公开(公告)号：WO2014000729A9

公开(公告)日：2014-06-19

申请号：PCT/DE2013000352

申请日：2013-06-24

Applicant: EMAMI ARMAN

Inventor： EMAMI ARMAN

IPC: B64B1/44 ,  A63H27/10

CPC classification number: B64C39/024 ,  A63H27/10 ,  A63H2027/1066 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/101 ,  B64C2201/162

Abstract: A flying robot (1) which is carried by a gas balloon for use in interior spaces is proposed, wherein the gas balloon (2) can be adjusted in such a way that a horizontal hovering height which is provided or predefined can be adjusted or implemented. Working devices (5) are located in a valve unit (3) and/or a housing which is arranged underneath the gas balloon (2). Together with the valve unit (3) or the housing, a drive unit (4) of which the direction can be adjusted is provided with respect to said unit and said housing for moving the flying robot (1). The flying robot can be used both for monitoring tasks and for filming.

Abstract translation: 所支持的气体的气球飞行机器人（1），用于内部空间的使用，其中所述气体球囊（2）是可调节的，使得预期的或预定的水平的浮动高度是可调节的或可行的。 在阀单元（3）和/或在气体球囊（2）布置在所述壳体的下方有工作装置（5）。 与阀单元（3）或所述壳体的飞行机器人（1）的移动相对地设置该一个方向上调节驱动单元（4）。 随着飞行机器人两种监测任务以及电影镜头可以实现的。

公开(公告)号：WO2012118731A3

公开(公告)日：2012-12-27

申请号：PCT/US2012026716

申请日：2012-02-27

Applicant: CIAMPA JOHN A

Inventor： CIAMPA JOHN A

IPC: B64B1/58 ,  B64B1/62 ,  B64C39/02 ,  B64D47/08

CPC classification number: B64C39/024 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/127 ,  B64C2201/146 ,  B64D47/08

Abstract: Lighter-than-air systems, methods, and kits for obtaining aerial images are described. For example, various methods for determining planned ascent, drift, and/ or descent of a lighter-than-air system are described. In addition, various structural arrangements of lighter-than-air systems for accomplishing planned ascent, drift, and/or descent and obtaining aerial images are described.

Abstract translation: 描述了用于获取空中图像的比空气系统更轻的方法和套件。 例如，描述了用于确定轻于空气系统的计划上升，漂移和/或下降的各种方法。 此外，描述了用于实现计划上升，漂移和/或下降并获得空中图像的轻于空气系统的各种结构布置。

公开(公告)号：WO2004106156A1

公开(公告)日：2004-12-09

申请号：PCT/GB2004/002209

申请日：2004-05-20

Applicant: QINETIQ LIMITED ,  KELLEHER, Christopher, Charles

Inventor： KELLEHER, Christopher, Charles

IPC: B64C37/02

CPC classification number: B64C37/02 ,  B64C39/024 ,  B64C39/026 ,  B64C2201/021 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/101 ,  B64C2201/104 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/128 ,  B64C2201/146 ,  B64C2201/148 ,  B64C2201/201 ,  B64D5/00

Abstract: A heavier-than-air air vehicle (1), particularly a long endurance, solar powered, unmanned aerial vehicle (UAV) intended for "perpetual" flight within the stratosphere, is carried to its operational altitude suspended on a tether (14) from a helium balloon (16). The tether is attached at or towards a tip of the UAV's wing (3) so that it is carried in effectively a 90° banked attitude. At the desired altitude the UAV's powerplant is started and it flies on its tether in an upwardly-spiralling path relative to the balloon until a level or near level attitude is attained, when the tether is released and the UAV is permitted to assume free flight.

Abstract translation: 一架重型空中飞行器（1），特别是用于在平流层内“永久”飞行的长寿命的太阳能无人驾驶飞行器（UAV）被运载到悬挂在系绳（14）上的操作高度 氦气球（16）。 系绳连接在无人机翼（3）的尖端处或朝向无人机翼（3）的尖端，使得其有效地承载90度的组合姿态。 在所需的高度，UAV的动力装置启动，并且相对于气球以相对于气球的向上螺旋方式飞行，直到达到水平或近似水平的姿态时，系绳被释放并且UAV被允许进行自由飞行。

公开(公告)号：WO2003004352A1

公开(公告)日：2003-01-16

申请号：PCT/JP2002/006031

申请日：2002-06-17

Applicant: セイコーエプソン株式会社

Inventor： 赤堀 豊

IPC: B64B1/06

CPC classification number: G08G5/0052 ,  B64B1/06 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/042 ,  B64C2201/048 ,  B64C2201/101 ,  B64C2201/122 ,  B64C2201/141 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/167 ,  B64F1/18 ,  G01S5/20 ,  G01S5/22 ,  G05D1/0202 ,  G08G5/00 ,  G08G5/0013

Abstract: An airship system, comprising an airship (110), a base station (120), and at least three measurement points, wherein, when the airship (110) receiving an instruction from the base station (120) transmits ultrasonic wave, the measurement point units (S1 to S3) receive the ultrasonic wave to measure distances between the airship and the three measurement points and an MPU incorporated in the base station (120) calculates the position of the airship (110) and, according to the calculated position, the base station (120) transmits a navigation instruction to the airship (110) to control the route of the airship (110), whereby the operation of the airship by an operator can be eliminated, and the weight of loads mounted on the airship and the power consumption thereof can be reduced.

Abstract translation: 一种飞艇系统，包括飞艇（110），基站（120）和至少三个测量点，其中当接收到来自基站（120）的指令的飞艇（110）发射超声波时，测量点 单元（S1至S3）接收超声波以测量飞艇与三个测量点之间的距离，并且包含在基站（120）中的MPU计算飞艇（110）的位置，并且根据计算的位置， 基站（120）向飞艇（110）发送导航指令以控制飞艇（110）的路线，由此可以消除操作者的飞艇的操作，并且安装在飞艇上的载荷和 其功耗可以降低。

公开(公告)号：EP2686237B1

公开(公告)日：2017-08-16

申请号：EP12711224.1

申请日：2012-03-07

Applicant: Voliris

Inventor： BERNARD, Alain

IPC: B64B1/04 ,  B64B1/62

CPC classification number: B64B1/58 ,  B64B1/04 ,  B64B1/62 ,  B64C2201/022 ,  B64C2201/101

公开(公告)号：EP3044092A4

公开(公告)日：2017-08-02

申请号：EP14844886

申请日：2014-09-11

Applicant: SILICIS TECH 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.

Abstract translation: 所公开的实施例包括用于由命令和控制界面控制的自主车辆的拖车。 拖车包括配置成将自主车辆保持在未展开配置中的拖车主体。 拖车还将自主车辆锚定在展开配置中。 提供系绳，其具有联接到拖车主体的第一端部和构造成联​​接到自主车辆的第二端部。 利用绞车调节系绳的长度以使自主车辆在未展开配置和展开配置之间移动。 此外，通信系统与命令和控制接口以及自主车辆通信，以控制自主车辆在未部署配置和部署配置之间的移动。

公开(公告)号：EP3013686B1

公开(公告)日：2017-04-05

申请号：EP14752660.2

申请日：2014-06-30

Applicant: Bellezza Quater, Paolo

Inventor： Bellezza Quater, Paolo

IPC: B64C27/20 ,  B64B1/34 ,  B64C3/30 ,  B64C39/02 ,  B64B1/30

CPC classification number: B64C39/024 ,  B64B1/34 ,  B64C3/30 ,  B64C27/20 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/101 ,  B64C2201/105 ,  B64C2201/165

公开(公告)号：EP2996937B1

公开(公告)日：2017-01-11

申请号：EP14732257.2

申请日：2014-05-09

Applicant: Ridengineering

Inventor： JONIOT, Jacques

IPC: B64B1/40 ,  B64C27/20 ,  B64C17/04 ,  B64C27/22 ,  B64C39/02 ,  B64B1/44

CPC classification number: B64C27/22 ,  B64B1/40 ,  B64B1/44 ,  B64C17/04 ,  B64C27/20 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/066 ,  B64C2201/101 ,  B64C2201/108 ,  B64C2201/122 ,  B64C2201/123 ,  B64D2211/00

公开(公告)号：EP3013680A1

公开(公告)日：2016-05-04

申请号：EP14817368.5

申请日：2014-06-26

Applicant: Plimp, Inc.

Inventor： EGAN, James, C. ,  EGAN, Joel, D.

IPC: B64B1/00

CPC classification number: B64B1/20 ,  B64B1/14 ,  B64B1/22 ,  B64B1/28 ,  B64B1/30 ,  B64B1/34 ,  B64B1/38 ,  B64B1/58 ,  B64B1/60 ,  B64B1/70 ,  B64B2201/00 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/104

Abstract: A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.

Abstract translation: 一种具有构造成提供静压浮力的封套的混合式垂直起降车辆，附接到信封上的机身，并且具有从其相对侧延伸的至少一对翼片，以产生通过运动的动态提升，以及每个机翼上的推力产生装置， 围绕围绕纵向轴线的侧壁的轴线旋转，以提供垂直起飞或着陆能力。 理想情况下，信封提供负静液压升力以提高低速和地面稳定性。

公开(公告)号：EP2665651A1

公开(公告)日：2013-11-27

申请号：EP11856460.8

申请日：2011-12-30

Applicant: Information Systems Laboratories, Inc.

Inventor： VAN STAAGEN, Peter, K. ,  MCDANIEL, William, Douglas ,  BOSCHMA, James, H., Jr.

IPC: B64F3/00

CPC classification number: B64B1/50 ,  B64B1/58 ,  B64C2201/022 ,  B64C2201/101 ,  B64C2201/123 ,  B64C2201/201 ,  B64C2201/208 ,  B64F1/14

Abstract: A system and method for deploying a payload with an aerostat uses a mobile transporter for moving the system to a deployment site. Structurally, the system includes a base unit with a rotation head mounted thereon. An envelope container for holding a deflated aerostat is mounted on the rotation head and a rotation of the container on the rotation head positions the aerostat for optimal compliance with the existing wind condition. Also included in the system is an inflator that is mounted on the base unit to inflate the aerostat with a Helium gas. And, the system includes a tether control unit for maintaining a connection with the aerostat during its deployment, in-flight use, and recovery. Preferably, a deployment computer is used for a coordinated control of the rotation head, inflator and tether.