专利快速检索-快速检索全球专利，免费商用专利数据库-IPRDB

21. 发明申请

WO2014080387A8 RESCUE DRONE 审中-公开
标题翻译：救援无效
公开(公告)号：WO2014080387A8
公开(公告)日：2014-06-19
申请号：PCT/IB2014000416
申请日：2014-03-25
申请人： ALSHDAIFAT WASFI , ALMUHAIRBI EIDA , KASSAB FARAH AFIF
发明人： ALSHDAIFAT WASFI , ALMUHAIRBI EIDA , KASSAB FARAH AFIF
IPC分类号： B64C27/08
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/12 , B64C2201/182 , B64C2201/206
摘要： To provide a rescue drone (20), for rescuing an idle drone (21), it consists of an adjustable length hook (22) to engage with the idle drone, to carry it away, an L- shaped metallic tool (27) to push the idle drone away from the middle of the road, or to help in repositioning it to be at a side that permits for the hook (22) to engage with it, an emergency light (SOS) (28), to assist while hovering over the idle drone located in a road, an electric shock stick (29), which is to be used against any person approaching the idle drone to steal it, a speaker (30) and camera (31), to assist a security person in a command center to assess the case, talk with and warn any person who is trying to steal the idle drone, or to advise and guide a volunteer who is trying to help and assist in rescuing the idle drone.
摘要翻译：为了提供救援无人驾驶飞机（20）的救援无人机（20），该无人驾驶飞机由可调节长度的挂钩（22）组成，以与无人驾驶飞机相接合，将L型金属工具（27）将无人驾驶飞机从道路中间推出，或帮助将其重新定位在允许挂钩（22）与其接合的一侧，应急灯（SOS）（28），以便在悬停时协助在位于道路上的空闲无人驾驶飞机上安装用于抵抗任何靠近空闲无人机以窃取它的人的电击棒（29），扬声器（30）和照相机（31），以协助安全人员指挥中心对案件进行评估，与任何试图偷走无人驾驶飞机的人进行交谈并发出警告，或者建议并指导正在尝试帮助并协助拯救无人驾驶飞机的志愿者。

22. 发明申请

WO2014080387A2 RESCUE DRONE 审中-公开
标题翻译：救护车
公开(公告)号：WO2014080387A2
公开(公告)日：2014-05-30
申请号：PCT/IB2014/000416
申请日：2014-03-25
申请人： ALSHDAIFAT, Wasfi , ALMUHAIRBI, Eida , KASSAB, Farah, Afif
发明人： ALMUHAIRBI, Eida , KASSAB, Farah, Afif
IPC分类号： B64C27/08
CPC分类号： B64C39/024 , B64C2201/027 , B64C2201/12 , B64C2201/182 , B64C2201/206
摘要： To provide a rescue drone (20), for rescuing an idle drone (21), it consists of an adjustable length hook (22) to engage with the idle drone, to carry it away, an L- shaped metallic tool (27) to push the idle drone away from the middle of the road, or to help in repositioning it to be at a side that permits for the hook (22) to engage with it, an emergency light (SOS) (28), to assist while hovering over the idle drone located in a road, an electric shock stick (29), which is to be used against any person approaching the idle drone to steal it, a speaker (30) and camera (31), to assist a security person in a command center to assess the case, talk with and warn any person who is trying to steal the idle drone, or to advise and guide a volunteer who is trying to help and assist in rescuing the idle drone.
摘要翻译：为了提供救援无人机（20），用于拯救闲置的无人机（21），它由可调节的长度的钩（22）组成，与空闲无人机接合以将其携带，将L形金属工具（27）将闲置的无人驾驶从道路中间推开，或帮助将其重新定位在允许钩子（22）与其接合的一侧，应急灯（SOS）（28），以在盘旋时协助在位于道路中的空闲无人机之外，一个电击棒（29），用于抵抗任何接近空闲无人机的人窃取它，扬声器（30）和照相机（31），以帮助安全人员指挥中心评估案件，与任何试图窃取闲置无人驾驶飞机的人进行交谈，并提出警告，并指导和指导正在协助救援闲置无人机的志愿者。

23. 发明申请

WO2008085536A3 DUAL-USE MODULAR PROPULSION SURVEILLANCE VEHICLE WITH DETACHABLE UNMANNED AIRBORNE VEHICLES 审中-公开
标题翻译：双用途模拟推进监控车辆与可拆卸的无人驾驶飞机
公开(公告)号：WO2008085536A3
公开(公告)日：2008-10-02
申请号：PCT/US2007069569
申请日：2007-05-23
申请人： AVID LLC , WILSON SAMUEL B , GELHAUSEN PAUL , TURNBULL ANDY , ROBERTS MICHAEL , GUERERRO IGNACIO , BECKER KIM
发明人： WILSON SAMUEL B , GELHAUSEN PAUL , TURNBULL ANDY , ROBERTS MICHAEL , GUERERRO IGNACIO , BECKER KIM
IPC分类号： F41G7/00 , F41H13/00
CPC分类号： B64C39/024 , B64C2201/028 , B64C2201/162 , B64C2201/206 , B64D5/00
摘要： The present invention provides a system for reconnaissance using autonomous unmanned airborne vehicles (UAV). The system comprises a mothership, which is generally a fixed wing fuel tank capable of providing a suitable surface for flight (lift) and one or more elements for attachment of individual UAVs. The system further comprises one or more UAVs that are detachably connected to the mothership, and which are independently controllable for reconnaissance and tracking. The system and its individual parts are reusable and independently controllable, permitting low cost reconnaissance over wide areas of geography.
摘要翻译：本发明提供一种使用自主无人驾驶飞行器（UAV）进行侦察的系统。该系统包括母舰，其通常是能够为飞行（提升）提供合适的表面的固定翼燃料箱和用于附接各个无人机的一个或多个元件。该系统还包括一个或多个UAV，其可拆卸地连接到母舰，并且可独立控制以用于侦察和跟踪。该系统及其各个部件是可重复使用的并且可独立控制，允许在广泛的地理区域进行低成本侦察。

24. 发明申请

WO2018236448A2 PRECISION DELIVERY VEHICLE 审中-公开
公开(公告)号：WO2018236448A2
公开(公告)日：2018-12-27
申请号：PCT/US2018/024768
申请日：2018-03-28
申请人： SKYWORKS GLOBAL INC.
发明人： GROEN, David
CPC分类号： B64D1/12 , B64C3/56 , B64C29/02 , B64C39/024 , B64C2201/102 , B64C2201/108 , B64C2201/128 , B64C2201/206 , B64D17/80
摘要： A precision delivery vehicle having a vehicle body assembly, a fixed wing system, a rotor system and a guidance system. The vehicle body assembly can retain a payload. The fixed wing system includes first and second wings coupled to the vehicle body for fixed wing flight. The rotor system includes a mast structure, a rotor hub rotatable about the mast structure and at least two rotor blades coupled to the rotor hub and rotatable with the rotor hub relative to the mast structure. The at least two rotor blades are movable between a collapsed configuration and a deployed configuration. In the collapsed configuration, the precision delivery vehicle is in fixed wing flight. Upon placement of the at least two rotor blades into the deployed configuration, the precision delivery vehicle is placed into rotative flight. The guidance system is structurally configured to direct the precision delivery vehicle to a target

25. 发明申请

WO2018063630A1 DRONE-CARRIER BROKERING 审中-公开
标题翻译： DRONE-CARRIER经纪人
公开(公告)号：WO2018063630A1
公开(公告)日：2018-04-05
申请号：PCT/US2017/048814
申请日：2017-08-28
申请人： INTEL CORPORATION
发明人： HUNT, Simon , SRIVASTAVA, Neeta
IPC分类号： G05D1/00 , B64C39/02 , G06Q10/08 , G06Q50/28
CPC分类号： B64C39/024 , B64C2201/128 , B64C2201/14 , B64C2201/205 , B64C2201/206 , B64C2201/208 , G06Q10/0835
摘要： In an example, there is disclosed a drone operator computing apparatus having : a network interface; and one or more logic elements providing a broker agent to: communicatively couple to a drone brokerage engine via the network interface; send a carrier request comprising a request for a carrier to carry a drone through a prohibitive zone; receive a brokered carrier response comprising an engage point; and dispatch the drone to the engage point. There is also disclosed a drone having a navigation engine to proceed to the engage point and engage a carrier. There is also disclosed a brokerage engine to broker a carrier request from the drone operator, receive a carrier response from a carrier operator, and broker the carrier response.
摘要翻译：在一个示例中，公开了一种无人驾驶飞机运营商计算设备，其具有：网络接口; 以及一个或多个逻辑元件，提供经纪人代理以：通过网络接口通信地耦合到无人驾驶经纪人引擎; 发送载体请求，该载体请求包括通过禁止区携带无人机的载体的请求; 接收包括参与点的代理的运营商响应; 并将无人机派送到接合点。还公开了一种无人驾驶飞机，其具有导航引擎以进入接合点并接合载体。另外还披露了一个经纪引擎，用于代理来自无人机运营商的运营商请求，接收运营商运营商的运营商回应，以及代理运营商回应。

26. 发明申请

WO2017139255A1 GAS-FILLED CARRIER AIRCRAFTS AND METHODS OF DISPERSING UNMANNED AIRCRAFT SYSTEMS IN DELIVERING PRODUCTS 审中-公开
标题翻译：气体填充载体飞机和分散无人机系统以提供产品的方法
公开(公告)号：WO2017139255A1
公开(公告)日：2017-08-17
申请号：PCT/US2017/016801
申请日：2017-02-07
申请人： WAL-MART STORES, INC.
发明人： HIGH, Donald R. , COX, David C.
IPC分类号： B64D1/10 , B64C39/02 , B64D1/00 , B64D1/02 , B64D1/08 , B64D1/12
CPC分类号： B64B1/02 , B64C39/024 , B64C2201/082 , B64C2201/128 , B64C2201/146 , B64C2201/206 , B64D5/00 , G05D1/0027 , G06Q10/0833 , G08G5/0034 , G08G5/0069
摘要： In some embodiments, apparatuses and methods are provided herein useful to transport unmanned aircraft systems to delivery products. In some embodiments, gas-filled aerial transport and launch system, comprises: a transport aircraft comprising: a gas chamber; and a carrier compartment where the gas chamber induces a lifting force on the carrier compartment; at least one propulsion system; and a navigation control system that controls the direction of travel of the transport aircraft; wherein the carrier compartment comprises: an unmanned aircraft system (UAS) storage area configured to receive multiple UASs; and an UAS launching bay that enables the UAS to be launched while the transport aircraft is in flight and while the UAS is carrying a package to be delivered.
摘要翻译：在一些实施例中，本文提供的设备和方法可用于将无人驾驶飞机系统运送到运送产品。在一些实施例中，充气式空中运输和发射系统包括：运输飞机，其包括：气室; 以及载气室，气体室在载体室上引起提升力; 至少一个推进系统; 以及控制运输机的行进方向的导航控制系统; 其中所述载体隔室包括：无人驾驶飞机系统（UAS）存储区域，其被配置为接收多个UAS; 和一个无人机系统发射舱，使无人机系统可以在运输飞机在飞行期间启动，而无人机系统正在运送包裹以供交付。

27. 发明申请

WO2017131823A2 SPACE COMBAT DRONE 审中-公开
标题翻译：空间战斗无人机
公开(公告)号：WO2017131823A2
公开(公告)日：2017-08-03
申请号：PCT/US2016/052091
申请日：2016-09-16
申请人： WILKINSON, Christopher
发明人： WILKINSON, Christopher
IPC分类号： B64C13/24 , A63H30/04
CPC分类号： B64C39/024 , B64C2201/02 , B64C2201/046 , B64C2201/082 , B64C2201/121 , B64C2201/123 , B64C2201/206 , B64C2201/22
摘要： An unmanned aerial combat vehicle system is disclosed. The system provides for an unmanned aerial combat vehicle that is capable of performing reconnaissance, disrupting enemy communications, or delivering a weaponized payload. The unmanned aerial combat vehicle may also be equipped with a cloaking mechanism, where it can mask it' s heat signature, or simulate an image on its outer surface.
摘要翻译：公开了一种无人空中作战车辆系统。该系统提供了一种无人驾驶的空中作战车辆，能够执行侦察，破坏敌方通信或发射武器化的有效载荷。无人驾驶飞行器也可以配备隐形装置，它可以掩盖它的热特征，或者在其外表面模拟图像。

28. 发明申请

WO2017049183A1 STOWABLE UNMANNED AERIAL VEHICLES AND ASSOCIATED SYSTEMS AND METHODS 审中-公开
标题翻译：可持续的无人驾驶飞机和相关系统和方法
公开(公告)号：WO2017049183A1
公开(公告)日：2017-03-23
申请号：PCT/US2016/052282
申请日：2016-09-16
申请人： NIXIE LABS, INC. , KOHSTALL, Christoph , JOVANOVIC, Jelena , OWENS, Dylan , LEEFER, Nathan , SAMPSON, Ben
发明人： KOHSTALL, Christoph , JOVANOVIC, Jelena , OWENS, Dylan , LEEFER, Nathan , SAMPSON, Ben
IPC分类号： B64C39/02 , B64C27/08 , B64C27/12 , B64C27/20 , B64D47/08
CPC分类号： B64C39/024 , B64C1/063 , B64C1/30 , B64C27/20 , B64C2201/027 , B64C2201/042 , B64C2201/108 , B64C2201/127 , B64C2201/20 , B64C2201/203 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64D47/08 , B64F5/10
摘要： Stowable and deployable unmanned aerial vehicles (UAVs), and associated systems and methods are disclosed. A UAV in accordance with a particular embodiment includes a main body, frames carried by the main body, and motors carried by the frames. At least two frames are positioned to move relative to each other between a stowed configuration in which the frames are generally aligned proximate to each other and a deployed configuration different from the stowed configuration. The main body can include a first body portion pivotably connected to a second body portion. In a stowed configuration, the body portions can generally overlap each other. A UAV in accordance with particular embodiments includes a modular electronics unit carried by the UAV and including a camera, a battery, and a vehicle controller. Modular electronics units can be configured to be removably connected to and disconnected from the UAV and other vehicles.
摘要翻译：公开了可以存放和部署的无人机（UAV）以及相关的系统和方法。根据特定实施例的UAV包括主体，由主体承载的框架和由框架承载的电动机。至少两个框架被定位成在收起的构型之间相对于彼此移动，其中框架通常彼此靠近对准，并且展开配置与收起的构造不同。主体可以包括可枢转地连接到第二主体部分的第一主体部分。在收起的构造中，主体部分通常可以彼此重叠。根据特定实施例的无人机包括由UAV携带并包括照相机，电池和车辆控制器的模块化电子单元。模块化电子单元可以配置为可拆卸地连接到UAV和其他车辆并与其断开连接。

29. 发明申请

WO2015051436A1 COMBINATION OF UNMANNED AERIAL VEHICLES AND THE METHOD AND SYSTEM TO ENGAGE IN MULTIPLE APPLICATIONS 审中-公开
标题翻译：无人驾驶航空器的组合以及多种应用中的方法和系统
公开(公告)号：WO2015051436A1
公开(公告)日：2015-04-16
申请号：PCT/CA2013/000941
申请日：2013-11-08
申请人： DE SILVA. SHELTON GAMINI
发明人： DE SILVA. SHELTON GAMINI
IPC分类号： B64D5/00 , B64C1/20 , B64C27/26 , B64C39/00
CPC分类号： B64D5/00 , B64C39/024 , B64C2201/021 , B64C2201/024 , B64C2201/082 , B64C2201/122 , B64C2201/126 , B64C2201/143 , B64C2201/145 , B64C2201/206 , B64D47/08 , G05D1/0011 , G05D1/104
摘要： This invention relates to an Unmanned Aerial Vehicle hereinafter called "Mother UAV" member (11) capable of carrying modules of Sub Unmanned Aerial Vehicle members (12) hereinafter called "Sub UAV" member. More particularly, the method and system that is capable of communicating via satellite and remote control technology wherein ejecting said Sub UAV members (12) from the Mother UAV member (11) wherein Sub UAV members (12) autonomously fly in sequence in a coordinated manner with the Mother UAV member (11), and capable of engaging in multiple missions in high, medium, low altitude, and surface, also communication with under sea submarines (27). Further, comprises of a method and system that the Sub UAV members (12) are able to return back to the Mother UAV member (11) after the mission is completed and be firmly secured to the flatbed (14) of the Mother UAV member (11). The present invention is specifically designed for multifunctional and multipurpose applications where humans and other vehicles are unable to access, for civil, commercial and military purposes.
摘要翻译：本发明涉及以下称为“无人机UAV”的无人飞行器，其能够携带以下称为“副无人机”（Sub UAV）成员的子无人机组件（12）的模块。更具体地，能够通过卫星和遥控技术进行通信的方法和系统，其中从UA无人机组成员（11）弹出所述副无人机部件（12），其中副无人机部件（12）以协调的方式自主地飞行与无人机无人机（11）成员（11），能够从事高，中，低空和地面的多个任务，并与海底潜艇（27）进行通信。此外，还包括一个方法和系统，子任务机构（12）能够在任务完成之后返回到无人机（UA）成员（11），并牢固地固定在无人机（UAV）成员的平板（14）上 11）。本发明专为多功能和多用途应用而设计，人类和其他车辆无法进入民用，商业和军事目的。

30. 发明申请

WO2015034557A1 AIR-LAUNCHABLE CONTAINER FOR DEPLOYING AIR VEHICLE 审中-公开
标题翻译：用于空运车辆的空运集装箱
公开(公告)号：WO2015034557A1
公开(公告)日：2015-03-12
申请号：PCT/US2014/035653
申请日：2014-04-28
申请人： RAYTHEON COMPANY
发明人： ELKINS, Erick, W. , MURPHY, Matthew, G. , THOMAS, Scott, D.
IPC分类号： B64C39/02
CPC分类号： B64D1/12 , B64C39/024 , B64C2201/021 , B64C2201/082 , B64C2201/102 , B64C2201/201 , B64C2201/206
摘要： A container 14 is used to launch a small aircraft 20, such as an unmanned aerial vehicle (UAV), from a host aircraft 100. The container protects the UAV from stresses during the initial ejection from a launcher 30 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 62, 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.
摘要翻译：容器14用于从主机100发射诸如无人驾驶飞行器（UAV）的小型飞机20.容器保护UAV在从作为主机的一部分的发射器30的初始喷射期间免受应力。初始应力可能是由于主机飞机附近的湍流，高空速和/或可能由主飞机从高空速下移动而导致的翻滚造成的。在将UAV从容器部署之前，容器可以部署拖动装置62，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数据，例如全球定位系统（GPS）数据，以允许UAV“启动”，使得能够立即启动任务。

你已经成功收藏专利！

检索式保存成功!

IPRDB

热门服务

关于我们

友情链接

联系方式