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公开(公告)号：WO2017040956A1
公开(公告)日：2017-03-09
申请号：PCT/US2016/050144
申请日：2016-09-02
Applicant: LOCKHEED MARTIN CORPORATION
Inventor： SYLVIA, Russell, M.
CPC classification number: B64F1/04 , B63G8/28 , B63G2008/008 , B64C39/024 , B64C2201/08 , B64C2201/088 , B64C2201/20 , B64C2201/201 , B64C2201/205
Abstract: A payload launch system that uses an inflatable air bag ram to launch a payload, such as an unmanned aerial vehicle, from a launch chamber of a launch tube. The air bag ram seals with the interior surface of the launch tube to isolate a dump valve that controls the flow of compressed gas from a gas storage chamber into the air bag ram. The air bag ram sealing with the interior surface of the launch tube isolates the dump valve, both pre-launch and post-launch, from any water or debris carried in with water in which the payload launch system is disposed
Abstract translation: 一种有效载荷发射系统，其使用可充气气囊压头从发射管的发射室发射有效载荷，例如无人驾驶飞行器。 气囊柱塞与发射管的内表面密封，以隔离一个排气阀，其将压缩气体从气体储存室流入气囊冲头。 与发射管的内表面密封的气囊柱塞将排放阀，预发射和发射后的任何水分或污染物与运载有有效载荷发射系统的水一起分离
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公开(公告)号：WO2016204843A2
公开(公告)日：2016-12-22
申请号：PCT/US2016/024347
申请日：2016-03-25
Applicant: PLANCK AEROSYSTEMS, INC.
Inventor： TWINING, David Merrick , WELLS, Joshua
CPC classification number: G05D1/0684 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/141 , B64C2201/18 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64D45/00 , B64D45/04 , B64F1/12 , G01C21/20 , G05D1/0669
Abstract: Systems, apparatuses and methods for landing an unmanned aircraft on a mobile structure are presented. Sensors on the aircraft identify a predetermined landing area on a mobile structure. The aircraft monitors the sensor data to maintain its position hovering over the landing area. The aircraft estimates a future attitude of the surface of the landing area and determines a landing time that corresponds to a desired attitude of the surface of the landing area. The unmanned aircraft executes a landing maneuver to bring the aircraft into contact with the surface of the landing area at the determined landing time.
Abstract translation: 介绍了将无人驾驶飞机降落在移动结构上的系统，设备和方法。 飞机上的传感器识别移动结构上的预定着陆区域。 飞机监控传感器数据，以保持其位置在着陆区域上悬停。 飞机估计着陆区域的表面的未来态度，并且确定对应于着陆区域的表面的期望姿态的着陆时间。 无人飞机执行着陆操作，以在确定的着陆时间使飞机与着陆区域的表面接触。
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3.发明申请
公开(公告)号：WO2015160394A2
公开(公告)日：2015-10-22
申请号：PCT/US2015/011149
申请日：2015-01-13
Applicant: ADVANCED PRODUCT DEVELOPMENT, LLC
Inventor： MCDONNELL, William Randall
CPC classification number: B64C3/10 , B63H9/0685 , B64C39/024 , B64C2201/028 , B64C2201/082 , B64C2201/182 , B64C2201/205 , B64C2201/208 , B64F1/02 , B64F1/04 , B64F1/222 , Y02T50/12 , Y02T50/826
Abstract: An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).
Abstract translation: 一种不对称的飞机（1）和一种飞机（1），其能够从小型船舶（8）中操作并以高密度储存在一个直升机机库（107）中，具有三架或更多架飞机而不需要 起落架或机翼折叠。 这些飞机可以像计算机中的电路板一样滑入和滑出飞机库（90），使用大型拖曳翼伞（6）启动和回收。
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公开(公告)号：WO2016205415A1
公开(公告)日：2016-12-22
申请号：PCT/US2016/037694
申请日：2016-06-15
Applicant: IMAGEKEEPER LLC
Inventor： SPEASL, Jerry , PATTERSON, Mike , ROBERTS, Mark
CPC classification number: G08G5/0034 , B64C39/024 , B64C2201/042 , B64C2201/066 , B64C2201/08 , B64C2201/082 , B64C2201/121 , B64C2201/126 , B64C2201/128 , B64C2201/145 , B64C2201/20 , B64C2201/201 , B64C2201/205 , B64C2201/206 , B64C2201/208 , B64F1/222 , G06Q10/08 , G08G5/0069 , G08G5/0082 , G08G5/0091
Abstract: A base module may be used to receive and house one or more unmanned aerial vehicles (UAVs) via one or more cavities. The base module receives commands from a manager device and identifies a flight plan that allows a UAV to execute the received commands. The base module transfers the flight plan to the UAV and frees the UAV. Once the UAV returns, the base module once again receives it. The base module then receives sensor data from the UAV from one or more sensors onboard the UAV, and optionally receives additional information describing its flight and identifying success or failure of the flight plan. The base module transmits the sensor data and optionally the additional information to a storage medium locally or remotely accessible by the manager device.
Abstract translation: 基座模块可以用于经由一个或多个空腔接收和容纳一个或多个无人机（UAV）。 基本模块从管理器设备接收命令，并识别允许UAV执行接收到的命令的飞行计划。 基地模块将飞行计划转移到无人机，并释放无人机。 一旦UAV返回，基本模块再次接收它。 然后，基本模块从UAV上的一个或多个传感器接收来自UAV的传感器数据，并且可选地接收描述其飞行并识别飞行计划的成功或失败的附加信息。 基本模块将传感器数据和可选的附加信息传输到本地或由管理器设备远程访问的存储介质。
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5.发明申请
公开(公告)号：WO2015160394A3
公开(公告)日：2015-12-10
申请号：PCT/US2015011149
申请日：2015-01-13
Applicant: ADVANCED PRODUCT DEV LLC
Inventor： MCDONNELL WILLIAM RANDALL
CPC classification number: B64C3/10 , B63H9/0685 , B64C39/024 , B64C2201/028 , B64C2201/082 , B64C2201/182 , B64C2201/205 , B64C2201/208 , B64F1/02 , B64F1/04 , B64F1/222 , Y02T50/12 , Y02T50/826
Abstract: An asymmetric aircraft (1) and an aircraft (1) that can operate from small ships (8) and be stored in high density with three aircraft or more in one helicopter hangar (107) without needing a landing gear or wing fold. These aircraft slide into and out of the hangar on dollies (90) like circuit boards in a computer and are launched and recovered using a large towed parafoil (6).
Abstract translation: 一架不对称的飞机（1）和一架可从小型船只运行的飞机（1），并在一架直升机机库（107）内以三个或更多的飞机高密度存储，无需起落架或机翼折叠。 这些飞机在计算机上像电路板一样滑入和移出机库（90）的机库，并使用大型拖缆机（6）发射和恢复。
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Patent Agency Ranking6.发明申请AIRBORNE RIGID KITE WITH ON-BOARD POWER PLANT FOR SHIP PROPULSION 审中-公开带有板载动力装置的AIRBORNE RIGID KITE用于船舶推进
公开(公告)号：WO2015160697A1
公开(公告)日：2015-10-22
申请号：PCT/US2015/025553
申请日：2015-04-13
Applicant: GOOGLE INC.
Inventor： VANDER LIND, Damon , VAN ALSENOY, Thomas , DEVAUL, Richard, Wayne
CPC classification number: B64C39/022 , B63H9/00 , B63H9/0685 , B63H21/20 , B63J2003/002 , B63J2003/046 , B64C31/06 , B64C2201/205 , B64D3/00 , B64F1/36 , B64F3/00 , B64F3/02 , C02F1/20 , C02F1/4693 , C02F2101/10 , C25B1/04 , C25B9/00 , F03D5/00 , F03D9/008 , F03D9/25 , F03D9/32 , F05B2240/917 , F05B2240/921 , F05B2240/923 , Y02E10/70 , Y02E10/725 , Y02E10/728 , Y02E60/366 , Y02P20/133 , Y02T70/5209 , Y02T70/5218 , Y02T70/70 , Y02T90/46
Abstract: A vehicle-based airborne wind turbine system having an aerial wing, a plurality of rotors each having a plurality of rotatable blades positioned on the aerial wing, an electrically conductive tether secured to the aerial wing and secured to a ground station positioned on a vehicle, wherein the aerial wing is adapted to receive electrical power from the vehicle that is delivered to the aerial wing through the electrically conductive tether; wherein the aerial wing is adapted to operate in a flying mode to harness wind energy to provide a first pulling force through the tether to pull the vehicle; and wherein the aerial wing is also adapted to operate in a powered flying mode wherein the rotors may be powered so that the turbine blades serve as thrust- generating propellers to provide a second pulling force through the tether to pull the vehicle.
Abstract translation: 一种具有空中翼面的车载机载风力涡轮机系统，多个转子，每个转子具有位于空中飞翼上的多个可旋转叶片，固定在飞行器上并固定在位于车辆上的地面站的导电系绳， 其中所述空中翼适于从通过所述导电系绳传送到所述空中翼的车辆接收电力; 其中所述空中翼适于以飞行模式操作以利用风能以提供穿过所述系绳的第一拉力以拉动所述车辆; 并且其中所述空中翼还适于以动力飞行模式操作，其中所述转子可以被供电，使得所述涡轮机叶片用作推力产生螺旋桨，以提供通过所述系绳拉动所述车辆的第二拉力。
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公开(公告)号：WO2010033833A1
公开(公告)日：2010-03-25
申请号：PCT/US2009/057525
申请日：2009-09-18
Applicant: RAYTHEON COMPANY , SAMPSON, Ray , BOSSERT, David E. , ZERBE, Jeffrey N.
Inventor： SAMPSON, Ray , BOSSERT, David E. , ZERBE, Jeffrey N.
CPC classification number: F41F3/07 , B63B22/003 , B63B22/24 , B63G6/00 , B63G8/30 , B64C2201/201 , B64C2201/205
Abstract: Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.
Abstract translation: 根据本发明的各个方面的用于船舶部署的方法和装置可以与适于由船用车辆展开的可浮动壳体结合操作。 可浮动壳体可以适于从船用车辆发射并升起到地面。 诸如无人驾驶飞行器的资产可以从表面浮动的壳体部署。
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公开(公告)号：WO2009079045A2
公开(公告)日：2009-06-25
申请号：PCT/US2008076769
申请日：2008-09-18
Applicant: RAYTHEON CO , BOSSERT DAVID , ZERBE JEFF , SAMPSON RAY
Inventor： BOSSERT DAVID , ZERBE JEFF , SAMPSON RAY
IPC: B64F1/06
CPC classification number: F41F3/07 , B64C2201/201 , B64C2201/205 , F42B15/20
Abstract: Methods and apparatus for marine deployment according to various aspects of the present invention may operate in conjunction with a floatable housing adapted to be deployed by a marine vehicle. The floatable housing may be adapted to be launched from a marine vehicle and rise to the surface. Assets, such as an unmanned aerial vehicle, may be deployed from the surfaced floatable housing.
Abstract translation: 根据本发明的各个方面的用于船舶部署的方法和装置可以与适于由船用车辆展开的可浮动壳体结合操作。 可浮动壳体可以适于从船用车辆发射并升起到地面。 诸如无人驾驶飞行器的资产可以从表面浮动的壳体部署。
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公开(公告)号：WO2016078822A1
公开(公告)日：2016-05-26
申请号：PCT/EP2015/073084
申请日：2015-10-07
Applicant: THYSSENKRUPP MARINE SYSTEMS GMBH , THYSSENKRUPP AG
Inventor： TREYDE, Hinnerk
CPC classification number: B64C39/024 , B63B35/50 , B64C2201/18 , B64C2201/205 , B64F1/125
Abstract: Die Erfindung betrifft ein System zur Einholung eines unbemannten Luftfahrzeugs (10), wobei das System eine Landeplattform und ein unbemanntes Luftfahrzeug (10) umfasst, wobei es sich bei dem unbemannten Luftfahrzeug (10) um ein senkrecht landendes unbemanntes Luftfahrzeug (10) handelt, wobei die Landeplattform ein Gitter (20) aufweist. Ferner betrifft die Erfindung ein Verfahren zur Einholung eines unbemannten Luftfahrzeugs (10) auf einer Landeplattform unter Verwendung eines erfindungsgemäßen Systems zur Einholung eines unbemannten Luftfahrzeugs (10).
Abstract translation: 本发明涉及一种系统，用于获得无人驾驶飞行器（10），其中所述系统包括一升降平台和无人驾驶飞行器（10），其特征在于，它是在无人驾驶飞行器（10）上的垂直全国各地形成无人驾驶飞行器（10），其中 着陆平台包括网格（20）。 本发明还涉及一种用于根据本发明的用于获得无人驾驶飞行器（10）使用的系统的着陆平台上获得无人驾驶飞行器（10）的方法。
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公开(公告)号：WO2014025444A3
公开(公告)日：2015-06-25
申请号：PCT/US2013042026
申请日：2013-05-21
Applicant: ARLTON PAUL E , ARLTON DAVID J
Inventor： ARLTON PAUL E , ARLTON DAVID J
IPC: B64C27/00
CPC classification number: B64C27/10 , B64C27/24 , B64C27/26 , B64C27/605 , B64C29/02 , B64C39/024 , B64C2027/8236 , B64C2201/024 , B64C2201/027 , B64C2201/042 , B64C2201/205 , B64C2201/206
Abstract: A rotary wing vehicle includes a body structure having an elongated tubular backbone or core, and a counter-rotating coaxial rotor system having rotors with each rotor having a separate motor to drive the rotors about a common rotor axis of rotation. The rotor system is used to move the rotary wing vehicle in directional flight.
Abstract translation: 旋转翼车辆包括具有细长管状骨架或芯体的主体结构，以及具有转子的反向旋转同轴转子系统，每个转子具有单独的电动机，以围绕公共转子旋转轴线驱动转子。 转子系统用于在定向飞行中移动旋翼机。
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