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公开(公告)号：US20160363938A1
公开(公告)日：2016-12-15
申请号：US14737814
申请日：2015-06-12
Applicant: SUNLIGHT PHOTONICS INC.
Inventor： SERGEY V. FROLOV , JOHN PETER MOUSSOURIS , MICHAEL CYRUS
CPC classification number: G05D1/104 , B64C3/56 , B64C29/0016 , B64C37/02 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/066 , B64C2201/088 , B64C2201/102 , B64C2201/128 , B64C2201/143 , B64C2201/145 , B64D1/02 , G05D1/0022 , G05D1/0027 , G05D1/005 , G05D1/0212 , G05D1/0669 , G05D1/102 , G08G5/0008 , G08G5/0013 , G08G5/0017 , G08G5/0021 , G08G5/003 , G08G5/0065 , G08G5/0069 , G08G5/025 , G08G5/045 , G08G7/02 , Y02T50/14
Abstract: Embodiments of the present invention provide an alternative distributed airborne transportation system. In some embodiments, a method for distributed airborne transportation includes: providing an airborne vehicle with a wing and a wing span, having capacity to carry one or more of passengers or cargo; landing of the airborne vehicle near one or more of passengers or cargo and loading at least one of passengers or cargo; taking-off and determining a flight direction for the airborne vehicle; locating at least one other airborne vehicle, which has substantially the same flight direction; and joining at least one other airborne vehicle in flight formation and forming a fleet, in which airborne vehicles fly with the same speed and direction and in which adjacent airborne vehicles are separated by distance of less than 100 wing spans.
Abstract translation: 本发明的实施例提供了一种替代的分布式机载运输系统。 在一些实施例中，一种用于分布式机载运输的方法包括：向机载车辆提供机翼和机翼跨度，具有携带乘客或货物中的一个或多个的能力; 机载车辆靠近一个或多个乘客或货物并装载至少一个乘客或货物; 起飞和确定机载飞行方向; 至少定位一个具有大致相同的飞行方向的其他机载车辆; 并将至少一架其他机载车辆接入飞行形成并形成一个舰队，其中机载车辆以相同的速度和方向飞行，并且相邻的机载车辆以小于100个翼跨的距离分开。
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公开(公告)号：US09481457B2
公开(公告)日：2016-11-01
申请号：US14243540
申请日：2014-04-02
Applicant: Sikorsky Aircraft Corporation
Inventor： Mark R. Alber
CPC classification number: B64C39/024 , B64C29/02 , B64C2201/021 , B64C2201/088 , B64C2201/102
Abstract: A vertical take-off and landing (VTOL) aircraft is provided and includes a fuselage, inboard wings extending from opposite sides of the fuselage to define a support plane and engine nacelles disposed along the wings. Each of the wings includes ground alighting elements and a variable geometry such that a portion of the ground alighting elements are alignable with the support plane during in-flight conditions and displaceable from the support plane.
Abstract translation: 提供垂直起飞和降落（VTOL）飞机，并包括机身，内侧翅膀从机身的相对侧延伸，以限定沿机翼设置的支撑平面和发动机舱。 每个翼包括地面下落元件和可变几何形状，使得地面下落元件的一部分在飞行状态期间与支撑平面对准并且可从支撑平面移位。
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公开(公告)号：US20160293015A1
公开(公告)日：2016-10-06
申请号：US14106733
申请日：2013-12-14
Applicant: Oleksiy Bragin
Inventor： Oleksiy Bragin
CPC classification number: G05D1/12 , B64C39/024 , B64C2201/08 , B64C2201/102 , B64C2201/108 , B64C2201/12 , B64C2201/127 , B64C2201/141
Abstract: A method, system and computer readable medium for projectile launched UAV reconnaissance/surveillance are described. The method can include determining a designated target. The method can also include estimating a distance and trajectory from a launch point to the target and communicating distance and trajectory information to a launcher, a projectile and a communication and control system. The method can also include firing a separation charge when the UAV projectile reaches a predetermined point along the flight path, the separation charge being configured to separate a UAV from a projectile casing. The method can further include deploying the UAV and activating a propulsion system of the UAV and obtaining signals via one or more sensors.
Abstract translation: 描述了用于射弹发射的UAV侦察/监视的方法，系统和计算机可读介质。 该方法可以包括确定指定的目标。 该方法还可以包括估计从发射点到目标的距离和轨迹，以及向发射器，射弹和通信和控制系统传送距离和轨迹信息。 该方法还可以包括在UAV弹丸到达沿着飞行路径的预定点时点燃分离费用，分离费用被配置为将UAV与射弹套管分开。 该方法还可以包括部署UAV并激活UAV的推进系统并通过一个或多个传感器获得信号。
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公开(公告)号：US09446845B2
公开(公告)日：2016-09-20
申请号：US14528024
申请日：2014-10-30
Inventor： Stefano Mintchev , Ludovic Daler , Dario Floreano
CPC classification number: B64C39/024 , A63H27/12 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/102 , B64C2201/108 , B64C2201/127
Abstract: An aerial vehicle including self-autonomous deployable arms and methods of deploying the vehicle are disclosed. The arms may include patterns located thereon that allow the arms to transition between wrapped, flat, and deployed configurations autonomously without the need for direct intervention by a user.
Abstract translation: 公开了一种包括自主部署臂的飞行器和部署车辆的方法。 臂可以包括位于其上的图案，其允许臂在包裹的，平坦的和部署的配置之间自主地转换，而不需要用户的直接干预。
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公开(公告)号：US20160176502A1
公开(公告)日：2016-06-23
申请号：US14660184
申请日：2015-03-17
Applicant: Blue Bear Systems Research Limited
Inventor： Michael SNOOK
CPC classification number: B64C3/546 , B64C3/40 , B64C3/54 , B64C39/024 , B64C2003/543 , B64C2201/102 , Y02T50/14
Abstract: Embodiments of the present invention relate to an adaptable wing having a variable geometry for influencing aerodynamic performance, the wing comprising a jointed leading edge having a main pivot, and a wrist joint, with a wing arm therebetween, 5 and a distal wing hand depending from the wrist joint; the wing being reciprocally actuable, via the main pivot and wrist joint, between a first state having an extended wing planform and a second state having a tucked wing planform.
Abstract translation: 本发明的实施例涉及一种具有可变几何形状以用于影响空气动力学性能的适应翼，所述机翼包括具有主枢轴的接合前缘和在其间具有翼臂的腕关节5，以及远侧翼手从 腕关节; 所述机翼通过主枢轴和腕关节在具有延伸机翼平面图的第一状态和具有卷起的机翼平面图的第二状态之间可往复地起动。
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Patent Agency Ranking
136.发明授权公开(公告)号：US09371130B1
公开(公告)日：2016-06-21
申请号：US14686052
申请日：2015-04-14
Applicant: CAWTU, LLC
Inventor： James Emmett Dee Barbieri
CPC classification number: B64C3/54 , B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/102 , B64C2201/203 , Y02T50/14
Abstract: A collapsible wing, methods of producing the collapsible wing, and an unmanned aircraft system that includes the collapsible wing are provided.
Abstract translation: 提供了可折叠机翼，生产可折叠机翼的方法以及包括可折叠机翼的无人飞行器系统。
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公开(公告)号：US09341457B2
公开(公告)日：2016-05-17
申请号：US14851453
申请日：2015-09-11
Applicant: Aurora Flight Sciences Corporation
Inventor： Robert Parks , Adam Woodworth , Tom Vaneck , Justin McClellan
CPC classification number: B64C37/00 , B60F5/02 , B63G8/001 , B63G8/08 , B63G2008/005 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/08 , B64C2201/102 , B64C2201/127 , B64C2201/165 , B64C2201/167 , F42B15/20
Abstract: A combined submersible vessel and unmanned aerial vehicle preferably includes a body structure, at least one wing structure, at least one vertical stabilizer structure, and at least one horizontal stabilizer structure. A propulsion system is coupled to the body structure and is configured to propel the flying submarine in both airborne flight and underwater operation. Preferably, the propulsion system includes a motor, a gearbox coupled to the motor and configured to receive power generated by the motor and provide variable output power, a drive shaft coupled to the gearbox and configured to transfer the variable output power provided by the gearbox, and a propeller coupled to the drive shaft and configured to accept power transferred to it from the drive shaft. The propeller is further configured to rotate and propel the flying submarine in both an airborne environment and in an underwater environment.
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公开(公告)号：US20160068251A1
公开(公告)日：2016-03-10
申请号：US14942174
申请日：2015-11-16
Applicant: TUFTS UNIVERSITY
Inventor： Alfram V. Bright , Richard Wlezien
CPC classification number: B64C3/30 , B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/102 , B64C2201/127 , D06M10/001 , D06M10/10 , D06M15/327 , E04H12/00 , F03D13/20 , H05G2/00 , Y02E10/728
Abstract: The present invention provides novel inflatable and rigidizable support elements, and methods of manufacture and use thereof. In particular, the present invention provides inflatable and rigidizable support elements which find use in rapidly deploying and supporting the wing of an aerial vehicle.
Abstract translation: 本发明提供了新颖的可膨胀和可固化的支撑元件，及其制造和使用方法。 特别地，本发明提供了充气和可固化的支撑元件，其可用于快速展开和支撑飞行器的机翼。
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公开(公告)号：US20160023725A1
公开(公告)日：2016-01-28
申请号：US14775489
申请日：2014-03-05
Applicant: LIQUID ROBOTICS, INC.
Inventor： Roger G. Hine , Derek L. Hine
CPC classification number: B63B35/50 , B63B35/00 , B63H19/02 , B64C19/00 , B64C39/024 , B64C2201/021 , B64C2201/08 , B64C2201/084 , B64C2201/102 , B64C2201/141 , B64C2201/201 , B64C2201/205 , B64F1/04 , B64F1/221 , Y02T70/59
Abstract: Equipment and methods that combine the use of wave powered vehicles and unmanned aerial vehicles (UAVs or drones). A UAV can be launched from a wave-powered vehicle, observe another vessel, and report the results of its observation to the wave-powered vehicle, and the wave-powered vehicle can report the results of the observation to a remote location. The UAV can land on water and can then be recovered by the wave-powered vehicle.
Abstract translation: 结合使用波动车辆和无人机（无人机或无人机）的设备和方法。 无人机可以从波浪式车辆发射，观察另一艘船，并将其观测结果报告给波动车辆，波浪式车辆可以将观测结果报告给偏远地区。 无人机可以登陆水面，然后可以由波浪式车辆回收。
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公开(公告)号：US09216813B2
公开(公告)日：2015-12-22
申请号：US13516453
申请日：2010-12-17
Applicant: Alfram V. Bright , Richard Wlezien
Inventor： Alfram V. Bright , Richard Wlezien
CPC classification number: B64C3/30 , B64C3/56 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/102 , B64C2201/127 , D06M10/001 , D06M10/10 , D06M15/327 , E04H12/00 , F03D13/20 , H05G2/00 , Y02E10/728
Abstract: The present invention provides novel inflatable and rigidizable support elements, and methods of manufacture and use thereof. In particular, the present invention provides inflatable and rigidizable support elements rapidly inflated and rigidized using an acrylic adhesive and UV light generated by combustion, which find use, for example, in rapidly deploying and supporting the wing of an aerial vehicle and wind turbine towers.
Abstract translation: 本发明提供了新颖的可膨胀和可固化的支撑元件，及其制造和使用方法。 特别地，本发明提供了使用丙烯酸粘合剂和由燃烧产生的UV光快速膨胀和刚性化的可膨胀和可固化的支撑元件，其可用于例如快速部署和支撑飞行器和风力涡轮机塔架的机翼。
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