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61.发明专利Launch and capture system for vertical take-off and landing (vtol) vehicle 审中-公开垂直起落架（垂直起落架）车辆起升和收获系统
公开(公告)号：JP2009227270A
公开(公告)日：2009-10-08
申请号：JP2009042259
申请日：2009-02-25
Applicant: Honeywell Internatl Inc , ハネウェル・インターナショナル・インコーポレーテッド
Inventor： GOOSSEN EMRAY R , SHEORAN YOGENDRA Y
CPC classification number: B64C39/024 , B64C2201/027 , B64C2201/088 , B64C2201/182 , B64C2201/201 , B64C2201/205 , B64C2201/208 , B64F1/04
Abstract: PROBLEM TO BE SOLVED: To provide a system for launching and capturing a vertical take-off and landing vehicle (VTOL). SOLUTION: A VTOL vehicle 101 comprises a thruster 104 and a duct 106 structured to direct air flow generated by the thruster, and this system 102 includes a capture plate 120 and an extension 122. The capture plate is structured to alter the air flow and generate the force for attracting the duct to the capture plate. The extension is coupled to the capture plate, and is structured to, at least, facilitate holding the VTOL vehicle against the capture plate. COPYRIGHT: (C)2010,JPO&INPIT
Abstract translation: 要解决的问题：提供一种用于发射和捕获垂直起飞和着陆车辆（VTOL）的系统。 解决方案：垂直起落架车辆101包括推进器104和构造成引导由推进器产生的空气流的管道106，并且该系统102包括捕获板120和延伸部122.捕获板被构造成改变空气 流动并产生用于将管道吸引到捕获板的力。 延伸部联接到捕获板，并且被构造成至少有利于将VTOL车辆保持抵靠捕获板。 版权所有（C）2010，JPO＆INPIT
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公开(公告)号：EP3408178A1
公开(公告)日：2018-12-05
申请号：EP16887827.0
申请日：2016-05-19
Applicant: Airobotics Ltd.
Inventor： KRAUSS, Ran , KLINER, Meir
IPC: B64F1/02
CPC classification number: B64F1/00 , B64C39/024 , B64C2201/066 , B64C2201/182 , B64C2201/201 , B64F1/02 , B64F1/12 , B64F1/18 , G05D1/0676
Abstract: A system for homing and recharging an unmanned vehicle comprises a plurality of homing layers operative along the radius of an imaginary circle that has the homing target at its center, each homing layer consisting of a sub-system provided with location means of increasing accuracy relative to that of a sub-system that operates along said radius farther away, from the center of said circle.
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公开(公告)号：EP3133019B1
公开(公告)日：2018-12-05
申请号：EP16179915.0
申请日：2010-09-09
Applicant: AeroVironment, Inc.
Inventor： Miralles, Carlos Thomas , Andryukov, Alexander , Su, Guan H. , McNeil, John
CPC classification number: B64F1/04 , B64C39/024 , B64C2201/08 , B64C2201/102 , B64C2201/146 , B64C2201/201 , B64F1/06 , F41A21/02 , F41F1/00 , F41F3/042 , F42B39/14
Abstract: 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).
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公开(公告)号：EP3124381B1
公开(公告)日：2018-10-24
申请号：EP16190021.2
申请日：2014-12-11
Applicant: Korea Aerospace Research Institute
Inventor： LEE, Sang-Cherl , KIM, Hae-Dong , GONG, Hyeon-Cheol , CHOI, Gi-Hyuk , HWANG, In-Hee , SUK, Byong-Suk
CPC classification number: B60L11/1824 , B60L2200/10 , B60L2230/10 , B64C39/024 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/182 , B64C2201/201 , B64D45/08 , B64F1/00 , B64F1/005 , B64F1/12 , B64F1/222 , F21S8/086 , F21V33/00 , F21W2131/103 , F21Y2115/10
Abstract: An apparatus and method for containing and charging an unmanned VTOL aircraft are disclosed. The apparatus for containing and charging an unmanned VTOL aircraft includes a post 110, an extended member 120, a cover 130, a fastening unit 140, and a charging unit 150. The post is placed on a ground. The extended member is connected to the post. The cover is provided on the extended member, and is configured to be opened or closed in order to contain and protect the unmanned VTOL aircraft. The fastening unit is provided in the cover, and is configured to fasten the unmanned VTOL aircraft. The charging unit is provided in the fastening unit, and is configured to charge the unmanned VTOL aircraft.
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公开(公告)号：EP3130535B1
公开(公告)日：2018-04-18
申请号：EP16157916.4
申请日：2016-02-29
Applicant: Wirth Research Limited
Inventor： WIRTH, Nicholas
CPC classification number: B64C3/56 , B64C3/16 , B64C39/024 , B64C2201/021 , B64C2201/102 , B64C2201/141 , B64C2201/146 , B64C2201/201
Abstract: An unmanned aerial vehicle 2 comprising: a fuselage 4; and a wing 6 comprising a central wing section 12 pivotably mounted to the fuselage 4 and a pair of outer wing sections 14a, 14b pivotably mounted to the central wing section 12; wherein the wing 6 has a folded configuration in which the central wing section 12 and the outer wing sections 14a, 14b are stacked on top of one another and are aligned with a longitudinal axis of the fuselage 4; and a deployed configuration in which the central wing section 12 is substantially perpendicular to the fuselage 4 and the outer wing sections 14a, 14b extend from the central wing section 12 away from the fuselage 4.
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Patent Agency Ranking
公开(公告)号：EP3253654A1
公开(公告)日：2017-12-13
申请号：EP16746225.8
申请日：2016-01-28
Applicant: Airobotics Ltd.
Inventor： KRAUSS, Ran , KLINER, Meir
CPC classification number: B64F1/00 , B64C39/024 , B64C2201/066 , B64C2201/182 , B64C2201/201 , B64F1/02 , B64F1/12 , B64F1/18 , G05D1/102
Abstract: A system for homing and recharging an unmanned vehicle comprises a plurality of homing layers operative along the radius of an imaginary circle that has the homing target at its center, each homing layer consisting of a sub-system provided with location means of increasing accuracy relative to that of a sub-system that operates along said radius farther away, from the center of said circle.
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67.发明公开DISPOSITIF DE RECEPTION D'UN DRONE ET SYSTEME DE REPARTITION DE DRONES ASSOCIE 审中-公开用于接收无声和相关的DRONES分配系统的设备
公开(公告)号：EP3241747A1
公开(公告)日：2017-11-08
申请号：EP17168913.6
申请日：2017-05-02
Applicant: Drone Hive
Inventor： GRAVE, Romain , MICHELETTI, Matthieu
CPC classification number: B64C39/024 , B64C2201/182 , B64C2201/201 , B64F1/007
Abstract: L'invention concerne un dispositif de réception (10a) d'un drone (12) comportant :
- une enceinte (11a) ; et
- un bras comportant une première extrémité fixée à ladite enceinte et une seconde extrémité munie de moyens de réception de drones;
- ledit bras étant mobile entre deux positions :
∘ une position dépliée dans laquelle lesdits moyens de réception s'étendent à l'extérieur de ladite enceinte; et
∘ une position repliée dans laquelle lesdits moyens de réception sont contenus à l'intérieur de ladite enceinte;
- lesdits moyens de réception comportant un berceau formé par une base aux bords de laquelle s'élèvent au moins deux surfaces de guidage en regard l'une de l'autre, lesdites au moins deux surfaces de guidage s'étendant vers l'extérieur avec un angle supérieur à 90° entre ladite base et lesdites au moins deux surfaces de guidage de sorte à guider un drone vers ladite base.Abstract translation: 本发明涉及一种用于接收无人机（12）的装置（10a），包括： - 外壳（11a）; 以及臂，其包括固定到所述外壳的第一端和设有用于接收无人驾驶飞机的装置的第二端; 所述臂可在两个位置之间移动：在所述展开位置，所述接收装置延伸到所述外壳之外; 和∘折叠位置，其中所述接收装置包含在所述外壳内; 所述接收装置包括由基座形成的支架，所述支架的边缘处至少两个引导表面彼此面对地升高，所述至少两个引导表面向外延伸 在所述基座和所述至少两个导向表面之间大于90°的角度，以便将无人机引向所述基座。
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公开(公告)号：EP3055203B1
公开(公告)日：2017-05-10
申请号：EP15703674.0
申请日：2015-01-22
Applicant: Northrop Grumman Systems Corporation
Inventor： TORRE, Christopher N.
CPC classification number: B64C3/56 , B64C1/30 , B64C39/02 , B64C39/024 , B64C2201/102 , B64C2201/201
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69.发明公开SYSTEMS AND DEVICES FOR REMOTELY OPERATED UNMANNED AERIAL VEHICLE REPORT-SUPPRESSING LAUNCHER WITH PORTABLE RF TRANSPARENT LAUNCH TUBE 审中-公开用于远程操作的无人机空中车辆报告的系统和装置 - 具有便携式射频透明发射管的压载式发射机
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
Applicant: AeroVironment, Inc.
Inventor： Miralles, Carlos Thomas , Andryukov, Alexander , Su, Guan H. , McNeil, John
CPC classification number: B64F1/04 , B64C39/024 , B64C2201/08 , B64C2201/102 , B64C2201/146 , B64C2201/201 , B64F1/06 , F41A21/02 , F41F1/00 , F41F3/042 , F42B39/14
Abstract: 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).
Abstract translation: 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。
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70.发明公开AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE 审中-公开AUS DER LUFT ABWERFBARERBEHÄLTERZUM EINSATZ EINES LUFTFAHRZEUGS
公开(公告)号：EP3041739A1
公开(公告)日：2016-07-13
申请号：EP14799061.8
申请日：2014-04-28
Applicant: Raytheon Company
Inventor： ELKINS, Erick W. , MURPHY, Matthew G. , THOMAS, Scott D.
IPC: B64C39/02
CPC classification number: B64D1/12 , B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/102 , B64C2201/201 , B64C2201/206
Abstract: A container is used to launch a small aircraft, such as an unmanned aerial vehicle (UAV), from a host aircraft. The container protects the UAV from stresses during the initial ejection from a launcher that is part of the host aircraft. The initial stresses may be due to turbulence in the vicinity of the host aircraft, high airspeed, and/or tumbling that may result from the ejection from the host aircraft moving at a high airspeed. The container may deploy a drag device, such as a drogue chute, to slow the container down and reorient the container, prior to deployment of the UAV from the container. During the time between ejection from the host aircraft and deployment from the container, the UAV may be powered up and acquire data, such as global positioning system (GPS) data, to allow the UAV a “hot start” enabling immediate mission commencement.
Abstract translation: 一个集装箱用于从一架主机上发射一架小型飞机，如无人飞行器（UAV）。 在从作为主机的一部分的发射器的初始弹出期间，该容器保护无人机免受应力。 初始应力可能是由于主飞机附近的湍流，高空速和/或可能由主飞机在高空速下移动而导致的翻滚造成的。 在从容器部署UAV之前，容器可以部署拖动装置，例如锥形滑槽，以使容器向下减速并重新定向容器。 在从主机飞行器和从集装箱部署之间的时间期间，UAV可以被加电并且获取诸如全球定位系统（GPS）数据的数据，以允许UAV“启动”，从而立即启动任务。
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