公开(公告)号：EP3405846A1

公开(公告)日：2018-11-28

申请号：EP17741886.0

申请日：2017-01-19

申请人： Alarm.com Incorporated

发明人： REZVANI, Babak

IPC分类号： G05D1/04 ,  G06Q30/06 ,  G08B13/00 ,  G08B25/00 ,  G08B29/00

CPC分类号： G05D1/02 ,  B64C39/024 ,  B64C2201/021 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/127 ,  G05D1/0022 ,  G06Q10/00 ,  G08B13/196 ,  G08B13/1965 ,  G08B15/00 ,  G08B15/02 ,  G08B25/008 ,  G08B25/14

摘要： In one general aspect, a drone control device includes a body, a motor that is configured to move the body, a network module, an input module, and a processor. The network module is configured to communicate with a security system that monitors a property and receive data associated with a location within the property. The input module is configured to receive user input. The processor is configured to perform operations that include: determine, from among the location within the property and other locations within the property, a target location within the property; move the body to the target location within the property by providing a signal to the motor; receive, from the input module, input data that is associated with an operation of the security system; and in response to receiving the input data, perform the operation of the security system.

公开(公告)号：EP3395674A1

公开(公告)日：2018-10-31

申请号：EP16877225.9

申请日：2016-06-17

申请人： Powervision Robot Inc.

发明人： ZHENG, Weifeng ,  HAN, Hui ,  ZHENG, Yi ,  WEI, Buwei ,  ZHENG, Guozhi

IPC分类号： B64C1/30 ,  B64C25/10

CPC分类号： B64C1/30 ,  B64C25/10 ,  B64C25/26 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/20 ,  B64D47/08 ,  H04N7/185

摘要： The invention relates to an aircraft (e.g. Unmanned Aerial Vehicle) and a main body thereof and an outer shell for the main body. The outer shell has: an inner cavity, the inner cavity having a space for at least accommodating main body components of the aircraft; and an outer surface, the outer surface enclosing the inner cavity and being bounded by a closed envelope surface. The main body includes the outer shell and the main body components accommodated in the inner cavity of the outer shell. The aircraft includes the main body, and a mechanical arm and/or a leg.

公开(公告)号：EP3394846A1

公开(公告)日：2018-10-31

申请号：EP15911026.1

申请日：2015-12-21

申请人： SZ DJI Technology Co., Ltd.

发明人： ZHANG, Guofang ,  XU, Xinan

IPC分类号： G08G5/00 ,  G05D1/00 ,  G01C21/00

CPC分类号： G08G5/006 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/141 ,  G05D1/101 ,  G05D1/102 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0039 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0086

摘要： A method for controlling an unmanned aerial vehicle includes assessing whether the UAV is within a flight-restriction region and, based on the assessment, generating signals that cause the UAV to take a flight response measure when within the flight-restriction region. The flight-restriction region is generated based on a location of a reference restriction feature and a functional parameter of the reference restriction feature.

公开(公告)号：EP3080673B1

公开(公告)日：2018-10-31

申请号：EP14906298.6

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： B64D31/06 ,  B64C39/02

CPC分类号： B64D31/06 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/146 ,  H04W8/26

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：EP3391163A1

公开(公告)日：2018-10-24

申请号：EP16828716.7

申请日：2016-12-19

申请人： Pfoertzsch, Antony

发明人： PFOERTZSCH, Antony

IPC分类号： G05D1/00

CPC分类号： B64C39/024 ,  B64C39/02 ,  B64C2201/024 ,  B64C2201/127 ,  B64C2201/14 ,  B64D47/08 ,  G05D1/0094 ,  G05D1/101 ,  G05D1/12 ,  G06F3/017 ,  G06K9/00 ,  G06K9/0063

摘要： The invention relates to a device and a method for an unmanned flying object, in particular for a drone. According to the invention, sensor data (21) of at least one imaging sensor (16A - 16D) and at least one distance-detecting sensor (12A - 12D) is received by a sensor interface (18) and supplied to a signal processing unit (20) which is designed to detect at least one specified object and/or differentiate said at least one specified object from other objects and to determine the parameters of the detected or differentiated object by comparing the sensor data (21) with reference data (25). The parameters of the specified object are then output by an output interface (29).

公开(公告)号：EP3385160A1

公开(公告)日：2018-10-10

申请号：EP17205736.6

申请日：2017-12-06

申请人： Bell Helicopter Textron Inc.

发明人： ROBERTSON, Daniel Bryan ,  GRONINGA, Kirk Landon

IPC分类号： B64C27/26

CPC分类号： B64C27/26 ,  B64C9/04 ,  B64C27/28 ,  B64C2027/8245 ,  B64C2201/024 ,  B64D27/10 ,  B64D27/24

摘要： A helicopter (100) has a fuselage (102), a main rotor system (110) connected to the fuselage (102) and configured to rotate in a rotor direction, the main rotor system (110) comprising a retreating rotor blade side and an opposing advancing rotor blade side, and a first wing (106) extending from the fuselage (102) on the retreating rotor blade side. The helicopter comprises no tail rotor system and comprises no counterrotating rotor system coaxial with the main rotor system (110).

公开(公告)号：EP3369658A1

公开(公告)日：2018-09-05

申请号：EP17872893.7

申请日：2017-11-30

申请人： Autel Robotics Co., Ltd.

发明人： LUO, Dongdong ,  NI, Feng ,  LV, Hang ,  SU, Wenbing

IPC分类号： B64D27/24

CPC分类号： B64C39/024 ,  B60L11/1861 ,  B60L11/1877 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/141 ,  B64D27/24 ,  Y02T10/7005 ,  Y02T50/62

摘要： The present invention discloses an unmanned aerial vehicle, including: a fuselage (11); a battery accommodation cavity (12), disposed on the fuselage (11); a battery pack, including at least two battery blocks and mounted inside the battery accommodation cavity (12); a battery circuit board (14), electrically connected to the battery blocks in the battery pack; and a functional module (15), electrically connected to the battery circuit board (14), the battery blocks in the battery pack supplying power to the functional module (15) via the battery circuit board (14) at the same time. By using the solution of the present invention, endurance of the unmanned aerial vehicle is increased.

公开(公告)号：EP3353054A1

公开(公告)日：2018-08-01

申请号：EP16777858.8

申请日：2016-09-22

申请人： Amazon Technologies, Inc.

发明人： BECKMAN, Brian C. ,  SKEELS, Matthew Lee

IPC分类号： B64C39/02 ,  B64D27/26

CPC分类号： B64D27/26 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/14 ,  B64C2220/00

摘要： A motor mount assembly is provided for coupling a propeller motor to a body of an unmanned aerial vehicle (UAV). The motor mount assembly includes a floating portion and acts to attenuate frequencies of vibration from the propeller motor during operation, which modifies the corresponding noise that is produced and reduces stresses on the various components. The floating portion is surrounded on all sides by isolation portions (e.g., made of elastomers or other materials) that are held within a casing that attaches to the body of the UAV. In one implementation, the motor mount assembly is modular such that one or more of the isolation portions may be replaced with different isolation portions (e.g., having different attenuation properties), depending on the direction and nature of the vibrations from the propeller motor that are to be attenuated for a particular application.

公开(公告)号：EP3347301A1

公开(公告)日：2018-07-18

申请号：EP16766512.4

申请日：2016-09-08

申请人： KRONES AG

发明人： KIRZINGER, Johannes

IPC分类号： B67C3/00 ,  B64C39/02

CPC分类号： H04N7/185 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/123 ,  B64C2201/126 ,  B64C2201/127 ,  B64C2201/14 ,  B64C2201/146 ,  B67C3/007 ,  B67C2003/227 ,  H04N5/23203 ,  H04N5/77

摘要： The invention relates to a device (1) for handling containers and/or packagings, comprising a first handling unit (2) which handles the containers and/or packagings in a first predetermined manner, and a second handling unit (6) which handles the containers and/or packagings in a second predetermined manner, and comprising a transport unit (8) for transporting the containers and/or packagings, and a monitoring unit for monitoring the device (1). According to the invention, the monitoring unit comprises an unmanned and remote-controlled flying device (20) and a control unit (40) for wirelessly controlling said flying device (20), wherein the flying device (20) comprises an image capturing unit (24), and wherein the device (1) comprises a delimiting unit (30) which delimits a flying region of the flying device (20).

公开(公告)号：EP3330176A1

公开(公告)日：2018-06-06

申请号：EP17203694.9

申请日：2017-11-27

申请人： The Boeing Company

发明人： NEWMAN, Daniel I.

IPC分类号： B64C27/08 ,  B64C1/30 ,  B64C27/50 ,  B64C39/02

CPC分类号： B64C39/024 ,  B64C1/30 ,  B64C27/08 ,  B64C27/50 ,  B64C2201/024 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/128 ,  B64C2201/146 ,  B64C2201/201 ,  B64D9/003

摘要： An aerial vehicle includes one or more rotors and a cargo container. The one or more rotors are configured to propel the aerial vehicle. The cargo container defines a cargo volume and is configured to travel with the aerial vehicle during propulsion by the one or more rotors. The cargo container is further configured to contain, at least, the one or more rotors, when the aerial vehicle is not configured for moving cargo.