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    DRONE
    221.
    发明申请
    DRONE 有权

    公开(公告)号：US20160122012A1

    公开(公告)日：2016-05-05

    申请号：US14805803

    申请日：2015-07-22

    Applicant: LG ELECTRONICS INC.

    Inventor： ZHIMIN CHOO ,  Chulbae LEE

    IPC: B64C27/50 ,  B64D47/08 ,  B64C27/10

    CPC classification number: B64C39/028 ,  A63H27/12 ,  B64C27/50 ,  B64C29/0025 ,  B64C39/02 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127

    Abstract: There is disclosed a drone including a main body comprising a motor, a shaft inserted in the main body vertically, a wing unit rotatable on the shaft by a power generated from the motor, the wing unit comprising a propeller unfolded horizontally and folded vertically, wherein the motor comprises a first motor and a second motor, and the shaft comprises an upper shaft inserted in the main body from a top vertically and a lower shaft inserted in the main body from a bottom vertically, and the wing unit comprises a first wing unit rotated on the upper shaft in a first direction by a power generated from the first motor, and a second wing unit rotated on the lower shaft in a second direction, which is the reverse of the first direction, by a power generated from the second motor.

    Abstract translation: 公开了一种无人机，包括：主体，包括电动机，垂直插入主体的轴;翼单元，其通过由电动机产生的动力在轴上旋转，所述翼单元包括水平地折叠并垂直折叠的螺旋桨，其中 所述电动机包括第一电动机和第二电动机，并且所述轴包括从垂直方向从底部插入主体的顶部垂直插入主体中的上轴，并且所述机翼单元包括第一翼单元 通过从第一马达产生的动力沿第一方向在上轴上旋转，并且第二翼单元通过从第二马达产生的动力沿与第一方向相反的第二方向在下轴上旋转 。

    Multi-rotor frame structure
    223.
    发明申请
    Multi-rotor frame structure 审中-公开
    多转子框架结构

    公开(公告)号：US20160101850A1

    公开(公告)日：2016-04-14

    申请号：US14873217

    申请日：2015-10-02

    Applicant: Che Min LIN

    Inventor： Che Min LIN

    IPC: B64C27/08 ,  B64C39/02 ,  B64C1/06

    CPC classification number: B64C39/024 ,  A63H27/12 ,  B64C2201/027

    Abstract: This invention relates to a multi-rotor aircraft frame structure, which is mainly the use of stainless steel tubes and engineering plastics has the rigidity and toughness, directly to the stainless steel tubes symmetrical inserted nailed in plastic sheet to constitute the main frame structure, and by connecting plurality support blocks and plurality support rods to construct a kind of peripheral support structure to obtain sufficient structural strength, thereby to constructing a light weight and low cost and practicality high-performance multi-rotor aircraft frame.

    Abstract translation: 本发明涉及一种多转子飞机框架结构，其主要是使用不锈钢管和工程塑料具有刚性和韧性，直接对称地插入不对称的管中钉入塑料板构成主框架结构， 通过连接多个支撑块和多个支撑杆来构造一种外围支撑结构，以获得足够的结构强度，从而构造重量轻，成本低，实用性高的多转子飞机框架。

    Airborne fulfillment center utilizing unmanned aerial vehicles for item delivery
    224.
    发明授权
    Airborne fulfillment center utilizing unmanned aerial vehicles for item delivery 有权
    机载实现中心利用无人驾驶飞行器进行货物交付

    公开(公告)号：US09305280B1

    公开(公告)日：2016-04-05

    申请号：US14580046

    申请日：2014-12-22

    Applicant: Amazon Technologies, Inc.

    Inventor： Paul William Berg ,  Scott Isaacs ,  Kelsey Lynn Blodgett

    IPC: G05D1/00 ,  G06Q10/08 ,  B64C29/00 ,  B64C39/02 ,  G05D1/10 ,  B64D5/00

    CPC classification number: G06Q10/083 ,  B64B1/00 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/126 ,  B64C2201/128 ,  B64C2201/14 ,  B64D1/08 ,  B64D5/00 ,  G05D1/104 ,  G06Q30/0265 ,  G08G5/0069

    Abstract: Described is an airborne fulfillment center (“AFC”) and the use of unmanned aerial vehicles (“UAV”) to deliver items from the AFC to users. For example, the AFC may be an airship that remains at a high altitude (e.g., 45,000 feet) and UAVs with ordered items may be deployed from the AFC to deliver ordered items to user designated delivery locations. As the UAVs descend, they can navigate horizontally toward a user specified delivery location using little to no power, other than to stabilize the UAV and/or guide the direction of descent. Shuttles (smaller airships) may be used to replenish the AFC with inventory, UAVs, supplies, fuel, etc. Likewise, the shuttles may be utilized to transport workers to and from the AFC.

    Abstract translation: 描述的是机载实现中心（“AFC”）和使用无人驾驶飞行器（“无人机”）将物品从AFC运送给用户。 例如，AFC可以是保持在高空（例如，45,000英尺）的飞艇，并且可以从AFC部署具有有序物品的UAV以将订购的物品运送到用户指定的运送地点。 随着无人机的下降，除了稳定UAV和/或引导下降方向以外，它们可以使用少量甚至无功率的水平朝向用户指定的传送位置进行导航。 可以使用班车（较小的飞艇）向库存，无人机，供应品，燃料等补充AFC。同样，梭子也可用于运输工人往返于AFC。

    Payload-release device and operation thereof
    225.
    发明授权
    Payload-release device and operation thereof 有权

    公开(公告)号：US09302770B2

    公开(公告)日：2016-04-05

    申请号：US14875362

    申请日：2015-10-05

    Applicant: Google Inc.

    Inventor： James Ryan Burgess ,  Joanna Cohen

    IPC: B64D1/12 ,  B64C39/02 ,  B64D9/00

    CPC classification number: B64D1/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/128 ,  B64D9/00

    Abstract: An unmanned aerial vehicle (UAV) is disclosed that includes a retractable payload delivery system. The payload delivery system can lower a payload to the ground using a delivery device that secures the payload during descent and releases the payload upon reaching the ground. The delivery device can include a channel in which a payload mount attachment for a payload can be inserted. The payload mount attachment can include an aperture for receiving a retaining rod to secure the attachment, and thus the payload, to the delivery device. The retaining rod can assume either an engaged position, in which a portion of the retaining rod engages the payload mount attachment while the payload mount attachment is inserted in the channel, or a disengaged position, in which the retaining rod does not engage the payload mount attachment.

    SYSTEMS AND METHODS FOR UNMANNED AERIAL PAINTING APPLICATIONS
    226.
    发明申请
    SYSTEMS AND METHODS FOR UNMANNED AERIAL PAINTING APPLICATIONS 有权
    用于无人值守绘画应用的系统和方法

    公开(公告)号：US20160082460A1

    公开(公告)日：2016-03-24

    申请号：US14491780

    申请日：2014-09-19

    Applicant: LURYTO, LLC

    Inventor： Ryan McMaster ,  Luke Andrew Busby ,  Todd Iverson

    IPC: B05B13/00 ,  B64C39/02

    CPC classification number: B05B13/005 ,  B05B9/007 ,  B05B9/0403 ,  B05B12/122 ,  B64C2201/027 ,  B64C2201/12 ,  B64C2201/146

    Abstract: Various embodiments of the present disclosure are directed to an Unmanned Aerial System (UAS) for applying a liquid to a surface. According to various embodiments, the UAS includes an Unmanned Aerial Vehicle (UAV) including flight control mechanisms. The UAV is configured to receive first control signals and to adjust an operational configuration of the flight control mechanisms in response to the first control signals. The UAS further includes a delivery assembly coupled to the UAV, where the delivery assembly is configured to receive second control signals and to apply the liquid to the surface located proximately to the UAV in response to the second control signals. The UAS further includes a control unit coupled to the UAV and the delivery assembly, the control unit configured to transmit the first and second control signals to the UAV and the delivery assembly, respectively.

    Abstract translation: 本公开的各种实施例涉及用于将液体施加到表面的无人空中系统（UAS）。 根据各种实施例，UAS包括包括飞行控制机构的无人飞行器（UAV）。 无人机被配置为接收第一控制信号并且响应于第一控制信号来调整飞行控制机构的操作配置。 UAS还包括耦合到UAV的输送组件，其中输送组件被配置为接收第二控制信号并且响应于第二控制信号将液体施加到位于UAV附近的表面。 UAS还包括耦合到UAV和输送组件的控制单元，该控制单元被配置为分别将第一和第二控制信号发送到UAV和输送组件。

    IMPACT PROTECTION APPARATUS
    227.
    发明申请
    IMPACT PROTECTION APPARATUS 有权
    防撞装置

    公开(公告)号：US20160075447A1

    公开(公告)日：2016-03-17

    申请号：US14948220

    申请日：2015-11-20

    Applicant: SZ DJI TECHNOLOGY CO., LTD.

    Inventor： Mingyu Wang

    IPC: B64D45/00 ,  B64C25/54 ,  B64C25/32

    CPC classification number: B64D25/00 ,  B64C25/32 ,  B64C25/54 ,  B64C25/56 ,  B64C39/024 ,  B64C2201/027 ,  B64D45/00 ,  B64D2201/00

    Abstract: An impact protection apparatus is provided, comprising a gas container configured to hold a compressed gas and an inflatable member configured to be inflated by the gas and function as an airbag of a movable object, such as an aerial vehicle. A valve controls flow of gas from the container to the inflatable member in response to a signal from a valve controller. The valve and valve controller are powered by an independent power source than one or more other systems of the movable object. A safety mechanism may also be provided that, unless deactivated, prevents inflation of the inflatable member.

    Abstract translation: 提供了一种冲击保护装置，包括构造成保持压缩气体的气体容器和构造成由气体膨胀并充当诸如飞行器的可移动物体的气囊的充气构件。 响应于来自阀控制器的信号，阀控制气体从容器到可膨胀构件的流动。 阀和阀门控制器由与可移动物体的一个或多个其它系统相独立的电源供电。 还可以提供一种安全机构，除非被去激活，否则防止可膨胀构件的膨胀。

    Compact unmanned rotary aircraft
    229.
    发明授权
    Compact unmanned rotary aircraft 有权
    紧凑型无人驾驶飞机

    公开(公告)号：US09260184B2

    公开(公告)日：2016-02-16

    申请号：US14277370

    申请日：2014-05-14

    Applicant: DRAGANFLY INNOVATIONS INC.

    Inventor： Orville Olm ,  Greg Wood ,  Zenon Dragan

    IPC: B64C27/08 ,  B64C39/02

    CPC classification number: B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/20

    Abstract: A rotary wing aircraft apparatus has arms extending from a body, and a rotor assembly attached to an end of each arm. Each rotor assembly has a rotor blade releasably attached by a lock mechanism. A clockwise rotor blade is releasably attached to a first rotor assembly by engagement in a clockwise lock mechanism, and a counterclockwise rotor blade is releasably attached to a second rotor assembly by engagement in a counterclockwise lock mechanism. The clockwise rotor blade is engageable only with the clockwise lock mechanism and the counterclockwise rotor blade is engageable only with the counterclockwise lock mechanism and cannot be engaged in the clockwise lock mechanism. A leg extends down from each rotor assembly to support the apparatus on the ground.

    Abstract translation: 旋翼飞机设备具有从主体延伸的臂和附接到每个臂的端部的转子组件。 每个转子组件具有通过锁定机构可释放地附接的转子叶片。 顺时针转子叶片通过接合在顺时针锁定机构中而可释放地附接到第一转子组件，并且逆时针转子叶片通过接合在逆时针方向的锁定机构中而可释放地附接到第二转子组件。 顺时针转子叶片只能与顺时针锁定机构啮合，而逆时针转子叶片只能与逆时针锁定机构啮合，不能接合在顺时针锁定机构中。 腿从每个转子组件向下延伸以支撑地面上的装置。

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