍摄空中照片。

    Sustained over-the-horizon vertical takeoff and landing sensing system
    260.
    发明授权
    Sustained over-the-horizon vertical takeoff and landing sensing system 有权
    持续的超视距垂直起飞和着陆感测系统

    公开(公告)号：US08948928B2

    公开(公告)日：2015-02-03

    申请号：US13866489

    申请日：2013-04-19

    Applicant: Sikorsky Aircraft Corporation

    Inventor： Mark R. Alber ,  Timothy Fred Lauder ,  Jonathan Hartman ,  Bryan Clark Holasek

    IPC: B64C39/00 ,  B64C27/00 ,  B64C19/00 ,  B64C29/00 ,  B64C39/02 ,  B64D47/00

    CPC classification number: B64C19/00 ,  B64C29/00 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/06 ,  B64C2201/123 ,  B64C2201/148 ,  B64D47/00

    Abstract: An electrically powered of the vertical takeoff and landing aircraft configured for use with a tether station having a continuous power source is provided including at least one rotor system. The vertical takeoff and landing aircraft additionally has an autonomous flight control system coupled to the continuous power source. The autonomous flight control system is configured to operate an electrical motor coupled to the at least one rotor system such that the vertical takeoff and landing aircraft continuously hovers above the tether station in a relative position. The vertical takeoff and landing aircraft also includes a detection system for detecting objects at a distance from the vertical takeoff and landing aircraft.

    Abstract translation: 提供了一种配置成与具有连续动力源的系绳站一起使用的垂直起飞和着陆飞机的电力供应器，其包括至少一个转子系统。 垂直起飞和着陆飞机还具有耦合到连续电源的自主飞行控制系统。 自主飞行控制系统被配置为操作耦合到至少一个转子系统的电动机，使得垂直起飞和着陆飞机在相对位置连续地悬挂在系绳站上方。 垂直起降飞机还包括一个检测系统，用于检测与垂直起飞和着陆飞机相距一定距离处的物体。

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