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81. 发明申请

WO2016138173A1 METHODS FOR PROVIDING A DURABLE SOLAR POWERED AIRCRAFT WITH A VARIABLE GEOMETRY WING 审中-公开
标题翻译：提供具有可变几何功能的耐用太阳能电动飞机的方法
公开(公告)号：WO2016138173A1
公开(公告)日：2016-09-01
申请号：PCT/US2016/019410
申请日：2016-02-24
申请人： KAREM AIRCRAFT, INC.
发明人： KAREM, Abe , TIGNER, Benjamin
IPC分类号： B64F5/00 , B64C3/38 , B64C13/50 , B64D41/00 , B64D27/24 , B64C11/28 , B64C39/02 , H02S10/40 , H02S40/38
CPC分类号： B64C3/42 , B64C3/16 , B64C11/28 , B64C39/024 , B64C2201/021 , B64C2201/042 , B64C2201/06 , B64C2201/104 , B64C2201/122 , B64C2201/165 , B64D27/24 , B64D2211/00 , B64F5/10 , G05D1/0011 , G05D1/0088 , H02S10/40 , H02S20/30 , H02S40/38 , Y02T50/12 , Y02T50/44 , Y02T50/62
摘要： Methods of manufacturing and operating a solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to rely on free flight control at high altitude and under conventional conditions, thereby providing flight duration in excess of 2 months. The aircraft is particularly suitable for use as part of a telecommunications network.
摘要翻译：描述了制造和操作具有分段翼的太阳能飞行器的方法，其可在飞行期间重新配置以优化太阳能收集。飞机具有刚性结构，耐恶劣天气，并配置为依靠高空和常规条件下的自由飞行控制，从而提供超过2个月的飞行时间。该飞机特别适合用作电信网络的一部分。

82. 发明申请

WO2016138139A1 SOLAR POWERED AIRCRAFT WITH A VARIABLE GEOMETRY WING AND TELECOMMUNICATIONS NETWORKS UTILIZING SUCH AIRCRAFT 审中-公开
标题翻译：具有可变几何形式的太阳能动力飞机和使用这种飞机的电信网络
公开(公告)号：WO2016138139A1
公开(公告)日：2016-09-01
申请号：PCT/US2016/019369
申请日：2016-02-24
申请人： KAREM AIRCRAFT, INC.
发明人： KAREM, Abe , TIGNER, Benjamin
IPC分类号： B64C39/02 , B64C3/38 , B64D27/24 , B64D41/00 , B64C11/28 , B64C13/50 , B64C25/10 , B64D45/00 , H04B7/185 , H02S10/40
CPC分类号： B64C3/52 , B64C3/24 , B64C3/42 , B64C3/546 , B64C11/30 , B64C13/00 , B64C25/10 , B64C39/02 , B64C39/024 , B64C39/04 , B64C39/10 , B64C2201/042 , B64C2201/102 , B64C2201/122 , B64C2201/165 , B64D27/24 , H04B7/18506
摘要： A solar powered aircraft having segmented wings that can be reconfigured during flight to optimize collection of solar energy are described. The aircraft have rigid construction that is resistant to inclement weather and is configured to rely on free flight control at high altitude and under conventional conditions, thereby providing flight duration in excess of 2 months. The aircraft is particularly suitable for use as part of a telecommunications network. A telecommunications network incorporating such aircraft is also discussed.
摘要翻译：描述了具有分段翼的太阳能飞行器，其可以在飞行期间重新配置以优化太阳能的收集。飞机具有刚性结构，耐恶劣天气，并配置为依靠高空和常规条件下的自由飞行控制，从而提供超过2个月的飞行时间。该飞机特别适合用作电信网络的一部分。还讨论了包含这种飞机的电信网络。

83. 发明申请

WO2015175057A2 BROADBAND ACCESS TO MOBILE PLATFORMS USING DRONE/UAV 审中-公开
标题翻译：宽带接入移动平台使用DRONE / UAV
公开(公告)号：WO2015175057A2
公开(公告)日：2015-11-19
申请号：PCT/US2015/016116
申请日：2015-02-17
申请人： UBIQOMM LLC
发明人： JALALI, Ahmad
CPC分类号： H04B7/18504 , B64C39/024 , B64C2201/122 , H04B7/1555 , H04B7/18506 , H04B7/18528 , H04B7/18539 , H04B7/18541 , H04B7/18543 , H04B7/18554 , H04B7/18578 , H04W24/02 , H04W36/0005 , H04W36/0016 , H04W36/0083 , H04W36/12 , H04W36/30 , H04W36/36 , H04W48/16 , H04W84/005 , H04W84/06 , H04W88/16 , Y02D70/00 , Y02D70/1242 , Y02D70/1262 , Y02D70/142 , Y02D70/164 , Y02D70/446
摘要： Systems and methods for providing broadband internet access to mobile platforms such as vehicles, aircraft, and portable devices, using a network of one or more entities such as drones/unmanned aerial vehicles (UAVs). In one embodiment, the drone communication system comprises an antenna sub-system, a radio sub-system and a data switching sub-system. The mobile platforms comprise antenna and radio sub-systems to communicate with the drones, detect changes in the mobile platforms azimuth and elevation changes, and adjust the mobile platform's antenna beam to compensate for the orientation changes to optimally point toward the drones. The exemplary mobile platform further comprises methods to detect the need for handoff to a different drone and to carry out the handoff. A mechanism to improve coverage to mobile platforms that may see obstruction on their path to the drone network is also disclosed, as are apparatus and methods for cost efficiently providing reliable internet access to portable devices.
摘要翻译：使用诸如无人机/无人驾驶飞行器（UAV）的一个或多个实体的网络来向诸如车辆，飞行器和便携式设备的移动平台提供宽带互联网接入的系统和方法。在一个实施例中，无人机通信系统包括天线子系统，无线电子系统和数据交换子系统。移动平台包括与无人机通信的天线和无线电子系统，检测移动平台方位角和高程变化的变化，并调整移动平台的天线波束以补偿朝向无人机的最佳方向变化。该示例性移动平台还包括检测对不同无人机进行切换的需要并执行切换的方法。还公开了一种用于提高可能看到其到无人机网络的路径上的阻碍的移动平台的覆盖的机制，以及用于成本有效地提供对便携式设备的可靠互联网访问的设备和方法。

84. 发明申请

WO2015073687A1 UNMANNED AERIAL VEHICLES FOR WELL MONITORING AND CONTROL 审中-公开
标题翻译：用于监测和控制的无人机动车
公开(公告)号：WO2015073687A1
公开(公告)日：2015-05-21
申请号：PCT/US2014/065479
申请日：2014-11-13
申请人： SCHLUMBERGER CANADA LIMITED , SERVICES PETROLIERS SCHLUMBERGER , SCHLUMBERGER HOLDINGS LIMITED , SCHLUMBERGER TECHNOLOGY B.V. , PRAD RESEARCH AND DEVELOPMENT LIMITED , SCHLUMBERGER TECHNOLOGY CORPORATION
发明人： COSTE, Emmanuel , TAMBOISE, Guillaume Daniel , ANDERSON, Jeffery
IPC分类号： B64C39/02 , E21B44/00
CPC分类号： B64C39/024 , B64C2201/122 , E21B47/0007 , H04B7/18504
摘要： Unmanned aerial vehicles (UAVs) for well monitoring and control are described. Example UAVs include drones, copters, and stationary or mobile airships. An example UAV includes an airborne controller that can retrieve data from a wireless network of a well. The UAV may relay the data to a remote center. In an implementation, the UAV stores the data. In an example, the UAV downloads a flight plan and connects to local WiFi networks of wells along a route. The airborne controller queries and retrieves data from wells and associated gauges, production tools, and monitoring equipment. The airborne controller may perform diagnosis based on retrieved data and autonomously provide well services during flyby or in a modified holding pattern for servicing the well. An onboard servicing engine may adjust equipment, change control settings, diagnose malfunctions, calibrate devices, update software and firmware, and perform a system reboot.
摘要翻译：描述了用于井监测和控制的无人机（UAV）。无人机的例子包括无人机，直升机和固定式或移动式飞艇。无人机的一个例子包括一个可从井的无线网络检索数据的机载控制器。 UAV可以将数据中继到远程中心。在实施中，UAV存储数据。在一个例子中，无人机下载飞行计划并连接到路线上的本地WiFi网络。机载控制器查询和检索井和相关量规，生产工具和监测设备的数据。机载控制器可以基于检索到的数据执行诊断，并且在飞越期间或以改进的保持模式自主地提供良好的服务以维护井。机载服务引擎可以调整设备，更改控制设置，诊断故障，校准设备，更新软件和固件，并执行系统重新启动。

85. 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。

86. 发明申请

WO2014094712A2 HILFSVORRICHTUNG FÜR HOCHFLIEGENDES FLUGZEUG 审中-公开
标题翻译：高飞机辅助装置
公开(公告)号：WO2014094712A2
公开(公告)日：2014-06-26
申请号：PCT/DE2013/000799
申请日：2013-12-18
申请人： ASTRIUM GMBH , EADS DEUTSCHLAND GMBH
发明人： KIEFER, Andreas , FEDERHEN, Jens , DRAGON, Dieter , SCHOLZ, Werner
IPC分类号： B64D5/00
CPC分类号： B64D27/26 , B64C39/024 , B64C2201/042 , B64C2201/082 , B64C2201/122 , B64D5/00 , B64D27/02 , B64D27/24 , B64D41/00 , B64D2211/00 , Y02T50/44 , Y02T50/62
摘要： Die Erfindung beschreibt eine Hilfsvorrichtung (20) für ein hochfliegendes Flugzeug (10). Die Hilfsvorrichtung (20) umfasst einen von dem Flugzeug (10) unabhängigen Antrieb (21) für den Aufstieg des mit der Hilfsvorrichtung (20) lösbar gekoppelten Flugzeugs (10) in die Stratosphäre und ist spätestens beim Erreichen einer vorbestimmten Missionshöhe von dem Flugzeug (10) lösbar.
摘要翻译：本发明描述了用于飞机（10）的辅助装置（20）。包括飞机（10）中的一个辅助设备（20）独立承担依赖性为导航用的驱动器（21）R辅助装置（20）升的上升＆ouml;在平流层BEAR重新释放地联接飞机（10），并且是的sp AUML;测试当从飞机（10）到达预定的任务高度时，可以

87. 发明申请

WO2012095658A1 DATA TRANSFER SYSTEM AND METHOD THEREOF 审中-公开
标题翻译：数据传输系统及其方法
公开(公告)号：WO2012095658A1
公开(公告)日：2012-07-19
申请号：PCT/GB2012/050043
申请日：2012-01-10
申请人： BAE SYSTEMS plc , TEBAY,Andrew, Christopher , STOCKTON,Simon , Graham
发明人： TEBAY,Andrew, Christopher , STOCKTON,Simon , Graham
IPC分类号： G06F3/06 , H04L29/08
CPC分类号： H04L67/10 , B64C2201/122 , B64C2201/123 , G06F3/0601 , G06F3/0605 , G06F3/0658 , G06F3/067 , G06F3/0673 , G06F2003/0697 , H04L67/06 , H04L67/12 , H04L67/125
摘要： A data transfer system is provided for an unmanned vehicle on a mission. The data transfer system comprises a first sensor associated with the unmanned vehicle and which collects a first data set, a second sensor associated with the unmanned vehicle and which collects a second data set, wherein the second data set is associated with the first data set by a predetermined association, and a transceiver for transmitting data from the unmanned vehicle to a remote data storage system. The system further comprises a mass data storage computer that is located on the unmanned vehicle which stores the first and second data sets based on the predetermined association. The mass data storage computer receives and executes requests from the remote data storage system to transmit the first data set from the unmanned vehicle to the remote data storage system. The mass data storage computer further receives and executes requests from the remote data storage system to transmit selected ones of the second data set from the unmanned vehicle to the remote data storage system. Also, the mass data storage computer is removably connectable to the unmanned vehicle such that at the end of the mission the mass data storage computer can be removed from the unmanned vehicle and connected to the remote data storage device to download any data which has not already been transmitted.
摘要翻译：为任务中的无人驾驶车辆提供数据传输系统。数据传输系统包括与无人车相关联并且收集第一数据集的第一传感器，与无人车相关联的第二传感器并且收集第二数据集，其中第二数据集与第一数据集相关联，预定关联，以及用于将数据从无人驾驶车辆发送到远程数据存储系统的收发器。该系统还包括位于无人驾驶车辆上的大容量数据存储计算机，其基于预定的关联来存储第一和第二数据集。大容量数据存储计算机接收并执行来自远程数据存储系统的请求，以将第一数据组从无人驾驶车辆发送到远程数据存储系统。大容量数据存储计算机还接收并执行来自远程数据存储系统的请求，以将来自无人驾驶车辆的第二数据集中的选定的数据传送到远程数据存储系统。此外，大容量数据存储计算机可拆卸地连接到无人驾驶车辆，使得在任务结束时，大容量数据存储计算机可以从无人驾驶车辆移除并连接到远程数据存储设备以下载尚未存在的任何数据被传送

88. 发明申请

WO2012063220A2 AERIAL UNIT AND METHOD FOR ELEVATING PAYLOADS 审中-公开
标题翻译：空运单位和提供付款的方法
公开(公告)号：WO2012063220A2
公开(公告)日：2012-05-18
申请号：PCT/IB2011/055021
申请日：2011-11-10
申请人： SHACHOR, Gabriel , COHEN, Shy , KEIDAR, Ronen , SKY SAPIENCE
发明人： SHACHOR, Gabriel , COHEN, Shy , KEIDAR, Ronen
IPC分类号： B64C27/04
CPC分类号： B64F1/12 , B64C27/04 , B64C27/08 , B64C29/04 , B64C39/022 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/122 , B64C2201/127 , B64C2201/148 , B64F1/007 , B64F1/125
摘要： An aerial unit, a method and a system are provide, the system includes a ground unit; an aerial unit; and a connecting element arranged to connect the ground unit to the aerial unit. The ground unit may include (a) a connecting element manipulator, for altering an effective length of the connecting element. The effective length of the connecting element defines a distance between the ground unit and the aerial unit, (b) a ground unit controller for controlling the connecting element manipulator; and (c) a positioning unit arranged to image the aerial unit and to generate metadata about a location of the aerial unit. The aerial unit may include (i) a first propeller; (ii) a frame; (iii) a first propeller motor that is configured to rotate the first propeller about a first axis. The first propeller motor is connected to the frame; at least one steering element, (iv) An interfacing module for coupling a payload to the aerial unit. At least one of the ground unit and the aerial unit may include a controller that is arranged to control, at least in response to the metadata, at least one of the first propeller motor and the at least one steering element to affect at least one of the location of the aerial unit and the orientation of the aerial unit.
摘要翻译：提供一种天线单元，方法和系统，该系统包括接地单元; 空中单位以及布置成将地面单元连接到天线单元的连接元件。接地单元可以包括（a）连接元件操纵器，用于改变连接元件的有效长度。连接元件的有效长度限定了地面单元与天线单元之间的距离，（b）用于控制连接元件操纵器的地面单元控制器; 以及（c）定位单元，其布置成对所述天线单元进行成像并产生关于所述天线单元的位置的元数据。天线单元可以包括（i）第一螺旋桨; （ii）框架; （iii）构造成绕第一轴线旋转第一螺旋桨的第一螺旋桨马达。第一螺旋桨马达连接到框架; 至少一个转向元件，（iv）用于将有效载荷耦合到天线单元的接口模块。地面单元和天线单元中的至少一个可以包括控制器，其被布置为至少响应于元数据来控制第一螺旋桨马达和至少一个操纵元件中的至少一个，以影响至少一个天线单元的位置和天线单元的方向。

89. 发明申请

WO2011117619A3 AERIAL VEHICLE AND METHOD OF FLIGHT 审中-公开
标题翻译：空中客车和飞行方法
公开(公告)号：WO2011117619A3
公开(公告)日：2011-11-17
申请号：PCT/GB2011050562
申请日：2011-03-22
申请人： ATHENE WORKS LTD , DEAKIN NICHOLAS JAMES
发明人： DEAKIN NICHOLAS JAMES
IPC分类号： B64B1/00
CPC分类号： B64B1/02 , B64B1/08 , B64B1/10 , B64B1/12 , B64B1/14 , B64B1/20 , B64B1/38 , B64B1/64 , B64B2201/00 , B64C2201/042 , B64C2201/044 , B64C2201/048 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/165 , B64C2201/167 , H01Q1/36 , H01Q9/27
摘要： An aerial vehicle is described which comprises: a first compartment (13) for holding a lighter than air gas; a second compartment (6, 4) for holding atmospheric air and having an inlet and an outlet; a solar panel (41) for converting sunlight into electricity; a compressor (242) for pumping atmospheric air through the inlet into the second compartment; control means (1,3) for controlling the pitch and yaw of the vehicle; and a controller (209) for controlling the buoyancy of the vehicle via the compressor and the outlet such that the vehicle is either lighter than the surrounding air and rising or heavier than the surrounding air and falling, and for controlling the control means such that the rising and falling motion includes a horizontal component. In another embodiment the solar panel is replaced by an engine and a fuel tank for storing fuel for the engine is also provided. The aerial vehicle can remain airborne for extended periods by using buoyancy propulsion. In the embodiments including a solar panel, a system including a light transmission station may be provided to supply energy to the solar panel from the light transmission station rather than relying on the incident sunlight alone. A method of flight using buoyancy propulsion is also described.
摘要翻译：描述了一种飞行器，其包括：用于保持比气体气体轻的第一隔室（13）; 用于保持大气空气并具有入口和出口的第二隔间（6,4）; 用于将太阳光转换成电的太阳能电池板（41）压缩机（242），用于将大气通过所述入口排入所述第二隔室; 控制装置（1,3），用于控制车辆的俯仰和偏航; 以及用于经由压缩机和出口控制车辆的浮力的控制器（209），使得车辆比周围空气要轻，并且比周围空气上升或者重，并且为了控制控制装置，上升和下降运动包括水平分量。在另一个实施例中，太阳能电池板被发动机代替，并且还提供了用于储存用于发动机的燃料的燃料箱。航空器可以通过使用浮力推进长时间保持空中。在包括太阳能电池板的实施例中，可以提供包括光传输站的系统，以从光传输站向太阳能电池板提供能量，而不是仅依赖于入射的太阳光。还描述了使用浮力推进的飞行方法。

90. 发明申请

WO2004000642A1 AIRSHIP AND METHOD OF OPERATION 审中-公开
标题翻译：航空和操作方法
公开(公告)号：WO2004000642A1
公开(公告)日：2003-12-31
申请号：PCT/CA2003/000945
申请日：2003-06-25
申请人： 21ST CENTURY AIRSHIPS INC. , COLTING, Hokan
发明人： COLTING, Hokan
IPC分类号： B64B1/00
CPC分类号： B64B1/34 , B64B1/02 , B64B1/32 , B64C21/02 , B64C39/024 , B64C2201/022 , B64C2201/042 , B64C2201/044 , B64C2201/101 , B64C2201/122 , B64C2201/127 , B64C2201/146 , B64C2201/165 , Y02T50/166
摘要： An airship (20) has a generally spherical shape and has an internal envelope (24) for containing a lifting gas such as Helium or Hydrogen. The airship has a propulsion and control system (36, 38) that permits it to be flown to a desired loitering location, and to be maintained in that location for a period of time. In one embodiment the airship may achieve neutral buoyancy when the internal envelope is as little as 7 % full of lifting gas, and may have a service ceiling of about 60,000 ft. The airship has an equipment module (180) that can include either communications equipment, or monitoring equipment, or both. The airship can be remotely controlled from a ground station. The airship has a solar cell array and electric motors (44, 46) of the propulsion and control system are driven by power obtained from the array. The airship also has an auxiliary power unit (52) that can be used to drive the electric motors. The airship can have a pusher propeller that assists in driving the airship and also moves the point of flow separation of the spherical airship further aft. In one embodiment the airship can be refuelled at altitude to permit extended loitering.
摘要翻译：飞艇（20）具有大致球形并且具有用于容纳诸如氦气或氢气的提升气体的内部封壳（24）。飞艇有一个推进和控制系统（36,38），允许飞行到期望的游荡地点，并在该地点保持一段时间。在一个实施例中，当内部信封充满提升气体的7％时，飞艇可以实现中性浮力，并且可以具有约6万英尺的服务天花板。飞艇具有可以包括通信设备，或监控设备，或两者兼而有之。飞艇可以从地面站遥控。飞艇具有太阳能电池阵列，推进和控制系统的电机（44,46）由阵列获得的功率驱动。飞艇还具有可用于驱动电动机的辅助动力单元（52）。飞艇可以有一个推动螺旋桨，有助于驾驶飞艇，还可以使球形飞艇进一步向后流动。在一个实施例中，飞艇可以在高度加油以允许延长的游荡。

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