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    TORQUE PRODUCTION VEHICLE AND METHOD
    261.
    发明申请
    TORQUE PRODUCTION VEHICLE AND METHOD 审中-公开
    扭矩生产车辆和方法

    公开(公告)号：WO2011081695A3

    公开(公告)日：2011-10-13

    申请号：PCT/US2010051948

    申请日：2010-10-08

    Applicant: RAYTHEON CO ,  SMITH TIMOTHY D

    Inventor： SMITH TIMOTHY D

    IPC: B64C39/06 ,  B64C39/02

    CPC classification number: B64C39/064 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/084 ,  B64C2201/205

    Abstract: A torque production vehicle (100) includes a plenum body (110) having a wall (112) with a central port (120) and a radial port (130) formed within the wall, an impeller (140) disposed within the plenum body to move air through the central port, an engine (145) coupled to the impeller to rotate the impeller about an axis (Ar), at least one arm (150) coupled to the plenum body, and a plurality of foils (160) disposed in the radial port to direct air about the plenum body to provide a torque force (Ft) about the plenum body.

    Abstract translation: 转矩生产车辆（100）包括具有壁（112）的增压室（110），所述壁具有中心端口（120）和形成在壁内的径向端口（130），设置在增压室内部的叶轮（140） 将空气移动通过中心端口，联接到叶轮的发动机（145），以使叶轮围绕轴线（Ar）旋转，至少一个臂（150）联接到增压室，以及多个箔（160） 径向端口，用于引导围绕增压室主体的空气以提供围绕增压室的扭矩力（Ft）。

    TORQUE PRODUCTION VEHICLE AND METHOD
    262.
    发明申请
    TORQUE PRODUCTION VEHICLE AND METHOD 审中-公开
    扭矩生产车辆和方法

    公开(公告)号：WO2011081695A2

    公开(公告)日：2011-07-07

    申请号：PCT/US2010/051948

    申请日：2010-10-08

    Applicant: RAYTHEON COMPANY ,  SMITH, Timothy, D.

    Inventor： SMITH, Timothy, D.

    IPC: B64C39/06

    CPC classification number: B64C39/064 ,  B64C39/024 ,  B64C2201/027 ,  B64C2201/084 ,  B64C2201/205

    Abstract: A torque production vehicle includes a plenum body having a wall with a central port and a radial port formed within the wall, an impeller disposed within the plenum body to move air through the central port, an engine coupled to the impeller to rotate the impeller about an axis, at least one arm coupled to the plenum body, and a plurality of foils disposed in the radial port to direct air about the plenum body to provide a torque force about the plenum body.

    Abstract translation: 扭矩生产车辆包括具有中心端口和形成在壁内的径向端口的壁的增压室，设置在增压室内的叶轮以将空气移动通过中心端口，发动机联接到叶轮以使叶轮围绕 一个轴线，至少一个连接到集气室主体的臂，以及设置在该径向端口中的多个箔，以引导围绕该增压室的空气以提供围绕该增压室的转矩力。

    METHOD FOR LAUNCHING A DRONE
    263.
    发明申请
    METHOD FOR LAUNCHING A DRONE 审中-公开
    启动DRON的方法

    公开(公告)号：WO2010031384A3

    公开(公告)日：2010-10-14

    申请号：PCT/DE2009001286

    申请日：2009-09-16

    Applicant: GABLER GMBH MASCHBAU ,  VIERTEL CHRISTIAN ,  TENBERGEN MARTIN

    Inventor： VIERTEL CHRISTIAN ,  TENBERGEN MARTIN

    IPC: B64F1/06

    CPC classification number: B64F1/06 ,  B64C2201/084

    Abstract: The method for launching a drone (10) is carried out by means of a launch catapult (9) which applies the launch energy, such that the launch catapult (9) is first of all aligned, before launch. In this case, the launch catapult (9) is concealed by means of visual protection (4), with the visual protection (4) being at least partially removed only after alignment and immediately before launch.

    Abstract translation: 通过施加初始能量的启动弹射器（9）启动无人机（10）的方法被执行，使得首先在启动之前对齐发射弹射器（9）。 在这种情况下，发射弹射器（9）通过屏幕（4）覆盖，其中屏幕（4）仅在对准之后且即将开始之前至少部分地被移除。

    SLIDING FRAME AIRCRAFT LAUNCHER AND RELATED METHOD
    264.
    发明申请
    SLIDING FRAME AIRCRAFT LAUNCHER AND RELATED METHOD 审中-公开
    滑动框架飞机推进器及相关方法

    公开(公告)号：WO2010048176A1

    公开(公告)日：2010-04-29

    申请号：PCT/US2009/061318

    申请日：2009-10-20

    Applicant: AAI Corporation ,  MILLER, Stephen William

    Inventor： MILLER, Stephen William

    IPC: B64F1/04

    CPC classification number: B64F1/06 ,  B64C2201/021 ,  B64C2201/084

    Abstract: An aircraft launcher includes a base frame, a first sliding frame that slides with respect to the base frame, a second sliding frame that slides with respect to the first sliding frame, an aircraft support located on the second sliding frame, and a drive apparatus adapted to slide at least one of the first sliding frame and the second sliding frame with respect to the base frame.

    Abstract translation: 飞机发射器包括基架，相对于基架滑动的第一滑动框架，相对于第一滑动框架滑动的第二滑动框架，位于第二滑动框架上的飞行器支架，以及适于 相对于基架滑动第一滑动框架和第二滑动框架中的至少一个。

    A CONNECTOR FOR HARSH ENVIRONMENTS
    266.
    发明申请
    A CONNECTOR FOR HARSH ENVIRONMENTS 审中-公开
    HARH环境连接器

    公开(公告)号：WO2007032816A2

    公开(公告)日：2007-03-22

    申请号：PCT/US2006/027570

    申请日：2006-07-15

    Applicant: PHYSICAL OPTICS CORPORATION

    Inventor： LEE, Kang ,  FORRESTER, Thomas ,  JANNSON, Tomasz ,  KOSTRZEWSKI, Andrew ,  SAVANT, Gajendra

    IPC: F16C11/00

    CPC classification number: B64F1/06 ,  B64C2201/084 ,  B64C2201/182 ,  H01R13/005 ,  H01R13/2421 ,  H01R35/04 ,  H01R39/64 ,  Y10T403/32606

    Abstract: Two embodiments of a connector that can be mated without regard for its orientation are disclosed. One embodiment is mated and demated autonomously as part of a system for recovering, docking with, recharging and re-launching unmanned aerial vehicles. Another embodiment is employed on the decks of vessels to facilitate mating and demating of various equipment providing different functions to reconfigure the vessel. Because both embodiments are configured for connection irrespective of angular orientation over 360°, they are especially suited for harsh environments including autonomous operation, rough seas, darkness and the like.

    Abstract translation: 公开了可以不考虑其取向而配合的连接器的两个实施例。 作为用于恢复，对接，再充电和重新发射无人驾驶飞行器的系统的一部分，一个实施例被自动地配合和排列。 在容器的甲板上采用另一个实施例，以便于提供不同功能的各种设备的配合和排气以重新配置容器。 由于两个实施例都被配置为连接，而不管角度取向超过360°，它们特别适用于恶劣的环境，包括自主操作，粗糙的海洋，黑暗等。

    UNMANNED AIRBORNE VEHICLE FOR GEOPHYSICAL SURVEYING
    267.
    发明申请
    UNMANNED AIRBORNE VEHICLE FOR GEOPHYSICAL SURVEYING 审中-公开
    无人机空中车辆进行地球物理测量

    公开(公告)号：WO2006037237A1

    公开(公告)日：2006-04-13

    申请号：PCT/CA2005/001557

    申请日：2005-10-11

    Applicant: FUGRO AIRBORNE SURVEYS CORP. ,  MILES, Philip John ,  PARTNER, Richard Thomas ,  KEELER, Kenneth Ronald ,  MCCONNELL, Terence James

    Inventor： MILES, Philip John ,  PARTNER, Richard Thomas ,  KEELER, Kenneth Ronald ,  MCCONNELL, Terence James

    IPC: G01V3/165 ,  G01V3/40 ,  B64C39/02

    CPC classification number: B64C39/024 ,  B64C2201/084 ,  B64C2201/127 ,  B64C2201/141 ,  B64C2201/182 ,  B64C2201/208 ,  G01V3/165

    Abstract: An un-manned airborne vehicle (UAV), for acquiring aeromagnetic data for geophysical surveying at low altitude on land or over water, comprising an extended fuselage that is adapted to hold and maintain magnetometer and a magnetic compensation magnetometer at a minimum distance from the avionics and propulsion systems of the UAV. The magnetometer measures magnetic anomalies and the magnetic compensation magnetometer measures magnetic responses corresponding to the pitch, yaw and roll of the UAV. A data acquisition system stores and removes the magnetic response measurements from the magnetic anomaly measurements. The data acquisition system also stores a survey flight plan and transmits the same to the avionics system. The generator of the UAV is shielded and the propulsion system is stabilized to reduce magnetic and vibrational noises that can interfere with the operation of the magnetometer.

    Abstract translation: 无人机（UAV），用于获取在陆地或水上低空进行地球物理勘测的航空磁测数据，包括适合于保持和保持磁力计的扩展机身和磁补偿 磁力计与无人机的航空电子设备和推进系统距离最小。 磁力计测量磁异常，磁补偿磁强计测量与无人机的俯仰，偏航和滚转相对应的磁响应。 数据采集​​系统存储并从磁异常测量中去除磁响应测量结果。 数据采集​​系统还存储调查飞行计划并将其发送给航空电子系统。 无人机的发电机被屏蔽并且推进系统稳定以减少可能干扰磁力计操作的磁性和振动噪音。

    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES
    269.
    发明申请
    LAUNCH AND RECOVERY SYSTEM FOR UNMANNED AERIAL VEHICLES 审中-公开
    无人驾驶飞机的发射和恢复系统

    公开(公告)号：WO01007318A1

    公开(公告)日：2001-02-01

    申请号：PCT/US2000/020099

    申请日：2000-07-24

    IPC: B64C25/68 ,  B64C39/02 ,  B64D3/00 ,  B64F1/02 ,  B64F1/04 ,  B64F1/10

    CPC classification number: B64F1/02 ,  B64C25/68 ,  B64C39/024 ,  B64C2201/084 ,  B64C2201/104 ,  B64C2201/165 ,  B64C2201/182 ,  B64C2201/205 ,  B64D3/00 ,  B64F1/04 ,  B64F1/10

    Abstract: An improved method of launching and retrieving a UAV (Unmanned Aerial Vehicle) (10) is disclosed. The preferred method of launch involves carrying the UAV (10) up to altitude using a parasail (8) similar to that used to carry tourists aloft. The UAV is dropped and picks up enough airspeed in the dive to perform a pull-up into level controlled flight. The preferred method of recovery is for the UAV to fly into and latch onto the parasail tow line (4) or cables hanging off the tow line and then be winched back down to the boat (2).

    Abstract translation: 公开了一种发射和检索无人机（无人机）（10）的改进方法。 优选的发射方法是将无人机（10）运送到高度，使用类似于用来搭载高层游客的伞（8）。 无人机被丢弃，并在潜水中获得足够的空速，执行上升到等级控制飞行。 回收的首选方法是使UAV飞入并锁定在悬挂拖线（4）上或挂在拖绳上的电缆，然后被绞盘回到船（2）。

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