公开(公告)号：JP4791492B2

公开(公告)日：2011-10-12

申请号：JP2007557040

申请日：2006-02-09

Applicant: ハネウェル・インターナショナル・インコーポレーテッド

Inventor： グーセン，エムレイ・アール

IPC: B64C29/00

CPC classification number: B64C39/024 ,  B64C27/20 ,  B64C29/0016 ,  B64C2201/027 ,  B64C2201/088 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/162 ,  B64C2201/165 ,  B64C2201/201

公开(公告)号：JP4499155B2

公开(公告)日：2010-07-07

申请号：JP2007508503

申请日：2005-04-14

Applicant: ジェー. アールトン,デイヴィッド ,  アールトン,ポール,イー.

Inventor： ジェー． アールトン，デイヴィッド ,  アールトン，ポール，イー．

IPC: B64C27/10 ,  H02P5/00 ,  B64C27/22 ,  B64C27/26 ,  B64C27/605 ,  B64C27/80 ,  B64C39/02

CPC classification number: B64C27/10 ,  B64C27/22 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/205

公开(公告)号：JP2010120641A

公开(公告)日：2010-06-03

申请号：JP2010032677

申请日：2010-02-17

Applicant: David J Arlton ,  Paul E Arlton ,  ジェー. アールトン,デイヴィッド ,  アールトン,ポール,イー.

Inventor： ARLTON PAUL E ,  ARLTON DAVID J

IPC: B64C27/10 ,  H02P5/00 ,  B64C27/22 ,  B64C27/26 ,  B64C39/02 ,  F41F7/00 ,  F41G9/00 ,  F42B5/00 ,  F42B12/00 ,  F42B15/00

CPC classification number: B64C27/10 ,  B64C27/22 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/082 ,  B64C2201/102 ,  B64C2201/108 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203 ,  B64C2201/205

Abstract: PROBLEM TO BE SOLVED: To provide an unmanned rotary wing vehicle in an unmanned air transportation vehicle. SOLUTION: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in a directional flight. COPYRIGHT: (C)2010,JPO&INPIT

Abstract translation: 要解决的问题：在无人驾驶的空中交通工具中提供无人驾驶的转翼车辆。 解决方案：旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。 转子系统用于在定向飞行中移动旋翼机。 版权所有（C）2010，JPO＆INPIT

公开(公告)号：JP2008542085A

公开(公告)日：2008-11-27

申请号：JP2008510119

申请日：2006-05-01

Applicant: ロッキード・マーチン・コーポレーション

Inventor： ダブリュー スティール ダニエル

IPC: B64F1/00 ,  B64C39/02

CPC classification number: B64F1/04 ,  B64C2201/08 ,  B64C2201/182 ,  B64C2201/201 ,  B64F1/02

Abstract: 本発明の実施の形態は、小型無人飛行機（ＵＡＶ）の捕捉から発射までの間でこのＵＡＶを制御し管理するためのシステムに関する。 このシステムは、組立られた及び／または部分的に分解された複数のＵＡＶのために環境的保護及び隔離をもたらす格納庫を備える。 このＵＡＶの制御及び管理には、捕捉されたＵＡＶの着陸ホストプラットフォームからの再配置及び格納庫への安全な引渡し、汚染除去、燃料抜取り、格納庫への搬入、任務ペイロードのダウンロード、ＵＡＶの分解、保管、ＵＡＶの取り出し及び再組立、任務のアップロード、ＵＡＶの格納庫からの搬出、燃料供給、エンジン試験、ならびに発射準備を含む。 典型的なシステムは、上述の機能を自律的に実行するための複合ロボット制御器によって制御される２つ以上のロボットを有する。 モジュラー式小型携帯用自律システムがＵＡＶ制御及び管理を行う。

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：EP3201088A4

公开(公告)日：2018-06-13

申请号：EP15847916

申请日：2015-09-24

Applicant: SWIFT ENG INC

Inventor： STREETT ANDREW

IPC: B64C39/02 ,  B64D41/00

CPC classification number: B60L11/182 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/201 ,  B64C2201/205 ,  B64F1/222 ,  G05D1/0011 ,  G05D1/0088 ,  H02J7/35 ,  H05K999/99

Abstract: A transportable ground station for a UAV includes a container in which the UAV may be transported and housed. The container includes a wireless or contact-based recharging station that recharges the UAV's batteries or other power sources after the UAV returns from a mission. The recharging station may be directly or indirectly connected to one or more solar panels that generate energy to power the recharging station. The ground station may be deployed virtually anywhere, from any vehicle (e.g., plane, train, boat, truck, etc.), and may operate over an extended period of time without human intervention.

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：EP3241758A4

公开(公告)日：2018-01-24

申请号：EP15875205

申请日：2015-12-29

Applicant: BEIJING ZERO ZERO INFINITY TECH CO LTD

Inventor： ZHANG TONG ,  WANG MENGQIU ,  WANG ZHAOZHE ,  ZHANG XUYANG ,  ZHANG GUANQUN ,  GONG SHUANG ,  ZHANG YALIN ,  WANG JINGLONG ,  LIU LIXIN

IPC: B64C39/02

CPC classification number: B64C27/006 ,  B64C1/30 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/20 ,  B64C2201/201

Abstract: A fully-protected unmanned aerial vehicle comprises an unmanned aerial vehicle body (1) and a rotor (2) connected to the unmanned aerial vehicle body (1), and further comprises a protection housing (3) connected to the unmanned aerial vehicle body (1). The protection housing (3) is a hollowed-out closed housing and has a hollow cavity (31), and the rotor (2) is installed in the hollow cavity (31). Because the rotor is installed in the hollow cavity of the protection housing, the rotor cannot make contact with a human body, so that the unmanned aerial vehicle can be released or reclaimed by an operator with the hand, and the operation portability and safety of the rotor are improved. The hollowed-out structure provides a forming space of lift for the rotor and normal flight of the unmanned aerial vehicle is ensured. The rotor is installed in the protection housing that is connected to the unmanned aerial vehicle body, so that the overall height of the unmanned aerial vehicle is reduced, and the portability of the unmanned aerial vehicle is further improved.

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：EP3206947A4

公开(公告)日：2017-11-01

申请号：EP15874388

申请日：2015-06-01

Applicant: SZ DJI TECHNOLOGY CO LTD

Inventor： WU XUMIN ,  WU XIAOLONG ,  LEE SUNGKI ,  AO JIYUAN ,  FENG ZHUANG

IPC: B64C1/30 ,  B64C39/02

CPC classification number: B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C27/12 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/201 ,  B64D47/08