公开(公告)号：EP2914490B1

公开(公告)日：2017-05-24

申请号：EP13811348.5

申请日：2013-10-22

申请人： AIRBUS DEFENCE AND SPACE GMBH

发明人： STEINWANDEL, Jürgen ,  STAGLIANO, Florian ,  VAN TOOR, Jan

IPC分类号： B64C39/02 ,  B64D27/02 ,  B64D27/24 ,  B64D31/00 ,  B64D41/00 ,  F02D29/02

CPC分类号： 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

公开(公告)号：EP3161502A1

公开(公告)日：2017-05-03

申请号：EP14900504.3

申请日：2014-08-29

申请人： SZ DJI Technology Co., Ltd.

发明人： XU, Xingwang ,  CAO, Zisheng ,  QIU, Hualiang ,  WANG, Mingyu ,  TANG, Xiaozheng

IPC分类号： G01S3/808 ,  G08G5/00

CPC分类号： B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2220/00 ,  G10L21/0208 ,  G10L2021/02165 ,  H04R1/1083 ,  H04R3/005 ,  H04R2410/05 ,  H04R2410/07 ,  H04R2430/20 ,  H04R2460/01

摘要： A UAV is provided to cancel background noise from audio data collected by the UAV. The UAV is provided with one or more background microphones in a proximity of one or more background noise-producing components. The UAV is also provided with one or more audio source collecting microphones. The audio data collected by the background microphones may be used to reduce or cancel interfering background noise from the audio signal detected by the audio source collecting microphone. The target audio may be captured or recorded with little or no background noise.

摘要翻译： 提供UAV以从UAV收集的音频数据中消除背景噪声。 无人机在一个或多个背景噪声产生部件附近提供一个或多个背景麦克风。 无人机还提供一个或多个音频源收集麦克风。 由背景麦克风收集的音频数据可以用于从由音频源收集麦克风检测的音频信号中减少或消除干扰背景噪声。 可以捕获或记录目标音频很少或没有背景噪声。

公开(公告)号：EP3147210A2

公开(公告)日：2017-03-29

申请号：EP16190742.3

申请日：2016-09-27

申请人： Ewatt Technology Co., Ltd.

发明人： ZHAO, Guocheng ,  LUO, Wei ,  QI, Pengcheng

IPC分类号： B64C27/04 ,  B64C27/82 ,  B64C39/02 ,  B64D33/02 ,  B64D33/04 ,  B64D33/08

CPC分类号： B64D33/02 ,  B64C27/82 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/044 ,  B64C2201/141 ,  B64C2201/146 ,  B64D27/08 ,  B64D33/06 ,  B64D33/08 ,  B64D2033/0246 ,  B64D2033/028

摘要： The present invention discloses an unmanned helicopter, and belongs to the technical field of unmanned aerial vehicles. The unmanned helicopter includes an air inlet system, an exhaust system, a cooling system and a dynamic balance system. The air inlet system is fixed on a second side; the exhaust system is fixed on a third side; and the cooling system is fixed on a first side, and the dynamic balance system is fixed on a tail. The airflow at the outside of the unmanned helicopter flows into the air inlet system smoothly, quickly and efficiently under the action of its own flow velocity relative to the unmanned helicopter, therefore the technical problem in the prior art that the air entering the fuselage with a unit volume is burnt insufficiently, which generates adverse effects on the normal flight of the unmanned helicopter, is solved.

摘要翻译： 本发明公开了一种无人直升机，属于无人驾驶飞行器技术领域。 无人直升机包括进气系统，排气系统，冷却系统和动平衡系统。 进气系统固定在第二侧; 排气系统固定在第三侧; 冷却系统固定在第一侧，动平衡系统固定在尾部。 无人直升机外部的气流在相对于无人驾驶直升机的自身流速的作用下，平稳，快速而有效地流入，因此现有技术中的技术问题是空气进入机身的空气 单位体积燃烧不足，对无人直升机的正常飞行产生不利影响，得到解决。

公开(公告)号：EP3145811A1

公开(公告)日：2017-03-29

申请号：EP15795669.9

申请日：2015-05-22

申请人： Lily Robotics, Inc.

发明人： BRADLOW, Henry W. ,  BALARESQUE, Antoine ,  ENGLIN, Robert N.

IPC分类号： B64C19/00 ,  B64C27/00 ,  B64C39/02 ,  G05D1/00

CPC分类号： G05D1/0661 ,  B64C19/00 ,  B64C27/00 ,  B64C27/08 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/08 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/146 ,  G05D1/0022 ,  G05D1/0094 ,  G05D1/0669 ,  G05D1/102

摘要： An unmanned aerial vehicle (UAV) copter for consumer photography or videography can be launched by a user throwing the UAV copter into mid-air. The UAV copter can detect that the UAV copter has been thrown upward while propeller drivers of the UAV copter are inert. In response to detecting that the UAV copter has been thrown upward, the UAV copter can compute power adjustments for propeller drivers of the UAV copter to have the UAV copter reach a predetermined elevation above an operator device. The UAV copter can then supply power to the propeller drivers in accordance with the computed power adjustments.

摘要翻译： 无人驾驶飞机（UAV）用于消费者摄影或录像的直升机可以由用户将无人机直升机投入空中。 无人机直升机可以检测到无人机直升机的螺旋桨驱动器是惰性的，无人机直升机已经向上抛出。 无人机直升机响应于检测到无人机直升机已经向上飞行，可以计算无人机直升机螺旋桨驱动器的功率调整，使无人机直升机达到操作员设备上方的预定高度。 无人机直升机然后可以根据计算的功率调整向螺旋桨驱动器供电。

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

申请人： Korea Aerospace Research Institute

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

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

CPC分类号： 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

摘要： 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.

摘要翻译： 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：EP3080673A4

公开(公告)日：2017-01-04

申请号：EP14906298

申请日：2014-11-20

申请人： SZ DJI TECHNOLOGY CO LTD

发明人： XIAO WENLONG ,  WAN XIAOJIAN

IPC分类号： G05D1/10 ,  B64C39/02

CPC分类号： B64D31/06 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/146

摘要： Systems, methods, and devices for assigning addresses to a plurality of functional modules carried by a movable object are provided. In one aspect, a method can comprise: (a) transmitting an activation signal from a control module to a functional module of the plurality of functional modules via a first communication interface, thereby activating the functional module for addressing, wherein the plurality of functional modules are each configured to control a component of the movable object; (b) transmitting an addressing signal comprising an address from the control module to each functional module of the plurality of functional modules via a second communication interface different from the first communication interface, thereby causing the address to be assigned to the activated functional module of step (a); and (c) repeating steps (a) and (b) for each functional module, thereby assigning an address to each functional module.

公开(公告)号：EP3048789B1

公开(公告)日：2016-12-28

申请号：EP16152385.7

申请日：2016-01-22

申请人： Parrot Drones

发明人： ELINE, Pierre

IPC分类号： H04N5/232 ,  H04N5/347 ,  H04N5/345 ,  A63H27/00 ,  A63H30/04 ,  B64C39/02

CPC分类号： H04N5/23287 ,  A63H27/12 ,  A63H30/04 ,  B64C27/08 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/024 ,  B64C2201/108 ,  B64C2201/127 ,  B64D47/08 ,  H04N5/2257 ,  H04N5/23238 ,  H04N5/23258 ,  H04N5/2327 ,  H04N5/23274 ,  H04N5/3454 ,  H04N5/347

公开(公告)号：EP3077669A1

公开(公告)日：2016-10-12

申请号：EP14815266.3

申请日：2014-12-01

申请人： HGZ Patentvermarktungs GmbH

发明人： ZELL, Horst

IPC分类号： F03D13/00

CPC分类号： F03D17/00 ,  B64C27/04 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/123 ,  B64D47/08 ,  F05B2240/2211 ,  F05B2260/83 ,  G01J5/047

摘要： The invention relates to a method for optically detecting a wind turbine (1) for testing purposes using an aircraft, in particular a manned or unmanned rotorcraft (9) equipped with at least one camera. The wind turbine comprises multiple rotor blades (2), the surface of which is scanned as part of the method, said scan being carried out optically. The method has the following method steps: aligning a first rotor blade (2
1 ) in a vertical position, then departing and scanning a first face (5) of the first rotor blade (2
1 ) in the vertical direction, then departing and scanning a second face (6) of the first rotor blade (2
1 ) in the vertical direction, then aligning a second rotor blade (2
2 ) in a vertical position, then departing and scanning a first face (5) of the second rotor blade (2
2 ) in the vertical direction, and then departing and scanning a second face (6) of the second rotor blade (2
2 ) in the vertical direction.

摘要翻译： 一种用于光学地获取的风力涡轮机用于监控目的与飞机的辅助方法，特别是有人或无人旋翼飞机，其具有至少一个相机安装在其上，worin风力涡轮机包括转子叶片的复数，其表面 是该方法的范围内进行扫描。

公开(公告)号：EP2960155A3

公开(公告)日：2016-05-04

申请号：EP15170625.6

申请日：2015-06-04

申请人： Thomson Licensing

发明人： FLEUREAU, Julien ,  TARIOLLE, Francois-Louis ,  KERBIRIOU, Paul ,  LE CLERC, Francois

IPC分类号： B64C27/08 ,  G05D1/00 ,  G05D1/08 ,  G05D1/10

CPC分类号： G05D1/101 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/141 ,  G05D1/0088 ,  G05D1/102

摘要： A method for controlling a path of a rotary-wing drone (1), characterized in that said method comprises:
• Establishing a first-order temporal relation between flight control parameters and flight dynamics for said rotary-wing drone (1) comprising:
∘ An Explicit Discrete Time-Variant State-Space Representation of a translation control of said rotary-wing drone (1);
∘ An Explicit Discrete Time-Variant State-Space Representation of a course control of said rotary-wing drone (1);

• Controlling the path of said rotary-wing drone (1) by:
∘ Estimating a course (17) of said rotary-wing drone (1) on the basis of said Explicit Discrete Time-Variant State-Space Representation of a course control of said rotary-wing drone (1);
∘ Estimating a position (18) of said rotary-wing drone (1) on the basis of said Explicit Discrete Time-Variant State-Space Representation of a translation control of said rotary-wing drone (1);

said steps of estimating (17; 18) being performed independently.

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

申请人： Korea Aerospace Research Institute

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

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

CPC分类号： 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

摘要： 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.

摘要翻译： 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。