公开(公告)号：EP2906469B1

公开(公告)日：2018-05-16

申请号：EP13774432.2

申请日：2013-10-10

Applicant: Institut Supérieur de l'Aéronautique et de l'Espace

Inventor： BERNARD, Dominique

IPC: B64C39/02

CPC classification number: B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/165 ,  B64C2201/182

公开(公告)号：EP3230164A2

公开(公告)日：2017-10-18

申请号：EP15816344.4

申请日：2015-12-09

Applicant: Lockheed Martin Corporation

Inventor： MCKEE, Thomas, Sandlin ,  RODEN, Steve, Conrad

IPC: B64F1/10 ,  B64C39/02

CPC classification number: B64F1/10 ,  B60P3/11 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/14 ,  B64C2201/182 ,  G05D1/021

Abstract: A UAV support vehicle carries a UAV support apparatus for launching and/or recovering a UAV while the UAV support vehicle is moving. The UAV support apparatus releases the UAV during launch and receives the UAV during recovery. An active suspension may be connected between the UAV support vehicle and at least a portion of the UAV support apparatus and reduce motion imparted to that portion of the UAV support apparatus. During UAV recovery, data from a synchronization link between the UAV and the UAV support vehicle may be used to maneuver the UAV and/or the UAV support vehicle.

Abstract translation: 无人飞行器支持车辆携带用于在无人飞行器支持车辆移动时发射和/或恢复无人飞行器的无人飞行器支持装置。 无人机辅助装置在发射期间释放无人机，并在恢复期间接收无人机。 主动悬架可以连接在无人飞行器支援车辆和无人飞行器支援装置的至少一部分之间，并减少传递给无人飞行器支援装置的该部分的动作。 在UAV恢复期间，来自UAV和UAV支持车辆之间的同步链路的数据可用于操纵UAV和/或UAV支持车辆。

公开(公告)号：EP3222530A1

公开(公告)日：2017-09-27

申请号：EP14906490.9

申请日：2014-11-19

Applicant: SZ DJI Technology Co., Ltd.

Inventor： WANG, Mingxi ,  CHEN, Hanping ,  CHEN, Xiangyu ,  LIN, Yuan

IPC: B64F1/02

CPC classification number: B64F1/02 ,  B64C39/024 ,  B64C2201/182

Abstract: Disclosed in the present invention is a positioning mechanism, a UAV dock using the positioning mechanism, and a UAV replenishment method. The positioning mechanism comprises a base provided with a landing area, with a positioning portion provided on said landing area; and a guide member movably arranged on said landing area and comprising a guide surface, wherein the moving states of said guide member relative to said base include a non-operating state and an operating state; the height of said guide member in said non-operating state is less than the height thereof in said operating state; and said guide surface in said operating state can be adjoined by said positioning portion. Compared with a totally active solution, the above-mentioned positioning mechanism reduces the number of actuators for positioning, thus reducing the cost and complexity of equipment and reducing the space occupied by the guide member in the non-operating state, thereby facilitating the miniaturized design of equipment.

Abstract translation: 本发明公开了一种定位机构，使用该定位机构的UAV码头以及无人机补货方法。 定位机构包括设置有着陆区域的基座，在所述着陆区域设置有定位部， 以及可移动地布置在所述着陆区域上并且包括引导表面的引导构件，其中所述引导构件相对于所述基部的移动状态包括非操作状态和操作状态; 在所述非操作状态下，所述引导构件的高度小于在所述操作状态下的高度; 并且在所述操作状态中的所述引导表面可以被所述定位部分邻接。 与完全有效的解决方案相比，上述定位机构减少了定位执行机构的数量，从而降低了设备的成本和复杂性，并减少了非工作状态下导向机构所占用的空间，有利于小型化设计 的设备。

公开(公告)号：EP2870068B1

公开(公告)日：2017-08-30

申请号：EP12880637.9

申请日：2012-07-05

Applicant: UMS Skeldar Sweden AB

Inventor： CARDELL, Per-Erik ,  STENBOM, Kjell

IPC: B64F1/12 ,  B64C25/68 ,  E01F3/00 ,  B64C25/52 ,  B64C25/32

CPC classification number: B64F1/02 ,  B64C25/52 ,  B64C25/68 ,  B64C2025/325 ,  B64C2201/182 ,  B64F1/007 ,  B64F1/125 ,  E01F3/00 ,  Y02T50/82

公开(公告)号：EP3060471A4

公开(公告)日：2017-06-28

申请号：EP14878708

申请日：2014-10-21

Applicant: KESPRY INC

Inventor： STABLER BENJAMIN STUART ,  HALL-SNYDER NATHANIEL ,  DOERSCH PAUL ,  HAMMOND MARCUS

IPC: B64C39/02 ,  B64F1/00 ,  H02J7/00

CPC classification number: B64F1/02 ,  A63H27/00 ,  A63H27/12 ,  B60L11/1816 ,  B60L11/182 ,  B60L11/1838 ,  B60L2200/10 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/141 ,  B64C2201/18 ,  B64C2201/182 ,  B64F1/12 ,  B64F1/20 ,  B64F1/362 ,  G05D1/0676 ,  G05D1/102 ,  Y02T10/7005 ,  Y02T10/7072 ,  Y02T90/122 ,  Y02T90/14

公开(公告)号：EP3124381A1

公开(公告)日：2017-02-01

申请号：EP16190021.2

申请日：2014-12-11

Applicant: Korea Aerospace Research Institute

Inventor： LEE, Sang-Cherl ,  KIM, Hae-Dong ,  GONG, Hyeon-Cheol ,  CHOI, Gi-Hyuk ,  HWANG, In-Hee ,  SUK, Byong-Suk

IPC: B64C39/02 ,  B64F1/12 ,  B64F1/22

CPC classification number: B60L11/1824 ,  B60L2200/10 ,  B60L2230/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201 ,  B64D45/08 ,  B64F1/00 ,  B64F1/005 ,  B64F1/12 ,  B64F1/222 ,  F21S8/086 ,  F21V33/00 ,  F21W2131/103 ,  F21Y2115/10

Abstract: An apparatus for containing and charging an unmanned VTOL aircraft 300, comprising a post 200 placed on a ground and at least one lateral fastening hole 210 formed in a side of the post, and configured such that a pole 340 of the unmanned VTOL aircraft is inserted and fastened into the lateral fastening hole, wherein an entrance of the lateral fastening hole is formed in a cone shape, and thus the pole of the unmanned VTOL aircraft is easily inserted into the lateral fastening hole during fastening of the unmanned VTOL aircraft. The lateral fastening hole is further configured such that target- and cross-shaped LED/IR lights are lit in order to guide the unmanned VTOL aircraft through automatic insertion via vision of the unmanned VTOL aircraft.

Abstract translation: 得到的装置用于容纳和无人驾驶垂直起落飞机300的充电，其包括一个柱200放置在地面和在所述柱的侧面的至少一个侧面的固定210形成，并且配置的搜索做了无人驾驶垂直起落飞机的极340被插入 紧固并进入横向紧固孔，worin在横向紧固孔的入口的圆锥形状是形成，因此无人垂直起落飞机的极无人驾驶垂直起落飞机的紧固过程中容易地插入到所述横向紧固孔。 横向紧固孔被构造进一步调查做靶和交叉形的LED / IR灯，以便经由无人垂直起落飞机的视力通过自动插入引导无人驾驶垂直起落飞机点亮。

公开(公告)号：EP2974958A3

公开(公告)日：2016-04-13

申请号：EP14197368.5

申请日：2014-12-11

Applicant: Korea Aerospace Research Institute

Inventor： Lee, Sang-Cherl ,  Kim, Hae-Dong ,  Gong, Hyeon-Cheol ,  Choi, Gi-Hyuk ,  Hwang, In-Hee ,  Suk, Byong-Suk

IPC: B64C39/02 ,  B64F1/12 ,  B64F1/22

CPC classification number: B60L11/1824 ,  B60L2200/10 ,  B60L2230/10 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201 ,  B64D45/08 ,  B64F1/00 ,  B64F1/005 ,  B64F1/12 ,  B64F1/222 ,  F21S8/086 ,  F21V33/00 ,  F21W2131/103 ,  F21Y2115/10

Abstract: An apparatus and method for containing and charging an unmanned VTOL aircraft are disclosed. The apparatus for containing and charging an unmanned VTOL aircraft includes a post 110, an extended member 120, a cover 130, a fastening unit 140, and a charging unit 150. The post is placed on a ground. The extended member is connected to the post. The cover is provided on the extended member, and is configured to be opened or closed in order to contain and protect the unmanned VTOL aircraft. The fastening unit is provided in the cover, and is configured to fasten the unmanned VTOL aircraft. The charging unit is provided in the fastening unit, and is configured to charge the unmanned VTOL aircraft.

Abstract translation: 用于容纳和无人垂直起落飞机的充电的装置和方法是游离缺失盘。 用于容纳和无人垂直起落飞机的充电的装置，包括：延伸件120上的柱110，一个盖130，紧固单元140和所述柱在地面上放置的充电单元150。 延伸件连接到所述后，提供所述延伸件上的盖，并且被配置以容纳和保护无人垂直起落飞机，以被打开或关闭。 所述紧固单元设置在所述盖中设置，并且被配置来紧固无人驾驶垂直起落飞机。 充电单元设置在所述紧固单元中提供，并且被配置为充电无人垂直起落飞机。

公开(公告)号：EP2414237B1

公开(公告)日：2015-07-15

申请号：EP10706015.4

申请日：2010-01-11

Applicant: DCNS

Inventor： AFFRE DE SAINT ROME, Ronan

IPC: B64F1/16 ,  F16B21/16

CPC classification number: B64F1/16 ,  B64C2201/182 ,  B64F1/125 ,  F16B21/16

公开(公告)号：EP2766260A4

公开(公告)日：2015-07-01

申请号：EP11874051

申请日：2011-10-12

Applicant: SAAB AB

Inventor： DANIELSSON TORKEL

IPC: B64F1/02 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C2201/084 ,  B64C2201/182 ,  B64C2201/201

公开(公告)号：EP2879952A2

公开(公告)日：2015-06-10

申请号：EP13846578.6

申请日：2013-07-31

Applicant: Neurosciences Research Foundation, Inc.

Inventor： HUTSON, Donald B.

IPC: B64C25/36

CPC classification number: B64D47/08 ,  B64C27/006 ,  B64C27/10 ,  B64C27/20 ,  B64C39/024 ,  B64C2025/325 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/108 ,  B64C2201/121 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/182 ,  B64D9/00 ,  F16M11/123 ,  F16M11/18 ,  F16M13/00 ,  F16M13/02 ,  F16M2200/041

Abstract: In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360 about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.