公开(公告)号：EP2515147B1

公开(公告)日：2016-10-26

申请号：EP12002777.6

申请日：2012-04-20

Applicant: Accenture Global Services Limited

Inventor： Spata, Gregory P.

IPC: G01W1/00 ,  G01W1/08 ,  B64C39/02 ,  G05D1/02

CPC classification number: G01W1/00 ,  B64C2201/125 ,  G01C23/00 ,  G01W1/08 ,  G01W2001/006 ,  G05D1/102 ,  G05D23/19 ,  G08G5/0069

公开(公告)号：EP3216335A1

公开(公告)日：2017-09-13

申请号：EP17401021.5

申请日：2017-03-02

Applicant: Amazonen-Werke H. Dreyer GmbH & Co. KG

Inventor： Wild, Karl

IPC: A01C21/00 ,  A01B79/00

CPC classification number: A01C21/007 ,  A01B79/005 ,  A01C17/008 ,  B64C39/024 ,  B64C2201/125 ,  B64C2201/208 ,  G01P5/00

Abstract: System und Verfahren zur Erfassung des Windes (10) bei Verteilvorgängen in der Landwirtschaft durch eine Erfassungsvorrichtung wenigstens eines im Wesentlichen vorzugsweise senkrecht start- und landefähiges, vorzugsweise autonom agierenden, unbemannten Luftfahrzeugs (12), welches wenigstens eine Einheit zur Erfassung von Umgebungsparametern aufweist, welches eine Einheit zum Empfangen von Steuersignalen von einer Basisstation und/oder Senden von Steuersignalen an ein landwirtschaftliches Arbeitsgerät (5) und eine Einheit zur Übermittlung der erfassten Umgebungsparameter an eine Basisstation und/oder an ein landwirtschaftliches Arbeitsgerät (5) aufweist. Um eine Echtzeit-Anpassung der Betriebsparameter einer landwirtschaftlichen Verteilmaschine an die vorherrschenden Windverhältnisse (10) zu ermöglichen, werden die Windverhältnisse über einer zu bearbeitenden Fläche (1) mithilfe der Erfassung von Windindikatoren (15) und/oder geeigneten Sensoren zur Erfassung von Windgeschwindigkeit(en) und/oder -richtung(en) erfasst.

Abstract translation: 由感测装置的至少一个优选地基本上垂直起飞和着陆能力的系统和方法，用于检测在Verteilvorgängen在农业风（10）的，优选地自主操作，无人飞行载具（12）具有至少一个单元，用于检测环境参数，这 用于从基站接收控制信号和/或向农具（5）发送控制信号的单元以及用于将检测到的环境参数传送到基站和/或农具（5）的单元。 为了使农业分配器与盛行风条件（10）的操作参数的实时调整，风条件是一个表面的上方被加工（1），使用的风指标的检测（15）和/或合适的传感器用于检测风速（S ）和/或方向。

公开(公告)号：EP3044092A2

公开(公告)日：2016-07-20

申请号：EP14844886.3

申请日：2014-09-11

Applicant: Silicis Technologies Inc.

Inventor： STIGLER, Michael J. ,  SETAR, Nicholas James

IPC: B64F1/12

CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

公开(公告)号：EP2977318A1

公开(公告)日：2016-01-27

申请号：EP15178010.3

申请日：2015-07-23

Applicant: ATM S.r.l.

Inventor： PETACCHI, Gianfranco

IPC: B64C39/02 ,  B64D1/12 ,  F42D3/00

CPC classification number: B64C39/024 ,  B64C2201/121 ,  B64C2201/125 ,  B64D1/12 ,  F42D3/00

Abstract: Remotely piloted aircraft or drone (1) adapted to induce artificial avalanche detachment, comprising: operating members (10) adapted to bring and/or keep said aircraft (1) in a flight condition; a cable (20) for connecting said aircraft (1) to an explosive charge (30) and holding said charge (30) suspended outside said aircraft (1); a triggering device (40) configured for causing the explosion of said charge (30).

Abstract translation: 遥控飞机或无人驾驶飞机（1）angepasst诱导人工雪崩脱离，包括：操作构件（10）适于使和/或保持所述飞行器（1）的飞行条件; 在可爆炸的炸药（30）悬挂在所述飞行器外部所述飞行器（1）连接至和保持所述电荷（30）的电缆（20）（1）; 构造成用于使所述电荷（30）的爆炸的触发装置（40）。

公开(公告)号：EP2103340B1

公开(公告)日：2015-06-17

申请号：EP09001803.7

申请日：2009-02-10

Applicant: Astrium GmbH

Inventor： Konigorski, Detlev

IPC: B64B1/20 ,  B01D53/00

CPC classification number: B64B1/20 ,  B01D53/002 ,  B01D2257/2025 ,  B01D2257/2064 ,  B01D2259/4558 ,  B64B2201/00 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/125 ,  Y10S244/90

公开(公告)号：KR101429157B1

公开(公告)日：2014-08-12

申请号：KR1020130150276

申请日：2013-12-04

Applicant: 대한민국(기상청 국립기상과학원장)

Inventor： 최규용 ,  이용희 ,  안광득 ,  이희춘

IPC: G01W1/00 ,  G01C11/02

CPC classification number: Y02A90/14 ,  G01W1/08 ,  B64C2201/125 ,  B64D47/08 ,  G01C11/02 ,  G06T2207/10032 ,  G06T2207/30192

Abstract: The present invention relates to a mode-convertible imaging system mounted on an aerial vehicle for meteorological observation. Specifically, the imaging system according to the present invention includes a fixed camera which is mounted on a central portion of the aerial vehicle; a rotating camera group having a left side rotating camera which is disposed on a left side of the fixed camera, and a right side rotating camera which is disposed on a right side of the fixed camera; and a control unit that controls conversion between (i) a single mode in which imaging is performed by the left side rotating camera, the right side rotating camera, and the fixed camera at a position on a rotation trajectory where the left side rotating camera and the right side rotating camera are in a direction substantially parallel to a direction of the fixed camera while the left side rotating camera and the right side rotating camera rotate along rotation trajectories thereof and (ii) a multi mode in which imaging is performed by the left side rotating camera, the right side rotating camera, and the fixed camera at a position on the rotation trajectory where the left side rotating camera and the right side rotating camera face the same subject as a subject the fixed camera faces while the left side rotating camera and the right side rotating camera rotate along the rotation trajectories thereof. According to the present invention, both general images and three-dimensional images of meteorological observation data can be obtained at the same time through a single flight.

Abstract translation: 本发明涉及安装在用于气象观测的飞行器上的可转换模式成像系统。 具体地，根据本发明的成像系统包括安装在飞行器的中心部分上的固定摄像机; 具有设置在固定摄像机的左侧的左侧旋转摄像机的旋转摄像机组和设置在固定摄像机的右侧的右侧旋转摄像机; 以及控制单元，其控制在所述左侧旋转相机和所述左侧旋转相机的旋转轨迹上的位置处的（i）由所述左侧旋转相机，所述右侧旋转相机和所述固定照相机执行成像的单个模式之间的转换;以及 右侧旋转摄像机处于与固定摄像机的方向基本平行的方向上，而左侧旋转摄像机和右侧旋转摄像机沿其旋转轨迹旋转，以及（ii）左侧进行摄像的多种模式 侧旋转摄像机，右侧旋转摄像机和固定摄像机在旋转轨迹上的位置，其中左侧旋转摄像机和右侧旋转摄像机面对与固定摄像机所面对的被摄体相同的被摄体，而左侧旋转摄像机 并且右侧旋转摄像机沿其旋转轨迹旋转。 根据本发明，可以通过单次飞行同时获得气象观测数据的一般图像和三维图像。

公开(公告)号：US20190219488A1

公开(公告)日：2019-07-18

申请号：US16248580

申请日：2019-01-15

Applicant: Richard John McNamara

Inventor： Richard John McNamara

IPC: G01N1/22 ,  B64D47/00 ,  B64C39/02

CPC classification number: G01N1/2247 ,  B64C39/024 ,  B64C2201/125 ,  B64D47/00 ,  G01N1/2273

Abstract: A system for converting propelling thrust to produce a continuous flow is provided. The system can be integrated and/or retrofitted to the body of an aircraft. The system includes a pressure-lowering device and a sample chamber. The pressure-lowering device is used produce a low-pressure, continuous flow from a high-velocity propelling thrust source. Moreover, the pressure-lowering device is a passive flow generator that does not require a power source in order to produce a continuous flow from a propelling thrust. The design of the pressure-lowering device produces a flow rate that is independent of the aircraft motion. The sample chamber is used to measure and analyze ambient gases which are pulled through the sample chamber by the pressure-lowering device, as a result of the high-velocity air stream produced by the propelling thrust source.

公开(公告)号：US20180259429A1

公开(公告)日：2018-09-13

申请号：US15530844

申请日：2017-03-07

Applicant: Alexander B. Adams

Inventor： Alexander B. Adams

IPC: G01N1/22 ,  G01N33/00 ,  B64C39/02 ,  B64D1/00

CPC classification number: G01N1/2273 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/108 ,  B64C2201/12 ,  B64C2201/125 ,  B64C2201/128 ,  B64C2201/165 ,  B64D1/00 ,  G01N33/0073 ,  G01N2001/245

Abstract: An atmosphere sampling system includes: an unmanned rotary-wing aircraft platform including: an airframe capable of lifting a selected payload mass; at least one motorized rotor; and, a flight control system including an on-board controller; an atmosphere sampling unit having a total mass no greater than the selected payload mass, and including: a blower preferably having backward-facing blades, an inlet structure to draw in air to be sampled, and an outlet to discharge air after sampling; a plurality of sample containers; and, an indexing mechanism to move selected sample containers, one at a time, into contact with the inlet structure so that samples may be collected; and, a power supply with sufficient capacity to operate the motorized rotor(s), the onboard portion of the flight controller, the blower, and the indexing system.

公开(公告)号：US20180244386A1

公开(公告)日：2018-08-30

申请号：US15893992

申请日：2018-02-12

Applicant: Top Flight Technologies, Inc.

Inventor： Long N. Phan

IPC: B64C39/02 ,  B64C27/12 ,  G08G5/00 ,  G01W1/02

CPC classification number: B64C39/024 ,  B64C27/12 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/108 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/162 ,  B64C2201/165 ,  B64C2201/208 ,  B64D2027/026 ,  G01W1/02 ,  G01W1/08 ,  G08G5/0069 ,  G08G5/0091

Abstract: An unmanned aerial vehicle includes an atmospheric sensor configured to measure an atmospheric condition. The unmanned aerial vehicle includes a rotor motor configured to drive rotation of a propeller of the unmanned aerial vehicle. The unmanned aerial vehicle includes a hybrid energy generation system including a rechargeable battery configured to provide electrical energy to the rotor motor; an engine configured to generate mechanical energy; and a generator coupled to the engine and configured to generate electrical energy from the mechanical energy generated by the engine, the electrical energy generated by the generator being provided to at least one of the rechargeable battery and the rotor motor.

公开(公告)号：US09902495B2

公开(公告)日：2018-02-27

申请号：US15594255

申请日：2017-05-12

Applicant: Top Flight Technologies, Inc.

Inventor： Long N. Phan ,  Samir Nayfeh ,  John J. Polo ,  Eli M. Davis ,  Paul A. DeBitetto

IPC: B64C39/02 ,  B64D47/08 ,  G08G5/00

CPC classification number: B64C39/024 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/108 ,  B64C2201/125 ,  B64D47/08 ,  B64D2221/00 ,  G08G5/0013 ,  G08G5/0039 ,  G08G5/0056 ,  G08G5/0069 ,  G08G5/025

Abstract: An unmanned aerial vehicle includes at least one rotor motor configured to drive at least one propeller to rotate. The unmanned aerial vehicle includes a data center including a processor; a data storage component; and a wireless communications component. The unmanned aerial vehicle includes a hybrid generator system configured to provide power to the at least one rotor motor and to the data center, the hybrid generator system including a rechargeable battery configured to provide power to the at least one rotor motor; an engine configured to generate mechanical power; and a generator motor coupled to the engine and configured to generate electrical power from the mechanical power generated by the engine. The data center may include an intelligent data management module configured to control power distribution and execution of mission tasks in response to available power generation and mission task priorities.