公开(公告)号：WO2007086055A1

公开(公告)日：2007-08-02

申请号：PCT/IL2007/000090

申请日：2007-01-25

Applicant: ISRAEL AEROSPACE INDUSTRIES LTD. ,  SOMECH, Haim

Inventor： SOMECH, Haim

IPC: B64C39/02 ,  B63B35/52 ,  B64D17/80 ,  B64F1/02

CPC classification number: B64C39/024 ,  B63B35/52 ,  B64C2201/021 ,  B64C2201/084 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/145 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/185 ,  B64C2201/205 ,  B64F1/02

Abstract: The invention provides a system, method and landing device for landing an aircraft (50) with respect to a predetermined landing location (P). The aircraft is configured for powered flight at least when the parafoil (60) is deployed, and includes an automatic landing system for controllably executing a landing approach maneuver for the aircraft while in free powered flight with the parafoil deployed to enable the aircraft to be brought into overlying proximity with the landing location. A landing device in the form of an energy absorbing landing net arrangement (20) is provided at the landing location for enabling the aircraft to be landed thereon at least partially vertically when in overlying proximity, and for dampening the landing impact of the aircraft.

Abstract translation: 本发明提供了一种用于相对于预定着陆位置（P）降落飞机（50）的系统，方法和着陆装置。 该飞机至少在翼展（60）部署时配置为动力飞行，并且包括一个自动着陆系统，用于在自由动力飞行中可控制地执行飞机的着陆进场操纵，其中部署了翼型飞机以使飞机能够被带到 与着陆位置相邻。 在着陆位置处设置能量吸收着陆网装置（20）形式的着陆装置，用于使飞机在覆盖在邻近位置时至少部分垂直地落在其上，并用于减轻飞机的着陆冲击。

公开(公告)号：US20180262674A1

公开(公告)日：2018-09-13

申请号：US15760276

申请日：2016-10-11

Applicant: Mitsubishi Electric Corporation

Inventor： Takashi IWAKURA ,  Takayuki ISHIDA

IPC: H04N5/232 ,  B64D47/08 ,  B64C39/02 ,  G05D1/00 ,  G01B11/24

CPC classification number: H04N5/23203 ,  B64C39/024 ,  B64C2201/123 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/185 ,  B64D17/00 ,  B64D47/08 ,  G01B11/24 ,  G01C11/06 ,  G01C15/00 ,  G05D1/0044 ,  G05D1/102 ,  H04N5/2257 ,  H04N5/23225

Abstract: An image capturing system for shape measurement includes: an image capturing device configured to capture an image of a structure; an air vehicle; an on-board control device configured to control the image capturing device and the air vehicle in accordance with an image capturing scenario; and a remote control device configured to create an image capturing scenario and transfer the created image capturing scenario to the on-board control device. The air vehicle autonomously flies to image capturing points sequentially so as to capture images. The captured data is transmitted to the remote control device via a wireless LAN.

公开(公告)号：US20180162552A1

公开(公告)日：2018-06-14

申请号：US15879166

申请日：2018-01-24

Applicant: Kitty Hawk Corporation

Inventor： Zachais Vawter ,  Todd Reichert

IPC: B64D45/04 ,  G05D1/10 ,  B64D17/72 ,  B64D1/10 ,  B64D1/12 ,  B64D25/08 ,  B64D17/80 ,  B64C39/02 ,  B64D45/00

CPC classification number: B64D45/04 ,  B64C39/024 ,  B64C2201/042 ,  B64C2201/185 ,  B64D1/10 ,  B64D1/12 ,  B64D17/725 ,  B64D17/80 ,  B64D25/08 ,  B64D2045/008 ,  G05D1/101

Abstract: A ballistic parachute associated with an aircraft is deployed where the aircraft includes a first part and a second part, the two parts are detachably coupled to each other when the ballistic parachute is deployed, and the ballistic parachute is coupled to the first part of the aircraft. A landing zone associated with the second part of the aircraft is determined and it is decided whether to decouple the two parts, including by deciding whether the landing zone associated with the second part of the aircraft is inhabited. If it is decided to decouple the two parts from each other, they are decoupled from each other.

公开(公告)号：US20170371332A1

公开(公告)日：2017-12-28

申请号：US15698303

申请日：2017-09-07

Applicant: SkyCat Oy

Inventor： Henri Hiisilä ,  Janne Laurinen

IPC: G05D1/00 ,  B64C19/00 ,  B64C39/02 ,  G08C17/02 ,  A63H30/04 ,  A63H33/20 ,  B64D17/80

CPC classification number: G05D1/0022 ,  A63H30/04 ,  A63H33/20 ,  B64C19/00 ,  B64C39/024 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/185 ,  B64D17/80 ,  G05D1/0055 ,  G08C17/02

Abstract: The present invention relates to a method for replacing a signal controlling an actuator in a remote-controlled flying device with another signal. A flight controller supplies control signals to a safety device, and the signal to be replaced may be a signal to be transmitted by the safety device to a speed controller of at least one motor, or to a servo unit controlling the same, or the signal to be replaced may be a signal to be transmitted from the safety device to a servo unit controlling legs, a camera rack, a camera, a stabilizing system or an electric motor of the flying device. A replacement signal is a signal stored in a memory of the safety device. The replacement signal may be capable of controlling the speed controller directly or via the servo unit, in such a way that power transmission to said motor/motors is stopped or reduced, and this motor is/these motors are switched off or its/their rotation is decelerated, or the replacement signal may be capable of controlling said servo unit in such a way that said actuator is moved to a second position. The replacement signal may be a signal to be transmitted from a receiver past a flight controller, capable of controlling the speed controller or servo unit of the motor in such a way that power transmission to the motor is stopped or reduced, or to control said actuator in such a way that this actuator is moved to another position.

公开(公告)号：US20170267348A1

公开(公告)日：2017-09-21

申请号：US15612989

申请日：2017-06-02

Applicant: Flirtey Holdings, Inc.

Inventor： Matthew Sweeny ,  John Elverum ,  John Foggia

IPC: B64D1/22 ,  B65D25/22 ,  B65D5/50 ,  B65D81/38 ,  B65D5/10 ,  A47J47/14 ,  B64C39/02 ,  B65D25/34

CPC classification number: B65D5/5007 ,  A47J47/14 ,  B64C25/58 ,  B64C39/024 ,  B64C2201/146 ,  B64C2201/185 ,  B64D17/70 ,  B64D17/80 ,  B65D5/10 ,  B65D25/22 ,  B65D25/34 ,  B65D81/3813

Abstract: Certain aspects of the technology disclosed involve a container for delivery by drone (e.g., an unmanned aerial vehicle). The container can include a coupling mechanism to lock and unlock a package attached to the drone based on a tension applied to the coupling mechanism. The package can include sidewalls affixed to a top wall. The sidewalls can include securing mechanisms to be secured to a bottom wall of the container. A rigid extremity can be a contiguous extension of any of the sidewalls and extend below a lower surface of the sidewalls. The rigid extremity can include a malleable contour proximate to a corner of the container. The malleable contour can extend from a base of the rigid extremity through the sidewall. An aperture in the top wall can be configured for a inserting member of a coupling mechanism.

公开(公告)号：US20170152051A1

公开(公告)日：2017-06-01

申请号：US15065963

申请日：2016-03-10

Applicant: OPTiM Corporation

Inventor： Shunji SUGAYA

IPC: B64D25/00 ,  B64C39/02

CPC classification number: B64D25/00 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/146 ,  B64C2201/185

Abstract: The present invention is to prevent an uninhabited airborne vehicle from crashing due to fall impact and from being damaged and to protect an object and a living being at the fall point. The uninhabited airborne vehicle 100 includes a rotary wing 10 and a buffer 111 that reduces impact on the airframe when crashed. The battery charge remaining measurement module 122 and the distance measurement module 123 measure the battery charge remaining and the distance to an object, respectively, and compare the measurement with the respective thresholds. If the measurement is less than the respective thresholds, the buffer module 111 is driven by the drive module 121.

公开(公告)号：US20160313734A1

公开(公告)日：2016-10-27

申请号：US15134284

申请日：2016-04-20

Applicant: GoPro, Inc.

Inventor： Joseph Anthony Enke

IPC: G05D1/00 ,  G08G5/04 ,  G08G5/00 ,  B64C39/02 ,  G07C5/08

CPC classification number: G05D1/0044 ,  B64C39/024 ,  B64C2201/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/145 ,  B64C2201/146 ,  B64C2201/18 ,  B64C2201/185 ,  B64C2201/20 ,  G01C23/00 ,  G05D1/0022 ,  G05D1/0038 ,  G05D1/0088 ,  G05D1/101 ,  G05D1/102 ,  G07C5/08 ,  G08G5/0013 ,  G08G5/0021 ,  G08G5/0026 ,  G08G5/0034 ,  G08G5/0039 ,  G08G5/006 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/0086 ,  G08G5/0091 ,  G08G5/045 ,  H04B7/18504 ,  H04W84/042 ,  H04W84/12

Abstract: Disclosed is a configuration to control automatic return of an aerial vehicle. The configuration stores a return location in a storage device of the aerial vehicle. The return location may correspond to a location where the aerial vehicle is to return. One or more sensors of the aerial vehicle are monitored during flight for detection of a predefined condition. When a predetermined condition is met a return path program may be loaded for execution to provide a return flight path for the aerial vehicle to automatically navigate to the return location.

Abstract translation: 公开了一种用于控制飞行器的自动返回的配置。 该配置将返回位置存储在飞行器的存储装置中。 返回位置可以对应于飞行器返回的位置。 在飞行中监视航空器的一个或多个传感器以检测预定义的状况。 当满足预定条件时，可以加载返回路径程序以执行以提供飞行器自动导航到返回位置的返回飞行路径。

公开(公告)号：US20160286128A1

公开(公告)日：2016-09-29

申请号：US15172673

申请日：2016-06-03

Applicant: Dylan TX Zhou

Inventor： Dylan TX Zhou

IPC: H04N5/232 ,  H04N7/00 ,  B64C39/02 ,  H04N5/38

CPC classification number: H04N5/23248 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/185 ,  B64D2211/00 ,  G06Q2220/00 ,  H04L65/1069 ,  H04L65/602 ,  H04L65/80 ,  H04N5/23238 ,  H04N5/38 ,  H04N7/00

Abstract: A mobile case system comprising a real time broadcast stream recording; an unmanned aerial vehicle; a camera stabilization device; a camera movement device; one or more onboard cameras providing real-time first-person video and real-time first-person views and and 360-degree panoramic video recording used for virtual reality views and interactive video; a video transmitter and receiver device configured to perform high definition low latency real time video downlink; a one and two way telemetry device; a live broadcast device; a headset enabling real-time first-person video; a public database for viewing flight activity; software for licensing videos with a watermarked preview; software for autonomously extracting and compiling the usable video footage into a video montage synced to music; and onboard or separate software for stitching videos to form virtual reality views or interactive video, alternative embodiments the case may be adapted as power bank memory device, and use for aerial delivery.

Abstract translation: 一种包括实时广播流记录的移动案例系统; 无人机; 相机稳定装置; 相机运动装置; 提供实时第一人称视频和实时第一人称视图的一个或多个车载摄像机和用于虚拟现实视图和交互式视频的360度全景视频记录; 配置为执行高清晰度低延迟实时视频下行链路的视频发射机和接收机设备; 一路双向遥测装置; 一个直播广播设备; 支持实时第一人称视频的耳机; 用于查看飞行活动的公共数据库; 使用水印预览授权视频的软件; 用于自动提取和编译可视频录像到同步到音乐的视频蒙太奇的软件; 以及用于拼接视频以形成虚拟现实视图或交互式视频的机载或单独的软件，该情况可以适用于电力银行存储器设备的替代实施例，并且用于空中传送。

公开(公告)号：US09234973B2

公开(公告)日：2016-01-12

申请号：US13870325

申请日：2013-04-25

Applicant: The Boeing Company

Inventor： David Scarlatti ,  David Esteban-Campillo ,  Javier Garcia

IPC: G01V1/16 ,  B64C27/68 ,  B64C39/02 ,  B64C27/51 ,  G01V1/18 ,  F42B12/36

CPC classification number: G01V1/168 ,  B64C27/51 ,  B64C27/68 ,  B64C39/02 ,  B64C2201/082 ,  B64C2201/123 ,  B64C2201/185 ,  F42B12/365 ,  G01V1/16 ,  G01V1/182

Abstract: A method includes enabling a power supply of a ground sensor device to provide power to one or more components of the ground sensor device based on one or more rotations of a rotor of the ground sensor device.

Abstract translation: 一种方法包括使得地面传感器装置的电源能够基于地面传感器装置的转子的一个或多个旋转来向地面传感器装置的一个或多个部件供电。

公开(公告)号：US09033281B1

公开(公告)日：2015-05-19

申请号：US13410225

申请日：2012-03-01

Applicant: Richard D. Adams

Inventor： Richard D. Adams

IPC: B64D9/00

CPC classification number: B64D9/00 ,  B64C39/024 ,  B64C2201/107 ,  B64C2201/127 ,  B64C2201/162 ,  B64C2201/185 ,  B64C2201/203

Abstract: A radio controlled UAV is disclosed. The UAV includes a parachute, with a cylindrical power and control module suspended vertically below the parachute. In one embodiment, a propulsion source is mounted on top of the power and control module with control lines connected to the module below the propulsion source, and in another embodiment the power and control module is suspended from a point above a propulsion source. The UAV is controlled by radio controls from a hand held controller, with actuators retracting and letting out control lines attached to the parachute in order to control direction of the parachute. The UAV may be launched from a tube using a pressurized tank with a nozzle expelling gas from the tank, the tank and nozzle towing a canister from which the UAV is deployed.

Abstract translation: 公开了一种无线电控制的无人机。 无人机包括一个降落伞，一个圆柱形的电源和控制模块垂直悬挂在降落伞下方。 在一个实施例中，推进源安装在功率和控制模块的顶部，其控制线连接到推进源下方的模块，并且在另一个实施例中，功率和控制模块从推进源上方的点悬挂。 无人机由手持控制器的无线电控制控制，执行器缩回并释放连接到降落伞的控制线，以控制降落伞的方向。 无人机可以使用加压罐从管中发射，喷嘴排出来自罐，罐和喷嘴的气体，其牵引无人机从其部署的罐。