公开(公告)号：KR101642721B1

公开(公告)日：2016-08-10

申请号：KR1020117025410

申请日：2010-01-11

Applicant: 나발 그룹

Inventor： 에프리드세인트롬,로난

IPC: B64F1/12 ,  F16B21/16 ,  B64B1/66 ,  B64G1/64

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

Abstract: 항공기용으로서플랫폼의고정격자(grate)와협력할수 있는고정하푼및 그러한하나의하푼을포함하는고정시스템에관한것으로, 고정하푼은실린더수단을지나서연장하는로드를구비하는가동(mobile) 피스톤수단을내장하는실린더수단을구비하는잭(jack) 수단을포함하며, 그자유단부는격자에후크식으로걸리고유지핑거를포함하는하푼헤드를포함하며, 상기유지핑거는제어수단에의해서후퇴위치와작동위치사이에서이동될수 있으며, 상기실린더수단은둘 이상의망원경식실린더부분을포함하고, 상기망원경식실린더부분들은하나의부분이다른부분내부로후퇴되는위치와하나의부분이다른부분으로부터돌출하는작동위치사이에서이동될수 있는구성을마련한다. 이러한항공기용고정하푼및 하푼을포함하는고정시스템을마련하는것에의해, 망원경식잭의이용은동일한접힘거리의경우에하푼의전개거리를 2배가될 수있게하고, 그에따라, 접힌위치에서하푼의길이를상당히감소시킬수 있다.

公开(公告)号：KR1020120009470A

公开(公告)日：2012-02-01

申请号：KR1020117025410

申请日：2010-01-11

Applicant: 나발 그룹

Inventor： 에프리드세인트롬,로난

IPC: B64F1/12 ,  F16B21/16 ,  B64B1/66 ,  B64G1/64

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

Abstract: 항공기용으로서 플랫폼의 고정 격자(grate)와 협력할 수 있는 고정 하푼 및 그러한 하나의 하푼을 포함하는 고정 시스템에 관한 것으로, 고정 하푼은 실린더 수단을 지나서 연장하는 로드를 구비하는 가동(mobile) 피스톤 수단을 내장하는 실린더 수단을 구비하는 잭(jack) 수단을 포함하며, 그 자유 단부는 격자에 후크식으로 걸리고 유지 핑거를 포함하는 하푼 헤드를 포함하며, 상기 유지 핑거는 제어 수단에 의해서 후퇴 위치와 작동 위치 사이에서 이동될 수 있으며, 상기 실린더 수단은 둘 이상의 망원경식 실린더 부분을 포함하고, 상기 망원경식 실린더 부분들은 하나의 부분이 다른 부분 내부로 후퇴되는 위치와 하나의 부분이 다른 부분으로부터 돌출하는 작동 위치 사이에서 이동될 수 있는 구성을 마련한다.
이러한 항공기용 고정 하푼 및 하푼을 포함하는 고정 시스템을 마련하는 것에 의해, 망원경식 잭의 이용은 동일한 접힘 거리의 경우에 하푼의 전개 거리를 2배가 될 수 있게 하고, 그에 따라, 접힌 위치에서 하푼의 길이를 상당히 감소시킬 수 있다.

公开(公告)号：EP3368411A1

公开(公告)日：2018-09-05

申请号：EP16788765.2

申请日：2016-10-28

Applicant: BAE Systems PLC

Inventor： WRIGHT, Julian, David ,  COLOSIMO, Nicholas, Giacomo, Robert ,  WARSOP, Clyde

IPC: B64C29/00 ,  A63H27/00 ,  A63H27/14

CPC classification number: B64C39/024 ,  A63H27/00 ,  B64C29/00 ,  B64C29/0033 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/182 ,  B64C2201/201

Abstract: A rotary-wing air vehicle comprising a main body (12) and at least two rotor devices (16a, 16b) arranged and configured to generate propulsion and thrust, in use, to lift and propel said air vehicle, said rotor devices (16a, 16b) being arranged and configured relative to said main body (12) such that the blades thereof do not cross through a central vertical axis of said main body (12) defining the centre of mass thereof, wherein said main body (12) is provided with an aperture (100) that extends therethrough to define a channel about said central vertical axis.

公开(公告)号：EP3288830A2

公开(公告)日：2018-03-07

申请号：EP16728069.2

申请日：2016-04-29

Applicant: Yearwood, Clebert O'Bryan Ricardo

Inventor： Yearwood, Clebert O'Bryan Ricardo

IPC: B64C39/02 ,  F41H7/00 ,  F41H11/00 ,  G06K9/00 ,  G08B13/196 ,  G08G1/09 ,  H04N7/18 ,  E04H1/12

CPC classification number: H04N7/181 ,  B25J11/002 ,  B60P3/025 ,  B60P3/32 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/08 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/182 ,  B64C2201/201 ,  B64C2201/208 ,  E04H1/1238 ,  E04H2001/1283 ,  F41H7/005 ,  F41H11/00 ,  G06K9/00288 ,  G06K9/00771 ,  G06K9/325 ,  G08B13/19632 ,  H04N7/18

Abstract: There is disclosed a deployable surveillance, security and/or enforcement unit, comprising: a container configured for deployment from a vehicle or by air at a surveillance, security and/or enforcement location; and two or more removable modules having equipment for performing surveillance, security and/or enforcement operations, wherein the container has a housing with at least one opening for receiving the two or more modules into the container. The unit may be comprised as part of a vehicle. The advantage of this arrangement is that it is flexible and can be deployed to meet temporary requirements, changing requirements, and can be easily equipped to meet differing roles. The deployable surveillance, security and/or enforcement unit may comprise removable modules including: a command module; a reconnaissance module; a sampling and diagnostic laboratory module; a decontamination module; and/or a utilities module.

公开(公告)号：EP3268278A1

公开(公告)日：2018-01-17

申请号：EP16762677.9

申请日：2016-03-11

Applicant: Nightingale Intelligent Systems

Inventor： CHEN, Ian ,  BOYER, Hugo ,  HSU, John Ming-Jey ,  GAUGEL, Frank Berthold Alfons ,  BAUK, Davor ,  SCHÖTER, Arnd ,  DAMM, Cyril ,  WU, Jack

IPC: B64C39/02 ,  G01C21/20

CPC classification number: G05D1/0038 ,  B64C39/024 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/182 ,  B64C2201/201 ,  G05D1/0044 ,  G06K9/00637 ,  G06K9/00664 ,  G06K9/00771 ,  G07C5/008 ,  G08C17/02 ,  G08G5/0013 ,  G08G5/0026 ,  G08G5/0052 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0086 ,  G08G5/045 ,  H04L65/4092 ,  H04L67/12 ,  H04L67/125

Abstract: An automated drone security system for surveilling a location includes one or more drones with onboard sensors and an imaging device for measuring surveillance data. The surveillance data may include images, telemetry data, infrared data, or other detectable information of the location. Drones may be capable of executing one or multiple flight operations as well as storing and transmitting the surveillance data to a server assembly operable for coordinating the drone and receiving the surveillance data. A drone dock may be included for drone launching, landing, and/or storing the drones. A user computing device may be in communication with the server assembly and the drone(s), the user computing device being capable of receiving user input and displaying surveillance data from the drone. Flight operations associated with surveilling the location may be automatically and/or manually controlled by the user computing device and/or or the server assembly in connection with the location.

公开(公告)号：EP2981462A4

公开(公告)日：2016-12-07

申请号：EP14814301

申请日：2014-04-01

Applicant: HOOD TECHNOLOGY CORPORATION

Inventor： HOOD TECHNOLOGY CORPORATION

IPC: B64D5/00 ,  B64C39/02 ,  B64D3/00

CPC classification number: B64D1/12 ,  B64C39/024 ,  B64C2201/082 ,  B64C2201/182 ,  B64D3/00 ,  B64D5/00

公开(公告)号：EP3060471A2

公开(公告)日：2016-08-31

申请号：EP14878708.8

申请日：2014-10-21

Applicant: Kespry Inc.

Inventor： STABLER, Benjamin, Stuart ,  HALL-SNYDER, Nathaniel ,  DOERSCH, Paul ,  HAMMOND, Marcus

IPC: B64C39/02 ,  B64D45/04 ,  B64F1/00 ,  B64C25/06 ,  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

Abstract: Provided herein are systems and method for autonomously or semi-autonomously landing an unmanned aerial vehicle (UAV) on a landing pad. The landing pad can include features configured to correct misalignment of the UAV on the landing pad. The landing pad can additionally include one or more markers than can be identified by the UAV to aid the UAV in locating the landing pad and determining the location of the UAV relative to the landing pad.

Abstract translation: 本文提供了用于在着陆垫上自主地或半自主地将无人驾驶飞行器（UAV）着陆的系统和方法。 着陆垫可以包括被配置成校正着陆垫上的UAV的未对准的特征。 着陆垫还可以包括一个或多个无人机识别的标记，以帮助UAV定位着陆垫，并确定无人机相对于着陆垫的位置。

公开(公告)号：EP3045392A1

公开(公告)日：2016-07-20

申请号：EP16150820.5

申请日：2016-01-11

Applicant: NEXTER Systems

Inventor： Bertrand, Ludovic ,  Capitaine, Arnaud

IPC: B64F1/02

CPC classification number: B64F1/02 ,  B64C2201/182

Abstract: L'invention porte sur un dispositif (1) d'aide à l'atterrissage d'un drone (100) sur une plateforme (2), dispositif (1) comportant une paire de mats (3a,3b) parallèles entre eux et articulés en site au niveau de premières extrémités relativement à la plateforme (2), les secondes extrémités des mats étant reliées entre elles par au moins un brin (5a, 5b) de câble (5) destiné à l'accrochage du drone (100), dispositif caractérisé en ce qu'il comporte au moins une paire de palets (9a,9b) portés par le ou les brins (5a, 5b) de câble (5) et pouvant être entraînés par un moyen de déplacement (6) d'une première position où chaque palet (9a,9b) est voisin de la seconde extrémité d'un mat (3a,3b) vers une seconde position où les palets (9a,9b) sont voisins l'un de l'autre et positionnés sensiblement à mi-distance des secondes extrémités des mats (3a,3b).

公开(公告)号：EP3031721A1

公开(公告)日：2016-06-15

申请号：EP15195677.8

申请日：2015-11-20

Applicant: Insitu, Inc.

Inventor： KUNZ, Peter ,  JACKSON, Clifford ,  THOMASIAN, Craig Aram

IPC: B64C39/02

CPC classification number: B64F1/02 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/182

Abstract: Capture devices for unmanned aerial vehicles, including track borne capture lines, and associated systems and methods are disclosed. A representative system includes at least one support having an upright portion and at least one boom portion, a carriage track carried by the at least one boom portion, and a carriage carried by, and movable along, the carriage track. The system can further include a capture line carried by and extending downwardly from the at least one boom portion, or the carriage, or both the at least one boom portion and the carriage.

Abstract translation: 无人机，其中包括轨道捕获承担线条，以及相关的系统和方法捕获设备是游离缺失盘。 代表性的系统包括直立部分和至少一个悬臂部分，由所述至少一个悬臂部分承载的滑架轨道，和由携带的滑架，和可动具有沿至少一个支承，滑架轨道。 该系统可以包括一个捕获此外线通过携带并从所述至少一个悬臂部分向下延伸，或滑架，或至少一个在两个臂部分和滑架。

公开(公告)号：EP2974958A2

公开(公告)日：2016-01-20

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

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: 公开了一种用于容纳和充电无人垂直起降飞机的装置和方法。 用于容纳和装载无人垂直起降架的设备包括立柱110，延伸构件120，盖130，紧固单元140和充电单元150.立柱置于地面上。 扩展成员连接到该帖子。 该盖设置在延伸构件上，并且构造成打开或关闭以容纳和保护无人驾驶垂直起降飞机。 紧固单元设置在盖上，并且被配置为紧固无人垂直起降架飞机。 充电单元设置在紧固单元中，并被配置为对无人驾驶垂直起降飞机充电。