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213 条记录 (耗时 0.021 秒)

    Apparatus for driving body with three-degree of freedom angular motion
    5.
    发明授权
    Apparatus for driving body with three-degree of freedom angular motion 有权
    具有三自由度角运动的车身驱动装置

    公开(公告)号：US07975467B2

    公开(公告)日：2011-07-12

    申请号：US11818029

    申请日：2007-06-13

    申请人： Sung-Jin Cho ,  Eul-Gon Kim ,  Hyung-Sik Lee

    发明人： Sung-Jin Cho ,  Eul-Gon Kim ,  Hyung-Sik Lee

    IPC分类号： F02K9/84

    CPC分类号： F02K9/84 ,  B64G1/401

    摘要： An apparatus for driving a body with 3-degree of freedom angular motion, comprises: a body connected to a fixing part so as to be rotatable centering around a pitch axis, a yaw axis, and a roll axis; a pitch axis driving unit for rotating the body centering around the pitch axis; and a yaw axis driving unit for rotating the body centering around the yaw axis. Since one of the pitch axis driving unit and the yaw axis driving unit restricts the body from rotating centering around the roll axis fixed to the body, the conventional roll-rotation restricting link is not needed between the body and the fixing part. Accordingly, a size of the apparatus is reduced.

    摘要翻译： 一种用于驱动具有3度自由度角运动的身体的装置，包括：主体，其连接到固定部分，以便能够围绕俯仰轴线，偏转轴线和侧倾轴线转动; 俯仰轴驱动单元，用于围绕俯仰轴线旋转体; 以及偏转轴驱动单元，用于围绕偏转轴线旋转身体。 由于俯仰轴驱动单元和偏航轴驱动单元之一限制了主体相对于固定在主体上的滚动轴线的中心旋转，因此在主体和固定部之间不需要传统的滚动旋转限制连杆。 因此，装置的尺寸减小。

    SYSTEM AND METHOD FOR MANEUVERING ROCKETS
    6.
    发明申请
    SYSTEM AND METHOD FOR MANEUVERING ROCKETS 审中-公开
    用于移动摇篮的系统和方法

    公开(公告)号：US20100275576A1

    公开(公告)日：2010-11-04

    申请号：US12772487

    申请日：2010-05-03

    申请人： Shaul Gutman ,  Benveniste Natan

    发明人： Shaul Gutman ,  Benveniste Natan

    IPC分类号： F02K9/08

    CPC分类号： F02K9/805 ,  F02K9/84 ,  F02K9/88

    摘要： A dual control system for a solid propellant propelled exoatmospheric kill-vehicle is disclosed. The system includes a primary solid propellant propulsion mechanism for controlling the propulsion of the kill-vehicle during a first phase of rocket flight, and a secondary solid propellant propulsion mechanism for maneuvering the kill-vehicle during a second phase of rocket flight. The primary propulsion mechanism controls the propulsion and direction of the kill-vehicle towards its target while the secondary propulsion mechanism may be used to provide lateral acceleration with a lower time-constant.

    摘要翻译： 公开了一种用于固体推进剂的双重控制系统，其推动了大气压灭火车辆。 该系统包括用于在火箭飞行的第一阶段期间控制杀伤车辆的推进的主固体推进剂推进机构和用于在第二阶段的火箭飞行期间操纵杀伤车辆的辅助固体推进剂推进机构。 主推进机构控制杀伤车辆向其目标的推进和方向，而次级推进机构可用于提供较低时间常数的横向加速度。

    Rocket engine having guide vanes in the nozzle of the engine
    7.
    发明申请
    Rocket engine having guide vanes in the nozzle of the engine 有权
    火箭发动机在发动机喷嘴中具有导向叶片

    公开(公告)号：US20070152096A1

    公开(公告)日：2007-07-05

    申请号：US10572862

    申请日：2004-09-14

    申请人： Erland Ørbekk

    发明人： Erland Ørbekk

    IPC分类号： F41G7/00

    CPC分类号： F02K9/88 ,  F02K9/84 ,  F42B10/663

    摘要： A rocket engine having guide vanes in the engine nozzle the guide vanes (2) being mounted for turning at or near the rearmost ends of fixed vanes (1) being parallel to the axis of the nozzle and protruding into the combustion chamber of the engine. The foremost ends (4) of the guide vanes (2) may be shielded by the rearmost ends of the fixed vanes (1), and the guide vanes (2) may be individually turnable.

    摘要翻译： 一种在发动机喷嘴中具有导向叶片的火箭发动机，所述导向叶片（2）被安装用于在固定叶片（1）的最后端处或其附近转动，该固定叶片平行于喷嘴的轴线并突出到发动机的燃烧室中。 导向叶片（2）的最前端（4）可以被固定叶片（1）的最后端部屏蔽，并且导向叶片（2）可以单独地转动。

    Device for preventing ball and socket joint from rolling
    8.
    发明申请
    Device for preventing ball and socket joint from rolling 有权
    防止球窝接头滚动的装置

    公开(公告)号：US20070117438A1

    公开(公告)日：2007-05-24

    申请号：US11590924

    申请日：2006-11-01

    申请人： Hwan-Gyu Lee ,  Sang-Youn Lee

    发明人： Hwan-Gyu Lee ,  Sang-Youn Lee

    IPC分类号： H01R11/22

    CPC分类号： F02K9/84 ,  F02K1/002 ,  Y10T403/32057 ,  Y10T403/32073 ,  Y10T403/32229 ,  Y10T403/32581

    摘要： The present invention provides an antirolling device of a ball and socket joint, which is to prevent the rolling movement of a moving body coupled to the ball effectively without hindering omnidirectional tilt rotational movement of the moving body, i.e. a moving part relative to the socket, a fixing part. Specifically, the antirolling device comprises: a bracket on the moving part (130) that is fixed to the circumference of the moving body; a guide channel (140) whose upper part is pivoted to the bracket on the moving part (130); a sliding bar (150) coupled to the guide channel in a way being possible to be slid thereinto; and a bracket on the fixing part (160) which is mounted on the fixing part and coupled with the lower part of the sliding bar.

    摘要翻译： 本发明提供了一种球窝接头的防滚动装置，其特征在于，不会妨碍移动体（即，相对于插座的移动部件）的全方向倾斜旋转运动， 固定部分。 具体地说，防盗装置包括：移动部件（130）上的支架，其固定在移动体的圆周上; 引导通道（140），其上部在所述移动部分（130）上枢转到所述支架; 以可能滑动的方式联接到所述引导通道的滑杆（150）; 以及固定部分（160）上的支架，其安装在固定部分上并与滑杆的下部连接。

    Variably angled propulsion/steering system
    10.
    发明申请
    Variably angled propulsion/steering system 审中-公开
    可变角度推进/转向系统

    公开(公告)号：US20050072876A1

    公开(公告)日：2005-04-07

    申请号：US10500258

    申请日：2002-12-26

    申请人： Ricardo Ducasse

    发明人： Ricardo Ducasse

    IPC分类号： B64C15/12 ,  B64C29/00 ,  B64D27/20 ,  B64D33/04 ,  F02K1/00 ,  F02K3/02 ,  F02K3/11 ,  F02K9/84 ,  B64B1/20

    CPC分类号： B64D33/04 ,  B64C15/12 ,  B64C29/0075 ,  B64D27/20 ,  F02K1/00 ,  F02K1/008 ,  F02K3/025 ,  F02K3/11 ,  F02K9/84

    摘要： An aircraft equipped with peripherally configured directional thrust capability has an onboard primary power source producing compressed air, and at least two thrust producing modules. Each thrust producing module has a fuel source and receives compressed air from the primary power source. Each module is attached to a respective rotatable support structure for independently varying the thrust angle of the thrust producing module with respect to the aircraft, all thrust producing modules being connected to a common controller for coordinated control of the aircraft.

    摘要翻译： 具有外围配置的方向推力能力的飞机具有产生压缩空气的至少一个主动力源和至少两个推力产生模块。 每个推力产生模块具有燃料源并且接收来自主电源的压缩空气。 每个模块附接到相应的可旋转支撑结构，用于独立地改变推力产生模块相对于飞机的推力角，所有推力产生模块连接到公共控制器以协调控制飞行器。