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    Transient surface contact vehicle
    181.
    发明授权
    Transient surface contact vehicle 失效
    瞬态表面接触载体

    公开(公告)号：US4505442A

    公开(公告)日：1985-03-19

    申请号：US505815

    申请日：1983-06-20

    Applicant: Jerome Kirsch ,  M. Alan Kopsco ,  Edward Markow ,  Michael Sturm

    Inventor： Jerome Kirsch ,  M. Alan Kopsco ,  Edward Markow ,  Michael Sturm

    IPC: B63B1/28 ,  F41G7/22 ,  F42B17/00 ,  F42B23/00 ,  F41G9/00 ,  F42B15/20

    CPC classification number: F42B23/00 ,  B64C25/54 ,  B64C37/00 ,  B64C39/024 ,  F41G7/22 ,  F42B17/00 ,  B63B1/322 ,  B64C2201/042 ,  B64C2201/088 ,  B64C2201/121 ,  B64C2201/205 ,  Y02T70/12

    Abstract: A transient surface contact vehicle for transporting a load from a surface starting point to a surface end point has a structure for carrying the load from the starting point to the end point. A vehicle support extends from the structure. A buoyancy control device mounted in the structure is coupled to the vehicle support for selectively making the support buoyant and non-buoyant whereby when the support is buoyant it abuts the surface of a body of water thereby supporting the vehicle at a predetermined distance above the surface of the body of water. An acquisition sensor mounted on the structure initiates water surface operations. A sensor is mounted on the structure and cooperates with the acquisition sensor to energize upon tracking of the target and to move the vehicle along the water surface to impact with the target at the end point. A position control mounted on the vehicle produces a negative pitching moment to maintain the structure in surface-following contact with the body of water.

    Abstract translation: 用于将载荷从表面起始点传送到表面终点的瞬时表面接触车辆具有用于承载起始点到终点的载荷的结构。 车辆支架从结构延伸。 安装在结构中的浮力控制装置联接到车辆支撑件，用于选择性地使支撑件浮力和非浮力，由此当支撑件浮力时，其抵靠水体表面，从而在车辆表面上方预定的距离处支撑车辆 的身体的水。 安装在结构上的采集传感器启动水面操作。 传感器安装在结构上并与采集传感器配合，以在跟踪目标时激励并沿着水面移动车辆以在终点处与目标撞击。 安装在车辆上的位置控制产生负俯仰力矩，以保持结构与水体的表面跟随接触。

    UNMANNED AERIAL VEHICLE MANAGEMENT
    182.
    发明申请
    UNMANNED AERIAL VEHICLE MANAGEMENT 审中-公开
    不定期的空中客车管理

    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

    IPC: B65F9/00 ,  G01C23/00 ,  B65G67/00

    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。

    TRAILER FOR AUTONOMOUS VEHICLE
    183.
    发明申请
    TRAILER FOR AUTONOMOUS VEHICLE 审中-公开
    自动车辆拖车

    公开(公告)号：WO2015038697A2

    公开(公告)日：2015-03-19

    申请号：PCT/US2014/055075

    申请日：2014-09-11

    Applicant: SILICIS TECHNOLOGIES, INC.

    Inventor： STIGLER, Michael, J. ,  SETAR, Nicholas, James

    CPC classification number: B60P3/11 ,  B60P7/06 ,  B60P7/0876 ,  B64B1/10 ,  B64B1/50 ,  B64B1/58 ,  B64B1/66 ,  B64C39/022 ,  B64C39/024 ,  B64C2201/022 ,  B64C2201/06 ,  B64C2201/101 ,  B64C2201/12 ,  B64C2201/121 ,  B64C2201/125 ,  B64C2201/127 ,  B64C2201/148 ,  B64C2201/208 ,  B64F1/14 ,  B64F3/02 ,  G08C17/02

    Abstract: The disclosed embodiments include a trailer for an autonomous vehicle controlled by a command and control interface. The trailer includes a trailer body configured to retain the autonomous vehicle in an undeployed configuration. The trailer also anchors the autonomous vehicle in a deployed configuration. A tether is provided having a first end coupled to the trailer body and a second end that is configured to couple to the autonomous vehicle. A winch is utilized to adjust a length of the tether to move the autonomous vehicle between the undeployed configuration and deployed configuration. Further, a communication system communicates with the command and control interface and the autonomous vehicle to control movement of the autonomous vehicle between the undeployed configuration and deployed configuration.

    Abstract translation: 所公开的实施例包括用于由命令和控制界面控制的自主车辆的拖车。 拖车包括配置成将自主车辆保持在未展开配置中的拖车主体。 拖车还将自主车辆锚定在展开配置中。 提供系绳，其具有联接到拖车主体的第一端部和构造成联​​接到自主车辆的第二端部。 利用绞车调节系绳的长度以使自主车辆在未展开配置和展开配置之间移动。 此外，通信系统与命令和控制接口以及自主车辆进行通信，以控制自主车辆在未部署配置和已部署配置之间的移动。

    UNMANNED AERIAL VEHICLE ANGULAR REORIENTATION
    185.
    发明申请
    UNMANNED AERIAL VEHICLE ANGULAR REORIENTATION 审中-公开
    不定期的空中客车航向转向

    公开(公告)号：WO2012119132A3

    公开(公告)日：2014-04-24

    申请号：PCT/US2012027619

    申请日：2012-03-02

    Applicant: AEROVIRONMENT INC ,  MIRALLES CARLOS

    Inventor： MIRALLES CARLOS

    IPC: B64C13/16

    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) (100) having wing elements (141, 142) and tail elements (143, 144) configured to roll to angularly orient the UAV (100) 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 (940) a boresight angle error correction value (850) bases on distance between a target point (812) and a boresight point (820) of a body-fixed frame; and (b) effecting a UAV maneuver comprising an angular role rate component translating the target point (812) to a re-oriented target point (814) in the body-fixed frame, to maintain the offset angle via (850) the offset angle correction value.

    Abstract translation: 一种包括具有翼元件（141,142）和尾部元件（143,144）的无人驾驶飞行器（UA）（100）的系统，所述尾部元件（143,144）被配置成滚动以通过滚动角度地定向所述UAV（100） 无人机在其末期阶段有一个目标。 一种UAV身体重新定位的方法，包括：（a）基于处理器（940）确定基于目标点（812）和身体 - 角度（820）的视轴点（820）之间的距离的视轴角度误差校正值（850） 固定框架 和（b）进行无人机操作，其包括将所述目标点（812）转换为所述身体固定框架中的重定向目标点（814）的角度角色分量，以通过（850）偏移角度 校正值。

    APPARATUS FOR UNMANNED VEHICLES
    186.
    发明申请
    APPARATUS FOR UNMANNED VEHICLES 审中-公开
    装备用于无人驾驶的车辆

    公开(公告)号：WO2012084635A1

    公开(公告)日：2012-06-28

    申请号：PCT/EP2011/072723

    申请日：2011-12-14

    Applicant: BAE SYSTEMS PLC ,  BEGGS, Kevin, William ,  AXFORD, Richard, Descond, Joseph

    Inventor： BEGGS, Kevin, William ,  AXFORD, Richard, Descond, Joseph

    IPC: B64C39/02 ,  F42B12/36 ,  F42C15/42

    CPC classification number: F42B12/365 ,  B64C2201/121 ,  B64C2201/146 ,  F42C15/42

    Abstract: Apparatus and a method performed by the apparatus, the apparatus being wholly or partially mounted on an unmanned vehicle (e.g. an unmanned air vehicle) and arranged to act upon a payload (e.g. a lethal effector), the payload being mounted on the unmanned vehicle and, under an action of the apparatus, able to be changed from being in a first state to being in a second state, the method comprising: receiving an instruction that the unmanned vehicle, with the payload mounted thereon, is to travel to a location; determining that the payload is in the first state; and responsive to the step of determining that the payload is in the first state: opposing the payload being changed to being in the second state; and providing, for an entity remote from the unmanned vehicle, an indication that the payload is in the first state.

    Abstract translation: 装置和由该装置执行的方法，该装置完全或部分地安装在无人驾驶车辆（例如无人驾驶飞行器车辆）上并被布置成作用于有效载荷（例如致命执行器）上，有效载荷安装在无人驾驶车辆上， 在装置的动作下，能够从第一状态变为处于第二状态，所述方法包括：接收无人驾驶车辆，其上安装有有效载荷的行驶到位置的指令; 确定有效载荷处于第一状态; 并且响应于确定所述有效负载处于所述第一状态的步骤：将所述有效负载改变为处于所述第二状态; 以及为远离所述无人驾驶车辆的实体提供所述有效载荷处于所述第一状态的指示。

    STOWABLE DESIGN FOR UNMANNED AERIAL VEHICLE
    189.
    发明申请
    STOWABLE DESIGN FOR UNMANNED AERIAL VEHICLE 审中-公开
    无人机的可携式设计

    公开(公告)号：WO2006073750A2

    公开(公告)日：2006-07-13

    申请号：PCT/US2005/045715

    申请日：2005-12-16

    Applicant: ALMAN, James

    Inventor： ALMAN, James

    IPC: B64D45/02

    CPC classification number: B64C39/024 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/105 ,  B64C2201/107 ,  B64C2201/121 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/165 ,  B64C2201/201 ,  B64C2201/203

    Abstract: An unmanned aerial vehicle (UAV) having a design for optimum stowability and low cost. The UAV having a collapsible wing section which can be easily removed from the fuselage, allowing for quick assembly and disassembly and ease of portability. The unmanned aerial vehicle includes a primary wing assembly, a fuselage, a means for propelling the unmanned aerial vehicle , and means for remotely controlling the unmanned aerial vehicle. The primary wing assembly includes a wing having a center spar and two outwardly diverging side spars. The wing also has a pliable flexible material supported by the center spar and the at least two outwardly diverging side spars. The pylon is connected to the wing and supports the wing. The fuselage is connected to the pylon such that the pylon extends away from the fuselage and spaces the wing a distance from the fuselage. The fuselage includes a tail having a rudder located along a trailing edge and elevators located along the trailing edge.

    Abstract translation: 无人驾驶飞行器（UAV）具有最佳装载性和低成本的设计。 该无人机具有可折叠的机翼部分，可以轻松地从机身上拆下，从而实现快速装配和拆卸，便于携带。 无人驾驶飞行器包括主翼组件，机身，用于推进无人飞行器的装置和用于远程控制无人飞行器的装置。 主翼组件包括具有中心翼梁和两个向外发散侧翼的翼。 机翼还具有由中心翼梁和至少两个向外分开的侧翼支撑的柔韧柔性材料。 塔架连接到机翼并支撑机翼。 机身连接到塔架，使得塔架远离机身延伸并将机翼与机身隔开一段距离。 机身包括尾部，其尾部有一个方向舵，后部有电梯，电梯位于尾部。

    WEAPONS PLATFORM CONSTRUCTION
    190.
    发明申请
    WEAPONS PLATFORM CONSTRUCTION 审中-公开
    武器平台建设

    公开(公告)号：WO2003042620A1

    公开(公告)日：2003-05-22

    申请号：PCT/AU2002/001441

    申请日：2002-10-24

    Applicant: METAL STORM LIMITED ,  O'DWYER, James, Michael

    Inventor： O'DWYER, James, Michael

    IPC: F41A23/00

    CPC classification number: B64D7/00 ,  B64C2201/121 ,  B64D7/04 ,  B64D7/08 ,  F41A21/48 ,  F41A23/00 ,  F42B5/035

    Abstract: A vehicular weapons platform (30) including a plurality of barrel assemblies (10), wherein each barrel assembly includes a barrel (11), a plurality of projectiles (14) axially disposed within the barrel for operative sealing engagement with the bore of the barrel (11) and discrete propellant charges (15) for propelling respective projectiles sequentially through the muzzle of the barrel; and at least one of said plurality of barrel assemblies (10) includes a barrel which also forms a structural member of the weapons platform. In one preferred form, the weapons platform takes the form of a small combat aerial vehicle (SCAV) (30), wherein the barrel assemblies (10) form the airframe. A method of constructing a weapons platform from the barrel assemblies is also described.

    Abstract translation: 一种包括多个筒体组件（10）的车辆武器平台（30），其中每个筒体组件包括筒体（11），多个射出件（14），其轴向设置在所述筒体内，用于与所述筒体 （11）和离散的推进剂装料（15），用于依次通过枪管的枪口推动各射弹; 并且所述多个筒组件（10）中的至少一个包括还形成武器平台的结构构件的筒体。 在一种优选形式中，武器平台采取小作战飞行器（SCAV）（30）的形式，其中枪管组件（10）形成机身。 还描述了从筒组件构造武器平台的方法。

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