公开(公告)号：EP4353586A1

公开(公告)日：2024-04-17

申请号：EP22819821.4

申请日：2022-02-21

申请人： Sony Group Corporation

发明人： KOSHIMAE, Hidenari

IPC分类号： B64C13/20 ,  B64C27/08 ,  B64C39/02 ,  B64D47/02 ,  B64D47/08 ,  G05D1/02 ,  G06F3/048

CPC分类号： B64C27/08 ,  B64C39/02 ,  B64D47/02 ,  B64D47/08 ,  G06F3/048 ,  B64U10/13 ,  B64U30/20 ,  B64U50/19 ,  B64U2101/3120230101 ,  B64U2201/2020230101

摘要： A movable object according to an embodiment of the present technology includes a body unit, a notification unit, and a notification control unit. The notification unit is provided in the body unit. The notification control unit controls an operation of the notification unit, to thereby notify of information regarding at least one of an orientation of the body unit or a position on the body unit as assistance information for assisting work of a user on the movable object. This enables the user to intuitively recognize which orientation the user should put the body unit in, and the workability in user's work can be improved.

公开(公告)号：EP3858737A1

公开(公告)日：2021-08-04

申请号：EP19864137.5

申请日：2019-08-22

申请人： Nipponkayaku Kabushikikaisha

发明人： NAKAMURA, Hiroshi ,  YAGIHASHI, Yasuhiko ,  TAMASHIRO, Akihiro

IPC分类号： B64D17/34 ,  B64C13/20 ,  B64C27/08 ,  B64C31/036 ,  B64C39/02 ,  B64D17/80 ,  B64D45/00 ,  B64D45/04

摘要： To provide a flying object including a lift generating member deployment device that makes it easier than before to automatically avoid collision with an obstacle. A flying object 30 includes an obstacle detecting unit 5, a control unit 6, a battery 7, a storage unit 8 that stores information transmitted from the control unit 6, a transmitting/receiving unit 9 that receives an operation signal from a controller 40 and transmits information regarding the flying object 30 to the controller 40, and others. The obstacle detecting unit 5 is to detect the altitude of the flying object 30 and outputs an altitude detection signal, which represents the detected altitude information, to the control unit 6. In addition, upon detecting an obstacle present within a predetermined distance, the obstacle detecting unit 5 outputs an obstacle detection signal to the control unit 6, detects the distance between the flying object body 31 and the obstacle, and outputs a distance detection signal, which represents the detected distance information, to the control unit 6. The control unit 6 determines whether or not to actuate left and right brake cord pulling devices 10 in accordance with the signal received from the obstacle detecting unit 5.

公开(公告)号：EP3530567A1

公开(公告)日：2019-08-28

申请号：EP17924444.7

申请日：2017-09-08

申请人： Agatsuma Co., Ltd.

发明人： TODOKORO Shinji

IPC分类号： B64C39/02 ,  B64C13/20 ,  B64D27/24

摘要： A flying body 1 includes a fixed rotor supporting a first rotor blade to revolve, a movable rotor supporting a second rotor blade to revolve, and a drive unit for changing an angle of a second revolving plane Pr of the second rotor blade relative to a first revolving plane Pf of a first rotor blade by rotating the movable rotor. The drive unit changes operation modes of the flying body among a normal movement mode where the first revolving plane Pf becomes parallel to the second revolving plane Pr, a high-speed flight mode where the second revolving plane Pr is tilted towards the first rotor blade relative to the first revolving plane Pf, and a high-speed running mode where the second revolving plane Pr is tilted more towards the first rotor blade relative to the first revolving plane Pf than in the high-speed flight mode.

公开(公告)号：EP3521163A1

公开(公告)日：2019-08-07

申请号：EP16918244.1

申请日：2016-10-03

申请人： Aeronext Inc.

发明人： SUZUKI, Youichi

IPC分类号： B64C39/02 ,  B64C13/20 ,  B64D45/02 ,  B64D47/08

摘要： Provided is a delivery rotary-wing aircraft capable of stably landing on a destination without being affected by an updraft occurring in a high-rise building or the like. This rotary-wing aircraft comprising a plurality of rotary wings, a central portion to which a plurality of arms for supporting the rotary wings are connected, a first mounting portion for loading a package, a second mounting portion which is located on the opposite side to the first mounting portion as viewed from the central portion, a first supporting member for coupling the first mounting portion with the central portion, and a connection portion between the central portion and the first supporting member, is characterized by being controlled in such a manner that the center point of lift occurring in the rotary-wing aircraft with the rotation of the plurality of rotary wings and the center point of gravity of the rotary-wing aircraft coincide with the center point of the connection portion, and the first supporting member is equipped with an adjustment mechanism for vertically downwardly extending the length of the first supporting member.

公开(公告)号：EP3467492A1

公开(公告)日：2019-04-10

申请号：EP17802642.3

申请日：2017-05-17

申请人： NEC Corporation

发明人： YAMASHITA, Toshiaki ,  ADACHI, Hideo ,  SHOZAWA, Michitaro

IPC分类号： G01N29/04 ,  B64C13/20 ,  B64C39/02 ,  E01D22/00 ,  E21D11/00 ,  G05D1/00 ,  G01N29/12 ,  G05D1/02 ,  G05D1/10

摘要： The objective of the present invention is to make it possible for an inspection operator to carry out a hammering sound inspection without it being necessary for the inspection operator to perform an operation to move an inspection device to the location to be inspected, and to make it possible to carry out a hammering sound inspection even with respect to a location to be tested that is difficult for a vehicle to reach. This inspection system is provided with: a flying device provided with a hammering sound inspection unit which performs an inspection by hitting a location to be inspected from a prescribed relative position relative to the location to be inspected, and a flying unit on which the hammering sound inspection unit is mounted and which flies; a ground-side device which is installed in a fixed relative position relative to the location to be inspected and which detects the position of the flying device; and a flight instruction unit which, on the basis of the position of the flying device as detected by the ground-side device, controls the flying device in such a way that the forward direction of the flying device is oriented from the ground-side device toward the location to be inspected.

公开(公告)号：EP3321179A1

公开(公告)日：2018-05-16

申请号：EP15897684.5

申请日：2015-07-06

申请人： Zero Co., Ltd.

发明人： SUZUKI, Youichi

IPC分类号： B64C13/20 ,  B64C39/02 ,  B64D45/04 ,  B64F1/32

CPC分类号： G05D1/0676 ,  A47G29/14 ,  A47G2029/1221 ,  B64C13/20 ,  B64C39/02 ,  B64C39/024 ,  B64C2201/128 ,  B64D1/12 ,  B64D45/04 ,  B64F1/00 ,  B64F1/32 ,  G05D1/102 ,  G06Q10/0832 ,  G06Q10/08355 ,  G08G5/0069 ,  G08G5/02

摘要： A drone 1 loaded with a package takes off from a takeoff device 11 and uses a GPS system to fly to a user house 20 that is a delivery destination of the package as the destination. Further, when the drone 1 approaches the user house that is the destination, the flight of the drones 1 is switched from autonomous navigation using the GPS system to remote control performed by a landing device 21 and an in-house control device 22 installed in the user house 20. The drone 1 lands on the landing device 21 by remote control from the landing device 21 and the in-house control device 22, separates the package 50, and then returns to the warehouse 10 using the GPS system and lands on the takeoff device 11.

摘要翻译： 装有包裹的无人驾驶飞机1从起飞装置11起飞，并使用GPS系统飞行到作为目的地的包裹的配送目的地的用户房屋20。 此外，当无人驾驶飞机1靠近作为目的地的用户房屋时，无人驾驶飞机1的飞行从使用GPS系统的自主导航切换到由降落装置21和安装在该降落装置中的室内控制装置22执行的遥控 通过来自着陆装置21和室内控制装置22的远程控制，无人驾驶飞机1着陆在着陆装置21上，分离包装50，然后使用GPS系统返回到仓库10，并着陆在 起飞装置11。

公开(公告)号：EP2558817A4

公开(公告)日：2018-01-31

申请号：EP10857987

申请日：2010-09-30

申请人： EMPIRE TECH DEVELOPMENT LLC

发明人： KRUGLICK EZEKIEL

IPC分类号： G01C11/02 ,  B64C13/20 ,  G01C21/00 ,  G05D1/04

CPC分类号： B64C39/024 ,  B64C19/00 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/146 ,  G05D1/0088 ,  G05D1/0094 ,  G05D1/101 ,  G06T17/05 ,  G06T17/10 ,  G06T2210/21 ,  G06T2210/61

摘要： Technologies are generally described for controlling a flight path of a UAV based image capture system for solid modeling. Upon determining an initial movement path based on an estimate of a structure to be modeled, images of the structure to be modeled may be captured and surface hypotheses formed for unobserved surfaces based on the captured images. A normal vector and a viewing cone may be computed for each hypothesized surface. A set of desired locations may be determined based on the viewing cones for the entire structure to be modeled and a least impact path for the UAV determined based on the desired locations and desired flight parameters.

公开(公告)号：EP3015939A4

公开(公告)日：2017-04-26

申请号：EP14818709

申请日：2014-06-27

申请人： YAMAHA MOTOR CO LTD

发明人： ADACHI HAJIME

IPC分类号： G05D1/00 ,  A63H30/04 ,  B64C13/20 ,  B64C27/04

CPC分类号： G05D13/04 ,  A63H27/12 ,  A63H30/04 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/146 ,  G05D1/0016 ,  G05D1/0033 ,  G05D1/0202

摘要： There is provided a remote control device capable of easily maintaining transportation equipment at a desired speed. A remote control device (10) includes an instruction section (25) and a controller (26) which controls a speed of an unmanned helicopter (1) based on an instruction from the instruction section (25). The instruction section (25) is capable of selectively outputting one of a speed change signal for changing the speed of the unmanned helicopter (1) and a speed determination signal for determining the speed of the unmanned helicopter (1). When an output from the instruction section (25) is changed from the speed change signal to the speed determination signal, the controller (26) determines whether the speed of the unmanned helicopter (1) should be maintained or brought to zero, based on a result of comparison between speed information of the unmanned helicopter (1) and a threshold value. Preferably, the speed change signal is a signal which changes the speed of the unmanned helicopter (1) by changing a tilt angle of a nose of the unmanned helicopter (1) in an up-down direction in accordance with an amount of operation made to the instruction section (25).

摘要翻译： 提供了一种能够以期望的速度容易地维护运输设备的遥控装置。 遥控装置（10）包括根据来自指示部（25）的指示来控制无人直升机（1）的速度的指示部（25）和控制器（26）。 指令部分（25）能够选择性地输出用于改变无人直升机（1）的速度的速度改变信号和用于确定无人直升机（1）的速度的速度确定信号中的一个。 当指令部分（25）的输出从速度改变信号改变为速度确定信号时，控制器（26）基于a，确定无人直升机（1）的速度是应该保持还是归零 比较无人直升机的速度信息（1）与阈值的结果。 优选地，速度改变信号是这样的信号，其通过根据对无人直升机（1）的操作量在上下方向上改变无人直升机（1）的鼻子的倾斜角度来改变无人直升机（1）的速度 指令部分（25）。

公开(公告)号：EP3133019A1

公开(公告)日：2017-02-22

申请号：EP16179915.0

申请日：2010-09-09

申请人： AeroVironment, Inc.

发明人： Miralles, Carlos Thomas ,  Andryukov, Alexander ,  Su, Guan H. ,  McNeil, John

IPC分类号： B64F1/04 ,  F41F3/04 ,  B64C13/20 ,  F42B39/14 ,  F41F1/00

CPC分类号： B64F1/04 ,  B64C39/024 ,  B64C2201/08 ,  B64C2201/102 ,  B64C2201/146 ,  B64C2201/201 ,  B64F1/06 ,  F41A21/02 ,  F41F1/00 ,  F41F3/042 ,  F42B39/14

摘要： An unmanned aerial vehicle (UAV) launch tube (100) that comprises at least one inner layer of prepreg substrate (370) disposed about a right parallelepiped aperture (305), at least one outer layer of prepreg substrate (380) disposed about the right parallelepiped aperture (305), and one or more structural panels (341-344) disposed between the at least one inner layer of prepreg substrate (340) and the at least one outer layer of prepreg substrate (380). An unmanned aerial vehicle (UAV) launch tube (100) that comprises a tethered sabot (700,740) configured to engage a UAV within a launcher volume defined by an inner wall, the tethered sabot (700,740) dimensioned to provide a pressure seal at the inner wall and tethered to the inner wall, and wherein the tethered sabot (700,740) is hollow having an open end oriented toward a high pressure volume and a tether (740) attached within a hollow (910) of the sabot (700) and attached to the inner wall retaining the high pressure volume or attach to the inner base wall (1013). A system comprising a communication node (1500-1505) and a launcher (1520) comprising an unmanned aerial vehicle (UAV) in a pre-launch state configured to receive and respond to command inputs from the communication node (1500-1505).

摘要翻译： 一种无人飞行器（UAV）发射管（100），其包括围绕直角平行六面体孔（305）布置的至少一个预浸料坯基底（370）的内层，至少一个预浸料坯基底 （305）以及设置在所述至少一个预浸料坯衬底（340）的内层和所述至少一个预浸料坯衬底（380）的外层之间的一个或多个结构面板（341-344）。 1。一种无人驾驶飞行器（UAV）发射管（100），其包括被配置成在由内壁限定的发射器体积内接合UAV的系留弹底（700,740），所述系留弹壳（700,740）的尺寸被设计成在内部提供压力密封 （700,740）是中空的，具有朝向高压容积的开口端和连接在弹壳（700）的中空部（910）内并连接到所述内壁的系绳（740） 内壁保持高压容积或附接到内部基壁（1013）。 一种包括通信节点（1500-1505）和启动器（1520）的系统，所述通信节点（1500-1505）和启动器（1520）包括处于预启动状态的无人飞行器（UAV），其被配置为接收并响应来自通信节点（1500-1505）的命令输入。

公开(公告)号：EP3015939A1

公开(公告)日：2016-05-04

申请号：EP14818709.9

申请日：2014-06-27

申请人： Yamaha Hatsudoki Kabushiki Kaisha

发明人： ADACHI Hajime

IPC分类号： G05D1/00 ,  B64C13/20 ,  B64C27/04 ,  A63H30/04

CPC分类号： G05D13/04 ,  A63H27/12 ,  A63H30/04 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/146 ,  G05D1/0016 ,  G05D1/0033 ,  G05D1/0202

摘要： There is provided a remote control device capable of easily maintaining transportation equipment at a desired speed. A remote control device (10) includes an instruction section (25) and a controller (26) which controls a speed of an unmanned helicopter (1) based on an instruction from the instruction section (25). The instruction section (25) is capable of selectively outputting one of a speed change signal for changing the speed of the unmanned helicopter (1) and a speed determination signal for determining the speed of the unmanned helicopter (1). When an output from the instruction section (25) is changed from the speed change signal to the speed determination signal, the controller (26) determines whether the speed of the unmanned helicopter (1) should be maintained or brought to zero, based on a result of comparison between speed information of the unmanned helicopter (1) and a threshold value. Preferably, the speed change signal is a signal which changes the speed of the unmanned helicopter (1) by changing a tilt angle of a nose of the unmanned helicopter (1) in an up-down direction in accordance with an amount of operation made to the instruction section (25).

摘要翻译： 提供了一种能够以期望的速度容易地维护运输设备的遥控装置。 遥控装置（10）包括根据来自指示部（25）的指示来控制无人直升机（1）的速度的指示部（25）和控制器（26）。 指令部分（25）能够选择性地输出用于改变无人直升机（1）的速度的速度改变信号和用于确定无人直升机（1）的速度的速度确定信号中的一个。 当指令部分（25）的输出从速度改变信号改变为速度确定信号时，控制器（26）基于a，确定无人直升机（1）的速度是应该保持还是归零 比较无人直升机的速度信息（1）与阈值的结果。 优选地，速度改变信号是这样的信号，其通过根据对无人直升机（1）的操作量在上下方向上改变无人直升机（1）的鼻子的倾斜角度来改变无人直升机（1）的速度 指令部分（25）。