公开(公告)号：EP3412579A1

公开(公告)日：2018-12-12

申请号：EP17814290.7

申请日：2017-09-11

申请人： Autel Robotics Co., Ltd.

发明人： NI, Feng

IPC分类号： B64D47/08 ,  B64C27/00 ,  B64C39/02 ,  F16M11/12 ,  G03B15/00

CPC分类号： B64C27/001 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64D47/08 ,  F16M11/123 ,  G03B15/006

摘要： The present invention relates to the field of aircrafts and provides a photographic assembly applied to an aircraft, where the aircraft includes a vehicle body. The photographic assembly includes: a vibration absorption member, a frame provided at the periphery of the vehicle body and connected to the vehicle body through a vibration absorption member, a gimbal connected to the frame and a camera connected to the gimbal. The frame of the photographic assembly in embodiments of the present invention can be mounted on unmanned aerial vehicle bodies of different specifications and the frame is sleeved over the vehicle body, so that the structure of the vehicle body can be designed compactly. The embodiments of the present invention further provide an unmanned aerial vehicle having the photographic assembly.

公开(公告)号：EP3022117B1

公开(公告)日：2018-12-12

申请号：EP14727411.2

申请日：2014-04-30

申请人： Niederberger Engineering AG

发明人： NIEDERBERGER, Anton

IPC分类号： A47L1/02 ,  A63H27/00 ,  B64C27/08 ,  B64C25/16 ,  B64C39/02 ,  E04G23/00

CPC分类号： B64C25/16 ,  A47L1/02 ,  A63H27/12 ,  B64C27/08 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/12 ,  E04G23/002

公开(公告)号：EP3408176A1

公开(公告)日：2018-12-05

申请号：EP17709332.5

申请日：2017-02-27

申请人： Amazon Technologies, Inc.

发明人： CHAMPAGNE, JR., Robert Roy ,  KIMCHI, Gur ,  LEGRAND III, Louis LeRoi ,  ROBERTS, Nicholas Hampel ,  WELSH, Ricky Dean

IPC分类号： B64C39/02

CPC分类号： B64C39/024 ,  B64C39/02 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/165 ,  G05D1/0858

摘要： This disclosure describes an aerial vehicle, such as an unmanned aerial vehicle (“UAV”), which includes a plurality of maneuverability propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll). The aerial vehicle may also include a lifting propulsion mechanism that operates to generate a force sufficient to maintain the aerial vehicle at an altitude.

公开(公告)号：EP3266730A3

公开(公告)日：2018-11-28

申请号：EP17175670.3

申请日：2017-06-13

申请人： Nickel Holding GmbH

发明人： Nickel, Alexander

IPC分类号： B65G1/137 ,  B64C39/02 ,  B65G1/127

CPC分类号： B65G1/1373 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/128 ,  B64C2201/141 ,  B65G1/127 ,  B65G47/52

摘要： Aufbewahrungs- und Transportvorrichtung (10) zum Aufbewahren und Transportieren von Bauteilen (18), umfassend einen Multicopter (11) und mindestens ein Teilemagazin (14) zur Aufnahme von Bauteilen (18), wobei das Teilemagazin (14) einen Boden (40) und Seitenwände (42) aufweist und wobei die Vorrichtung (10) für einen fliegenden Transport der im Teilemagazin (14) aufgenommenen Bauteile (18) eingerichtet ist. Die Kombination aus dem Multicopter (11) und dem Teilemagazin (14) wird als Flugmagazin bezeichnet. Ferner ist vorgesehen, dass das mindestens eine Teilemagazin (14) fest mit dem Multicopter (11) verbunden ist und die Vorrichtung (10) ferner eingerichtet ist, als Aufbewahrungseinrichtung an einer Entnahmestation einer Verarbeitungseinrichtung aufgenommen zu werden, wobei in dem Teilemagazin (14) aufgenommene Bauteile (18) durch die Entnahmestation von oben aus dem Teilemagazin (14) entnehmbar sind.

公开(公告)号：EP3401215A1

公开(公告)日：2018-11-14

申请号：EP18171228.2

申请日：2018-05-08

申请人： Pinnacle Vista, LLC

发明人： TU, Haofeng

IPC分类号： B64C29/00 ,  B64C39/12 ,  B64C27/26 ,  B64C27/82 ,  B64C39/02 ,  G05D1/02 ,  G05D1/04 ,  G05D1/08

CPC分类号： B64C27/26 ,  B64C27/82 ,  B64C29/0025 ,  B64C39/024 ,  B64C39/12 ,  B64C2027/8236 ,  B64C2201/021 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/165 ,  G05D1/0202 ,  G05D1/042 ,  G05D1/0858

摘要： A multi-copter lift body aircraft has a push or pull propeller (26) and a lift body (70) that has a first airfoil shape (71) on a front to rear cross-section and a second airfoil shape (72) on a left to right cross-section. The lift body (70) is made from a top shell and a bottom shell. The lift body (70) has a nose (22) and a tail (25). Multi-copter propellers (60) are attached to the lift body. The multi-copter propellers (60) provide a lift at low speeds and the lift body (70) provides a lift at high speeds. Avionics (68) can be stored in a hollow cavity of the lift body. The avionics (68) may include a control circuit (65), batteries (66), and a radio receiver. The multi-copter has a lift body (70) made from an upper shell (36, 38) and a lower shell (37, 39). The lift body (70) has an optimum attack angle (91) at a cruising speed, and the lift body provides a combined lift mode.

公开(公告)号：EP3400493A1

公开(公告)日：2018-11-14

申请号：EP16829181.3

申请日：2016-12-26

申请人： Microsoft Technology Licensing, LLC

发明人： CHANDRA, Ranveer ,  KAPOOR, Ashish ,  WON, Jongho

IPC分类号： G05D1/02 ,  G05D1/08 ,  B64C39/02

CPC分类号： G05D1/0808 ,  B64C27/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/141 ,  B64C2201/146 ,  G05D1/0011 ,  G05D1/0202 ,  G05D1/0204 ,  G05D1/08 ,  G05D1/0858

摘要： Methods and apparatus for avoiding or exploiting air drag on an aerial vehicle are disclosed. In embodiments, the methods and apparatus may be implemented in a controller and used to increase the energy efficiency of an aerial vehicle. In the embodiments, at least one parameter associated with a force on an aerial vehicle is determined. A yaw setting for the aerial vehicle is then determined that exploits or avoids air drag on the aerial vehicle for energy efficiency. The yaw setting may be referenced to a yaw based on directionality in the shape of the aerial vehicle. In other embodiments, a drag associated with a force on an aerial vehicle is determined. It is then determined if there is a selected component in the drag based on a desired maneuver of the aerial vehicle. A yaw setting is then determined based on whether the selected component is in the drag.

公开(公告)号：EP3124381B1

公开(公告)日：2018-10-24

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 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.

公开(公告)号：EP3379362A1

公开(公告)日：2018-09-26

申请号：EP18160908.2

申请日：2018-03-09

申请人： Samsung Electronics Co., Ltd.

发明人： KIM, Jongho ,  LEE, Yun Woo ,  CHOI, Kyonggon

IPC分类号： G05D1/00

CPC分类号： G05D1/12 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/141 ,  B64D47/08 ,  G05D1/0016 ,  G05D1/0094 ,  G06T7/248 ,  G06T7/70 ,  G06T2207/30241

摘要： An electronic device may include a communication module, a memory storing instructions, and one or more processors coupled to the communication module. The one or more processors may be configured to execute the instructions to receive information related to a movement of an external electronic device from the external electronic device by using the communication module, determine a range of moving the electronic device, at least on the basis of the information related to the movement, determine a location to which the electronic device is moved, at least on the basis of the range, and move the electronic device to the location.

公开(公告)号：EP3375216A1

公开(公告)日：2018-09-19

申请号：EP15795144.3

申请日：2015-11-12

申请人： Sony Mobile Communications Inc.

发明人： LJUNG, Rickard ,  YING, Zhinong ,  TRANG, Linh ,  KARLSSON, Peter C. ,  PERSSON, Magnus

IPC分类号： H04W16/26

CPC分类号： H04W16/18 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/122 ,  H04B7/18504 ,  H04W16/24 ,  H04W16/26 ,  H04W24/02 ,  H04W36/22 ,  H04W36/32 ,  H04W84/005

摘要： Apparatus, systems, and methods are disclosed for determining dynamic positioning of mobile cells. Dynamic positioning provides for navigating a mobile cell, such as an unmanned aerial vehicle or the like, to a location suitable for offloading current network traffic, such that the suitable location maximizes offloading capabilities. The methodology describes takes into account both the current traffic load on the network and the location of the highest system capacity-intensive mobile terminals in determining an initial position for deploying the mobile cell. Additionally, the location of the deployed mobile cell is optimized, over time, based on tracking the direction of movement of the highest capacity-intensive mobile terminals, and, in some embodiments, service quality indicators provided by the mobile terminals and/or contextual information captured by the mobile cell apparatus.

公开(公告)号：EP3374263A1

公开(公告)日：2018-09-19

申请号：EP16864925.9

申请日：2016-11-09

申请人： Matternet, Inc.

发明人： RAPTOPOULOS, Andreas ,  BARUCHIN, Ido ,  HINKLE, Christopher, Winson ,  MA, Derek, X. ,  O'SULLIVAN, James, Standish

IPC分类号： B64D1/12 ,  B64C39/02 ,  B64D1/08 ,  B64D9/00 ,  B64F1/32 ,  G05D1/00

CPC分类号： B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/128 ,  B64C2201/208 ,  G08G5/0069 ,  G08G5/025

摘要： An unmanned aerial vehicle (UAV) for transporting a payload is provided. The UAV comprises a body and one or more propellers rotatably connected to the body. The UAV further comprises a battery mounted to the body. The battery is releasable from the bottom of the UAV. The UAV further comprises a payload container mounted to the body. The payload container is releasable from the bottom of the UAV to a landing platform associated with a UAV station.