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    METHOD OF DRONE DELIVERY USING AIRCRAFT
    122.
    发明申请
    METHOD OF DRONE DELIVERY USING AIRCRAFT 审中-公开
    使用飞机的送货方式

    公开(公告)号：US20170038780A1

    公开(公告)日：2017-02-09

    申请号：US14817356

    申请日：2015-08-04

    Applicant: Gerald N. Fandetti

    Inventor： Gerald N. Fandetti

    IPC: G05D1/10 ,  B64D1/02 ,  B64D5/00 ,  B64C39/02 ,  B64B1/22

    CPC classification number: G05D1/104 ,  B64B1/22 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/128 ,  B64D5/00 ,  G06Q10/083

    Abstract: A drone delivery method is provided. The present invention includes an aircraft having a cargo area. The cargo area may include at least one package and at least one unmanned aerial vehicle (UAV). The aircraft flies to a location. The aircraft then releases the UAV from the cargo area while the aircraft is flying or hovering. The package is secured to the UAV prior to releasing the UAV from the cargo area. The UAV is then directed to a delivery destination. Once the UAV has reached the delivery destination, the package is released for delivery. Once the package has been released, the UAV may be directed back to the cargo area within the aircraft.

    Abstract translation: 提供无人机的传送方式。 本发明包括具有货物区域的飞行器。 货物区域可以包括至少一个包装和至少一个无人机（UAV）。 飞机飞到一个位置。 飞机然后在飞机飞行或悬停时从货物区域释放无人机。 在将UAV从货物区域释放之前，该包装被固定在无人机上。 无人机然后被定向到一个运送目的地。 一旦无人机到达发货目的地，该包将被释放送货。 一旦包装被释放，UAV可以被引导回飞机内的货物区域。

    Line Intersect Vehicle Launch and Recovery
    123.
    发明申请
    Line Intersect Vehicle Launch and Recovery 审中-公开
    线相交车辆启动和恢复

    公开(公告)号：US20160221689A1

    公开(公告)日：2016-08-04

    申请号：US14952949

    申请日：2015-11-26

    Applicant: Christopher Ralph Tridico

    Inventor： Christopher Ralph Tridico

    IPC: B64F1/04 ,  B64D3/00 ,  B64D47/02 ,  B64F1/08

    CPC classification number: B64F1/04 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/182 ,  B64C2201/206 ,  B64D5/00

    Abstract: The present invention is a system which facilitates the launch and recovery of an aircraft or other vehicle by another vehicle or site. This system includes cables, wires or other “lines” that are connected to both the subject vehicle and the launch and recovery platform and facilities to extend, retract and position these lines. When the relative motion of the subject vehicle and launch and recovery platform causes the lines to intersect, the lines are connected to each other by means of a hook, carabiner or similar attachment device resulting in the effective capture of the subject vehicle. One or both of the lines may then be retracted resulting in the recovery of the subject vehicle. Launch is accomplished by extending one or both of the lines and subsequently releasing the attachment device.

    Abstract translation: 本发明是一种便于由其他车辆或场所发射和回收飞机或其他车辆的系统。 该系统包括连接到主车辆和发射和恢复平台的电缆，电线或其他“线路”以及用于延伸，缩回和定位这些线路的设备。 当主体车辆和发射和恢复平台的相对运动导致线路相交时，线路通过钩，卡扣或相似的附接装置彼此连接，从而有效地捕获本车辆。 然后可以将一条或两条线缩回，导致本车辆的恢复。 发射通过延伸一条或两条线并随后释放附着装置来实现。

    Tethercraft
    124.
    发明申请
    Tethercraft 审中-公开

    公开(公告)号：US20160194080A1

    公开(公告)日：2016-07-07

    申请号：US14986562

    申请日：2015-12-31

    Applicant: David Webb

    Inventor： David Webb

    IPC: B64D3/00 ,  B64C39/02 ,  G05D1/00

    CPC classification number: B64D3/00 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/18

    Abstract: A Tethercraft is a type of UAV coupled to a Lead Aerial Vehicle (LAV) forming a single aerial vehicle operated by a single flight crew thereby increasing cargo capacity and vehicle capability. Automated Flight Control Systems (AFCS) in both the Tethercraft and LAV provide the capability to ‘lock’ a Tethercraft in specific positions relative to its LAV for flight operations such as, but not limited to, takeoff, cruising, and landing. The LAV provides all (towing), some (assisted towing), or none (navigation only) of the propulsion for a Tethercraft depending on the embodiment.A Tethercraft might be positioned closer to the LAV during takeoffs and landings and further away from the LAV during cruising in order to maintain optimum efficiency.A tether can be any rigid, non-rigid, electronic, or other means of coupling two aerial vehicles. Some embodiments might use a means to change the length of the tether such as a winch. Other embodiments might use a fixed-length tether or other means of coupling.

    Abstract translation: Tethercraft是一种无人机，与一架引导型空中飞行器（LAV）相结合，形成由单个机组人员操作的单个飞行器，从而提高货物能力和车辆能力。 Tethercraft和LAV中的自动飞行控制系统（AFCS）提供了在相对于其LAV的特定位置“锁定”Tethercraft的能力，用于飞行操作，例如但不限于起飞，巡航和着陆。 根据实施例，LAV为Tethercraft的推进提供所有（牵引），一些（辅助牵引）或无（仅导航）。 在起飞和着陆期间，Tethercraft可能位于LAV附近，并在巡航期间远离LAV，以保持最佳效率。 系绳可以是任何刚性，非刚性，电子或其他联接两架飞行器的手段。 一些实施例可以使用改变诸如绞车的系绳长度的方法。 其他实施例可以使用固定长度的系绳或其他联接装置。

    AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE
    126.
    发明申请
    AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE 有权
    用于空运车辆的空运集装箱

    公开(公告)号：US20150266578A1

    公开(公告)日：2015-09-24

    申请号：US14018493

    申请日：2013-09-05

    Applicant: Raytheon Company

    Inventor： Erick W. Elkins ,  Matthew Glenn Murphy ,  Scott D. Thomas

    IPC: B64D1/12 ,  B64C39/02

    CPC classification number: B64D1/12 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/201 ,  B64C2201/206

    Abstract: A container is used to launch a small aircraft, such as an unmanned aerial vehicle (UAV), from a host aircraft. The container protects the UAV from stresses during the initial ejection from a launcher that is part of the host aircraft. The initial stresses may be due to turbulence in the vicinity of the host aircraft, high airspeed, and/or tumbling that may result from the ejection from the host aircraft moving at a high airspeed. The container may deploy a drag device, such as a drogue chute, to slow the container down and reorient the container, prior to deployment of the UAV from the container. During the time between ejection from the host aircraft and deployment from the container, the UAV may be powered up and acquire data, such as global positioning system (GPS) data, to allow the UAV a “hot start” enabling immediate mission commencement.

    Abstract translation: 一个集装箱用于从一架主机上发射一架小型飞机，如无人飞行器（UAV）。 该容器保护无人机在最初从作为主机的一部分的发射器弹出之前受到压力。 初始应力可能是由于主机飞机附近的湍流，高空速和/或可能由主飞机从高空速下移动而导致的翻滚造成的。 在从容器部署UAV之前，容器可以部署拖动装置，例如锥形滑槽，以使容器向下减速并重新定向容器。 在从主机飞行器和从集装箱部署之间的时间内，UAV可以被加电并且获取诸如全球定位系统（GPS）数据的数据，以允许UAV“启动”，从而能够立即启动任务。

    UNMANNED AERIAL VEHICLE AND METHOD FOR LAUNCHING
    128.
    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 。

    System for carrying and dropping loads for a transport airplane
    129.
    发明授权
    System for carrying and dropping loads for a transport airplane 有权
    用于运输飞机载运的系统

    公开(公告)号：US08979029B2

    公开(公告)日：2015-03-17

    申请号：US13515760

    申请日：2010-12-13

    Applicant: Benoît Jaurand ,  Frédéric Michaud

    Inventor： Benoît Jaurand ,  Frédéric Michaud

    IPC: B64C1/22 ,  B64D1/10 ,  B64D1/12

    CPC classification number: B64D1/10 ,  B64C2201/082 ,  B64C2201/206 ,  B64D1/12

    Abstract: The present disclosure relates to a system for carrying and dropping ammunition for a transport airplane. The system includes a container which contains at least one load, in particular ammunition, which is capable of being brought into a drop position, in which a portion is located outside the airplane, and from which a load can be dropped, usually by simply releasing the load.

    Abstract translation: 本公开涉及一种用于运输和运送飞机弹药的系统。 该系统包括容器，该容器包含至少一个负载，特别是弹药，其能够进入下降位置，其中一部分位于飞机外部，并且可以通过简单地释放负载， 负载。

    Convertible compounded rotorcraft
    130.
    发明授权
    Convertible compounded rotorcraft 有权
    可转换复合旋翼航空器

    公开(公告)号：US08950698B1

    公开(公告)日：2015-02-10

    申请号：US13661567

    申请日：2012-10-26

    Applicant: The Boeing Company

    Inventor： Glenn T. Rossi

    IPC: B64D5/00 ,  B64C37/02 ,  B64C29/02

    CPC classification number: B64C27/26 ,  B64C27/28 ,  B64C29/0033 ,  B64C29/02 ,  B64C37/02 ,  B64C39/003 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/206 ,  B64D5/00

    Abstract: A compound rotorcraft including a rotary wing aircraft having a fuselage and at least one rotor and a fixed-wing aircraft coupled to the rotary wing aircraft, wherein the rotary wing aircraft can fly on the rotor or the fixed-wing aircraft, and wherein the fixed-wing aircraft is detachable from the rotary wing aircraft to fly independently.

    Abstract translation: 一种复合旋翼航空器，其包括具有机身的旋翼飞机和至少一个转子以及耦合到旋转翼飞行器的固定翼飞行器，其中所述旋翼飞机可以在所述转子或所述固定翼飞行器上飞行，并且其中所述固定 飞机可以从旋翼飞机上拆下来独立飞行。

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