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公开(公告)号：US20180022423A1
公开(公告)日：2018-01-25
申请号：US15694215
申请日：2017-09-01
Applicant: Lockheed Martin Corporation
Inventor： Nathan E. Low , Peter J. Demas
CPC classification number: B63B25/002 , B63B35/00 , B63H11/00 , B63H2011/006 , B64C39/022 , B64C39/024 , B64C2201/121
Abstract: A water-propelled or water-powered unmanned aerial vehicle including a base configured to carry a payload, and at least one nozzle attached thereto. The at least one nozzle is configured to selectively receive pressurized fluid from a source located remotely from the vehicle. The vehicle includes a control system configured to alter or otherwise selectively dictate the flow of fluid through the at least one nozzle and/or the orientation of the at least one nozzle with respect to the base in response to a received control signal for providing controlled unmanned vehicle flight.
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公开(公告)号：US20170308087A1
公开(公告)日：2017-10-26
申请号：US15494454
申请日：2017-04-22
Applicant: Yuneec International (China) Co, Ltd
Inventor： Yu TIAN , Wenyan JIANG
CPC classification number: G05D1/0094 , B64C39/024 , B64C2201/121 , B64C2201/141
Abstract: The present disclosure relates to an aerial shooting method and system using a drone, wherein the aerial shooting method using a drone comprises steps of presetting an aerial path and generating a first operation instruction based on the preset aerial path; controlling the drone to fly along the preset aerial path according to the first operation instruction; marking a plurality of waypoints during the flight of the drone along the preset aerial path; planning a flight path based on the plurality of waypoints and generating a flight instruction based on the flight path; making the drone automatically fly along the flight path according to the flight instruction; and controlling the drone to shoot during the automatic flight of the drone.
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公开(公告)号：US20170261613A1
公开(公告)日：2017-09-14
申请号：US15443143
申请日：2017-02-27
Applicant: Raytheon BBN Technologies Corp.
Inventor： Brian R. Van Voorst
CPC classification number: G01S17/026 , B64C39/024 , B64C2201/027 , B64C2201/108 , B64C2201/12 , B64C2201/121 , B64C2201/141 , B64C2201/146 , F41H11/02 , F41H13/0006 , G01S7/4817 , G01S7/495 , G01S7/51 , G01S17/023 , G01S17/66 , G01S17/87 , G01S17/89 , G01S17/933 , G05D1/0016 , G05D1/0088 , G05D1/0094 , G05D1/101 , G05D1/12 , G06K9/0063 , G06K2209/21 , G06T17/05 , G08G5/0026 , G08G5/0069 , G08G5/0082 , H04W4/021
Abstract: A counter drone system includes a cueing sensor to detect the presence of an object wherein the cueing sensor cues the presence of a target drone, a long range LIDAR system having a sensor pointed in a direction of the target drone to acquire and track at long range the target drone to provide an accurate location of the target drone wherein once a track is acquired, the motion of the target drone is used to maintain the track of the target drone and a threat detector wherein LIDAR data is provided to the threat detector to determine if the target drone is a threat.
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公开(公告)号：US20170254622A1
公开(公告)日：2017-09-07
申请号：US15057574
申请日：2016-03-01
Applicant: Northrop Grumman Systems Corporation
Inventor： David W. Evans , Gregory L. Larson , Jeffrey M. Yang
CPC classification number: F41G7/2206 , B64C39/024 , B64C2201/121 , B64C2201/141 , B64C2201/146 , B64D7/00 , F41G3/04 , F41G7/007 , F41G7/2233 , F41G7/30
Abstract: A manned aircraft and unmanned aerial vehicles (UAVs) fly on a mission as a team. The UAVs carry additional weapons and/or munitions that can be controlled by the manned aircraft. The pilot of the manned aircraft selects weapons or munitions carried by either the manned aircraft or one of the UAVs. A display in the manned aircraft illustrates weapons available on both the manned aircraft and UAVs. The pilot of the manned aircraft picks a weapon from the display and then targets and fires the weapon. The targeting and guidance of the weapon can be carried out using computers on the manned aircraft and/or computers on the UAV.
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公开(公告)号：US20170082397A1
公开(公告)日：2017-03-23
申请号：US14861010
申请日：2015-09-22
Applicant: The Boeing Company
Inventor： William C. Hester, JR.
CPC classification number: F41F5/00 , B64C39/024 , B64C2201/024 , B64C2201/121 , B64D1/06 , F41F3/065 , F41G7/007 , F41G7/226 , F41G7/2293 , F41G7/346 , F41G9/002
Abstract: A munitions dispenser employs a plurality of launch tubes mounted in an array as a segmented dispenser assembly. Each tube in the array is configured to carry a selected munition releasably coupled in a cylindrical bore of the tube for substantially vertical release through a lower aperture. A frame, mountable to an air vehicle, carries the array of launch tubes. A skin covers the array of launch tubes with the skin and frame with the array configured for nested engagement of multiple segmented assemblies.
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Patent Agency Ranking
公开(公告)号：US20160185447A1
公开(公告)日：2016-06-30
申请号：US14947871
申请日：2015-11-20
Applicant: AeroVironment, Inc.
Inventor： Carlos Thomas Miralles
CPC classification number: B64C13/16 , B64B2201/00 , B64C39/024 , B64C2201/04 , B64C2201/121 , B64C2201/141 , B64C2201/165 , F41G7/2253 , F41G7/2286 , F41G7/2293 , G05D1/12
Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
Abstract translation: 一种包括具有翼元件和尾部元件的无人飞行器（UAV）的系统，其被配置成滚动以通过滚动来成角度地定向UAV，以便在其后期终点阶段将UAV的纵向平面与目标对准。 一种UAV身体重定向的方法，包括：（a）由处理器确定基于身体固定框架的目标点和视轴之间的距离的视轴角度误差校正值; 和（b）实现UAV机动，其包括将目标点平移到身体固定框架中的重定向目标点的角度角色率分量，以经由偏移角度校正值来保持偏移角度。
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公开(公告)号：US09211947B2
公开(公告)日：2015-12-15
申请号：US14016602
申请日：2013-09-03
Applicant: AEROVIRONMENT, INC.
Inventor： Carlos Miralles
CPC classification number: B64C13/16 , B64B2201/00 , B64C39/024 , B64C2201/04 , B64C2201/121 , B64C2201/141 , B64C2201/165 , F41G7/2253 , F41G7/2286 , F41G7/2293 , G05D1/12
Abstract: A system comprising an unmanned aerial vehicle (UAV) having wing elements and tail elements configured to roll to angularly orient the UAV by rolling so as to align a longitudinal plane of the UAV, in its late terminal phase, with a target. A method of UAV body re-orientation comprising: (a) determining by a processor a boresight angle error correction value bases on distance between a target point and a boresight point of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point to a re-oriented target point in the body-fixed frame, to maintain the offset angle via the offset angle correction value.
Abstract translation: 一种包括具有翼元件和尾部元件的无人飞行器（UAV）的系统，其被配置成滚动以通过滚动来成角度地定向UAV，以便在其后期终点阶段将UAV的纵向平面与目标对准。 一种UAV身体重定向的方法，包括：（a）由处理器确定基于身体固定框架的目标点和视轴之间的距离的视轴角度误差校正值; 和（b）实现UAV机动，其包括将目标点平移到身体固定框架中的重定向目标点的角度角色率分量，以经由偏移角度校正值来保持偏移角度。
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公开(公告)号：US20150266576A1
公开(公告)日：2015-09-24
申请号：US14484138
申请日：2014-09-11
Applicant: Sandia Corporation
Inventor： Clinton G. Hobbart , William D. Morse , Robert James Bickerstaff
CPC classification number: B60F5/02 , B60F3/0007 , B60F3/003 , B60F5/006 , B63G8/001 , B63G8/08 , B63G2008/004 , B64C37/00 , B64C39/024 , B64C2201/00 , B64C2201/021 , B64C2201/028 , B64C2201/082 , B64C2201/121 , B64C2201/126 , B64C2201/127 , B64C2201/146 , B64C2211/00 , B64D47/08
Abstract: A MEUV that is able to navigate aerial, aquatic, and terrestrial environments through the use of different mission mobility attachments is disclosed. The attachments allow the MEUV to be deployed from the air or through the water prior to any terrestrial navigation. The mobility attachments can be removed or detached by and from the vehicle during a mission.
Abstract translation: 公开了能够通过使用不同的任务移动附件导航航空，水上和陆地环境的MEUV。 附件允许在任何地面导航之前从空中或通过水部署MEUV。 在任务期间，移动附件可以从车辆移除或拆卸。
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公开(公告)号：US20150203201A1
公开(公告)日：2015-07-23
申请号：US14592362
申请日：2015-01-08
Applicant: AEROVIRONMENT, INC.
Inventor： TONY SHUO TAO , NATHAN OLSON , CARLOS THOMAS MIRALLES , ROBERT NICKERSON PLUMB
CPC classification number: B64C3/56 , B64C3/44 , B64C3/50 , B64C5/12 , B64C9/02 , B64C9/08 , B64C9/18 , B64C11/00 , B64C13/18 , B64C13/34 , B64C39/024 , B64C2009/005 , B64C2201/021 , B64C2201/08 , B64C2201/102 , B64C2201/121 , B64C2201/14 , B64C2201/145 , B64C2201/146
Abstract: A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) configured to control pitch, roll, and/or yaw via airfoils having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns. Embodiments include one or more rudder elements which may be rotatably attached and actuated by an effector member disposed within the fuselage housing and extendible in part to engage the one or more rudder elements.
Abstract translation: 一种包括飞行器或无人驾驶飞行器（UAV）的系统，其构造成经由具有弹性安装的后缘的机翼来控制俯仰，滚动和/或偏航，所述后翼与机身偏转致动器角相对。 实施例包括一个或多个舵元件，其可以由设置在机身壳体内的效应器构件可旋转地附接和致动，并且部分地可部分地接合一个或多个舵元件。
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公开(公告)号：US08794566B2
公开(公告)日：2014-08-05
申请号：US13565654
申请日：2012-08-02
Applicant: Donald B. Hutson
Inventor： Donald B. Hutson
CPC classification number: B64D47/08 , B64C27/006 , B64C27/10 , B64C27/20 , B64C39/024 , B64C2025/325 , B64C2201/024 , B64C2201/042 , B64C2201/066 , B64C2201/108 , B64C2201/121 , B64C2201/126 , B64C2201/127 , B64C2201/182 , B64D9/00 , F16M11/123 , F16M11/18 , F16M13/00 , F16M13/02 , F16M2200/041
Abstract: In specific embodiments, a vehicle propellable through fluids comprises a main work section and a plurality of propulsion units. The main work section includes a payload support hub, a payload support structure rotatable in 360° about the payload support hub in at least one axis, and a core including at least one microprocessor, the core at least partially nested within the payload support hub. The at least one microprocessor is adapted to substantially maintain an orientation of the payload support structure relative to a horizon line as the vehicle is propelled. One or more payloads are mountable on the rotatable payload support structure.
Abstract translation: 在具体实施例中，通过流体推进的车辆包括主工作部分和多个推进单元。 主工作部分包括有效载荷支撑轮毂，在至少一个轴线上围绕有效载荷支撑轮毂360°旋转的有效载荷支撑结构，以及包括至少一个微处理器的核心，至少部分地嵌套在有效载荷支撑轮毂内。 所述至少一个微处理器适于在车辆被推进时基本上保持有效载荷支撑结构相对于水平线的取向。 一个或多个有效载荷可安装在可旋转的有效载荷支撑结构上。
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