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：EP3124380A1

公开(公告)日：2017-02-01

申请号：EP16181405.8

申请日：2016-07-27

Applicant: Airbus SAS

Inventor： ALONSO TABARES, Diego ,  DELSAUT, Gerard ,  DEMAISON, Sebastien

IPC: B64C39/02

CPC classification number: G08G5/02 ,  B60L11/182 ,  B60L2230/22 ,  B64C39/024 ,  B64C2201/066 ,  B64C2201/14 ,  B64C2201/18 ,  B64D45/04 ,  B64F1/02 ,  B64F1/362 ,  G08G5/0013 ,  G08G5/0091

Abstract: - Station d'accueil de drone et ensemble de gestion d'une telle station d'accueil.
- La station d'accueil (1) comporte une structure (3) apte à être montée sur un support et pourvue d'une plate-forme (4) de réception de drone (2), un système de transmission d'informations (5) de type sans fil, le système de transmission d'informations comportant un premier ensemble de transmission d'informations apte à communiquer avec au moins un centre de contrôle et un second ensemble de transmission d'informations apte à communiquer avec au moins un drone (2), ainsi qu'une unité centrale reliée audit système de transmission d'informations (5).

Abstract translation: 无人机垫包括被配置为安装在基座上并且具有用于无人机和无线数据传输系统的平台的结构。 数据传输系统包括被配置为与至少一个控制中心进行通信的第一数据传输单元和被配置为与至少一个无人机通信的第二数据传输单元以及与数据传输系统链接的中央单元。

公开(公告)号：EP3006334A1

公开(公告)日：2016-04-13

申请号：EP14461575.4

申请日：2014-10-06

Applicant: Patents Factory Ltd. Sp. z o.o.

Inventor： Paczkowski, Jacek ,  Nalewa, Tomasz ,  Kramek, Krzysztof

IPC: B64C39/02 ,  B64C39/10 ,  B64D5/00

CPC classification number: B64D5/00 ,  B64B2201/00 ,  B64C39/024 ,  B64C39/10 ,  B64C2201/028 ,  B64C2201/042 ,  B64C2201/063 ,  B64C2201/066 ,  B64C2201/082 ,  B64C2201/206 ,  B64D27/02 ,  B64D39/00 ,  B64D2211/00

Abstract: A system for connecting an all-wing carrier with a parasite flying unit, characterized in that the carrier (1) and the parasite flying unit (2) are connected via energy distribution means (11 a, 21a, 11b, 21b) configured to exchange energy bi-directionally, wherein the system further comprises a controller (41) configured to control the direction of the flow and the amount of said energy.

Abstract translation: 一种用于连接全翼载体与寄生飞行单元的系统，其特征在于，所述载体（1）和所述寄生虫飞行单元（2）通过经配置以交换的能量分配装置（11a，21a，11b，21b）连接 其中所述系统还包括被配置为控制所述流动方向和所述能量的控制器（41）。

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：EP2996937A1

公开(公告)日：2016-03-23

申请号：EP14732257.2

申请日：2014-05-09

Applicant: Ridengineering

Inventor： JONIOT, Jacques

IPC: B64B1/44 ,  B64C27/20

CPC classification number: B64C27/22 ,  B64B1/40 ,  B64B1/44 ,  B64C17/04 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/123 ,  B64D2211/00

Abstract: The invention relates to a drone comprising: two contra-rotating annular propellers (2, 4) defining a plane therebetween which is referred to as an equatorial plane and is assumed to be horizontal, means for driving the propellers, a load arranged below the equatorial plane, and means (20) for moving the load relative to the equatorial plane, an enclosure referred to as an upper enclosure (6) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially above the equatorial plane, and an enclosure referred to as a lower enclosure (8) filled with a gas or a gaseous mixture having a density of less than 1 and arranged essentially below the equatorial plane, the load being placed inside the lower enclosure (8).

Abstract translation: 无人机技术领域本发明涉及一种无人机，包括：两个反向转动的环形螺旋桨（2,4），在其间限定一个平面，被称为赤道平面，并被假设为水平的，用于驱动螺旋桨的装置，设置在赤道 平面和用于相对于赤道平面移动负载的装置（20），被称为上部外壳（6）的外壳，其填充有密度小于1且基本上位于赤道平面上方的气体或气体混合物 ，以及被称为下部外壳（8）的外壳，其中填充有密度小于1且基本上位于赤道平面下方的气体或气体混合物，负载被放置在下部外壳内。

公开(公告)号：EP2935003A1

公开(公告)日：2015-10-28

申请号：EP13811509.2

申请日：2013-12-19

Applicant: European Aeronautic Defence And Space Company Eads France

Inventor： SMAOUI, Hichem ,  NESPOULOUS, Charles ,  RECHAIN, Bruno ,  JOUBERT, Emmanuel ,  ESTEYNE, Didier

IPC: B64C39/02 ,  B64D27/24 ,  B64D39/00 ,  H01R13/62 ,  H01R24/38

CPC classification number: B64C39/024 ,  B60L11/1818 ,  B60L2200/10 ,  B64C39/02 ,  B64C2201/066 ,  B64D27/24 ,  B64D39/00 ,  H01R13/6205 ,  H01R24/38 ,  H02J7/0014 ,  H02J7/0021 ,  H02J7/0026 ,  H02J7/0045 ,  H02J7/007 ,  Y02T10/7005 ,  Y02T10/7072 ,  Y02T50/44 ,  Y02T50/64 ,  Y02T90/14

Abstract: The subject of the invention is a system for recharging the batteries (6) carried on board an electrically powered aircraft (10), characterized in that it comprises a charging aircraft (1), means (2, 3a, 3b, 4) of temporarily electrically connecting the charging aircraft to the electrically powered aircraft and a charge-regulating device (5) in the electrically powered aircraft.

公开(公告)号：EP2914490A1

公开(公告)日：2015-09-09

申请号：EP13811348.5

申请日：2013-10-22

Applicant: AIRBUS DEFENCE AND SPACE GMBH

Inventor： STEINWANDEL, Jürgen ,  STAGLIANO, Florian ,  VAN TOOR, Jan

IPC: B64C39/02 ,  B64D27/02 ,  B64D27/24

CPC classification number: F02D29/02 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/066 ,  B64C2201/086 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/16 ,  B64D27/02 ,  B64D27/24 ,  B64D31/00 ,  B64D41/00 ,  B64D2027/026 ,  Y02T50/44 ,  Y02T50/64

Abstract: The invention relates to an unmanned aircraft (10), the drive (12) of which comprises an internal combustion engine (28) designed as a diesel and/or kerosene engine and having a charging device (30) for charging the engine. In particular a hybrid drive (32), more especially a parallel hybrid drive, is provided as the drive (12).

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.

公开(公告)号：KR102236965B1

公开(公告)日：2021-04-07

申请号：KR1020200061415A

申请日：2020-05-22

Applicant: 김성

Inventor： 김성

IPC: G06Q50/14 ,  B64D47/08 ,  G06F3/01 ,  G06N3/08

CPC classification number: G06Q50/14 ,  B64C39/024 ,  B64D47/08 ,  G06F3/017 ,  G06N3/08 ,  B64C2201/022 ,  B64C2201/066 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/146 ,  Y02T50/50

Abstract: 본 발명은 드론을 이용한 원격 여행 지원장치에 관한 것으로, 더욱 상세하게는 사용자가 원하는 특정 나라의 여행 코스를 제공하고, 인공지능 딥러닝 기술을 이용하여 바디모션 인터페이스를 통해 드론의 이동을 원격지에서 제어하여 사용자가 드론에 의해 촬영된 주변 여행 풍경을 감상할 수 있도록 하는 드론을 이용한 원격 여행 지원장치에 관한 것이다.
본 발명을 통해, 드론 조작자가 조작하는 것이 아닌, 여행자(사용자)가 바디모션을 이용하여 드론을 원격지에서 조작하기 때문에 여행이 더욱 실감나는 효과를 제공하게 된다.

公开(公告)号：KR102231048B1

公开(公告)日：2021-03-23

申请号：KR1020190101483A

申请日：2019-08-20

Applicant: 주식회사 만물공작소

Inventor： 정봉현

IPC: B64F3/02 ,  B64C39/02 ,  B64D27/24 ,  H02G11/02

CPC classification number: B64F3/02 ,  B64C39/022 ,  B64C39/024 ,  B64D27/24 ,  H02G11/02 ,  B64C2201/042 ,  B64C2201/066 ,  Y02T50/50 ,  Y02T50/60

Abstract: 실시예에 따른 유전 전원공급장치를 이용한 테더 드론 시스템은, 테더 드론과 지상 스테이션에 전원을 공급하는 전원공급부; 상기 테더 드론과 지상 스테이션을 연결하는 케이블을 권취 또는 권출하는 장력제어부; 상기 케이블을 수용하여 제어하는 케이블 가이드; 상기 케이블을 기반으로 상기 테더 드론과 통신하는 지상 통신부; 및 상기 지상 통신부와 상기 전원공급부를 제어하여 상기 케이블을 통해 상기 테더 드론으로 전원을 공급하고, 상기 장력제어부를 제어하여 상기 케이블의 길이를 조절하며, 상기 케이블 가이드를 제어하여 상기 테더 드론의 이동반경을 조절하는 제어부;를 포함하고, 상기 케이블 가이드는, 다단의 샤프트로 구현되어 상기 케이블 가이드의 높이를 조절하는 가이드 샤프트와, 상기 가이드 샤프트와 회전가능하게 연결되어 상기 테더 드론의 이동반경이 조절되도록 상기 케이블을 제어하는 가이드 헤더를 포함한다.