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136 条记录 (耗时 0.077 秒)

    Hierarchical closed-loop control system for aircraft, missiles and munitions
    31.
    发明授权
    Hierarchical closed-loop control system for aircraft, missiles and munitions 有权
    用于飞机，导弹和弹药的分层闭环控制系统

    公开(公告)号：US08548650B1

    公开(公告)日：2013-10-01

    申请号：US13455182

    申请日：2012-04-25

    申请人： Troy S. Prince ,  Richard Kolacinski ,  Mehul Patel

    发明人： Troy S. Prince ,  Richard Kolacinski ,  Mehul Patel

    IPC分类号： B64C13/00 ,  F41G7/00 ,  G01C23/00

    CPC分类号： G05D1/107 ,  F42B10/38 ,  F42B10/40 ,  F42B10/42 ,  F42B10/668 ,  F42B15/01

    摘要： The present invention relates to a missile or munition with a hierarchical, modular, closed-loop flow control system, more particularly to aircraft or munition with flow control system for enhanced aerodynamic control, maneuverability and stabilization. The present invention further relates to a method of operating the flow control system.Various embodiments of the flow control system involve elements including flow sensors, active flow control devices or activatable flow effectors, and logic devices with closed loop control architecture. The sensors are used to estimate or determine flow conditions on the surfaces of a missile or munition. The active flow control device or activatable flow effectors create on-demand flow disturbances, preferably micro-disturbances, at different points along the various aerodynamic surfaces of the missile or aircraft to achieve a desired stabilization or maneuverability effect. The logic devices are embedded with a hierarchical control structure allowing for rapid, real-time control at the flow surface.

    摘要翻译： 本发明涉及具有分级，模块化，闭环流量控制系统的导弹或弹药，更具体地涉及具有用于增强的空气动力学控制，机动性和稳定性的流量控制系统的飞机或弹药。 本发明还涉及一种操作流量控制系统的方法。 流量控制系统的各种实施例涉及包括流量传感器，主动流量控制装置或可激活流动效应器以及具有闭环控制架构的逻辑装置的元件。 传感器用于估计或确定导弹或弹药表面的流动状况。 主动流量控制装置或可激活流动效应器沿着导弹或飞行器的各种空气动力学表面在不同点处产生按需的流动干扰，优选微扰动，以实现期望的稳定性或机动性效果。 逻辑器件嵌入了分层控制结构，允许在流表面进行快速，实时的控制。

    Aircraft, missile, projectile, or underwater vehicle with reconfigurable control surfaces
    32.
    发明授权
    Aircraft, missile, projectile, or underwater vehicle with reconfigurable control surfaces 失效
    飞机，导弹，射弹或水下车辆与可重构控制面

    公开(公告)号：US08367992B1

    公开(公告)日：2013-02-05

    申请号：US12977519

    申请日：2010-12-23

    申请人： Mehul Patel ,  T Terry Ng ,  Alan B Cain ,  Zak Sowle ,  Jack DiCocco

    发明人： Mehul Patel ,  T Terry Ng ,  Alan B Cain ,  Zak Sowle ,  Jack DiCocco

    IPC分类号： F42B10/02 ,  B64C3/54

    CPC分类号： F42B10/64 ,  F41G7/20 ,  F42B3/006 ,  F42B10/02 ,  F42B15/00 ,  F42B15/01 ,  F42B15/36 ,  F42B19/01

    摘要： The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and a method for increasing the maneuverability or stability of an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to a method for increasing the maneuverability or stability of an aircraft, missile, underwater vehicle or projectile through the use of removable control surfaces. The technical advantage of the removable control surface system (or “removable control surface”) over other systems is that the removable control surface system enables the aircraft, missile, underwater vehicle or projectile to have two or more design configurations, each configuration being tailored to the aircraft, missile, projectile, or underwater vehicle's specific stability or maneuverability requirements during a specific portion of the flight.

    摘要翻译： 本发明涉及一种具有改进的控制系统的飞机，导弹，射弹或水下车辆，以及用于增加飞机，导弹，射弹或水下航行器的机动性或稳定性的方法。 更具体地说，本发明涉及通过使用可拆卸的控制表面来提高飞机，导弹，水下航行器或射弹的机动性或稳定性的方法。 可移动控制表面系统（或可移除控制面）在其他系统上的技术优点在于，可移动控制面系统使得飞机，导弹，水下航行器或射弹能够具有两个或多个设计配置，每个配置适合飞机 ，导弹，射弹或水下航行器在特定部分飞行过程中的具体稳定性或机动性要求。

    Aircraft and missile afterbody flow control device and method of controlling flow
    33.
    发明授权
    Aircraft and missile afterbody flow control device and method of controlling flow 有权
    飞机和导弹后体流量控制装置及流量控制方法

    公开(公告)号：US08191833B1

    公开(公告)日：2012-06-05

    申请号：US11415534

    申请日：2006-05-02

    申请人： Jack DiCocco ,  Troy Prince ,  Mehul Patel ,  Tsun Ming Terry Ng

    发明人： Jack DiCocco ,  Troy Prince ,  Mehul Patel ,  Tsun Ming Terry Ng

    IPC分类号： B64C21/00

    CPC分类号： B64C21/00 ,  B64C5/12 ,  F41G7/00 ,  F42B10/14 ,  F42B10/60 ,  F42B10/62 ,  F42B15/01 ,  G05D1/0088

    摘要： The present invention relates to an afterbody flow control system and more particularly to aircraft or missile flow control system for enhanced maneuverability and stabilization. The present invention further relates to a method of operating the flow control system.In one embodiment, the present invention includes a missile or aircraft comprising an afterbody and a forebody; at least one activatable flow effector on the missile or aircraft afterbody; at least one sensor each having a signal, the at least one sensor being positioned to detect forces or flow conditions on the missile or aircraft afterbody; and a closed loop control system; wherein the closed loop control system is used for activating and deactivating the at least one activatable flow effector based on at least in part the signal of the at least one sensor.

    摘要翻译： 本发明涉及后体流量控制系统，更具体地涉及用于增强机动性和稳定性的飞机或导弹流量控制系统。 本发明还涉及一种操作流量控制系统的方法。 在一个实施例中，本发明包括一个包括后身体和前体的导弹或飞机; 在导弹或飞机后身上至少有一个可激活的流动执行器; 每个具有信号的至少一个传感器，所述至少一个传感器被定位成检测导弹或飞机后身上的力或流动状况; 和闭环控制系统; 其中所述闭环控制系统用于至少部分地基于所述至少一个传感器的信号来激活和去激活所述至少一个可激活的流动效应器。

    Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces
    35.
    发明授权
    Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces 有权
    飞机，导弹，射弹或水下车辆与可重构控制面

    公开(公告)号：US07880125B1

    公开(公告)日：2011-02-01

    申请号：US12077447

    申请日：2008-03-19

    申请人： Mehul Patel ,  T. Terry Ng ,  Alan B. Cain ,  Zak Sowle ,  Jack DiCocco

    发明人： Mehul Patel ,  T. Terry Ng ,  Alan B. Cain ,  Zak Sowle ,  Jack DiCocco

    IPC分类号： F42B15/01

    CPC分类号： F42B10/64 ,  F41G7/20 ,  F42B3/006 ,  F42B10/02 ,  F42B15/00 ,  F42B15/01 ,  F42B15/36 ,  F42B19/01

    摘要： The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and an improved control system for maneuvering an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, underwater vehicle or projectile with removable control surfaces. The technical advantage of the removable control surface system (or “removable control surface”) over other systems is that the removable control surface system enables the aircraft, missile, underwater vehicle or projectile to have two or more design configurations, each configuration being tailored to the aircraft, missile, projectile, or underwater vehicle's specific stability or maneuverability requirements during a specific portion of the flight.

    摘要翻译： 本发明涉及具有改进的控制系统的飞机，导弹，射弹或水下航行器，以及用于操纵飞机，导弹，射弹或水下航行器的改进的控制系统。 更具体地，本发明涉及具有可移除控制表面的飞机，导弹，水下航行器或射弹。 可移动控制表面系统（或“可移除控制表面”）在其他系统上的技术优点是可移动控制表面系统使得飞机，导弹，水下航行器或射弹能够具有两个或多个设计配置，每个配置被定制为 飞机，导弹，射弹或水下航行器在特定部分飞行过程中的具体稳定性或机动性要求。

    Aircraft, missile, projectile or underwater vehicle with improved control system
    36.
    发明授权
    Aircraft, missile, projectile or underwater vehicle with improved control system 失效
    飞机，导弹，射弹或水下车辆具有改进的控制系统

    公开(公告)号：US07709772B1

    公开(公告)日：2010-05-04

    申请号：US11292972

    申请日：2005-12-02

    申请人： Mehul Patel ,  T. Terry Ng ,  Alan B. Cain ,  Zak Sowle ,  Jack DiCocco

    发明人： Mehul Patel ,  T. Terry Ng ,  Alan B. Cain ,  Zak Sowle ,  Jack DiCocco

    IPC分类号： F42B15/01

    CPC分类号： F42B10/64 ,  F41G7/20 ,  F42B3/006 ,  F42B10/02 ,  F42B15/00 ,  F42B15/01 ,  F42B15/36 ,  F42B19/01

    摘要： The present invention relates to an aircraft, missile, projectile, or underwater vehicle with an improved control system and an improved control system for maneuvering an aircraft, missile, projectile, or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, underwater vehicle or projectile with removable control surfaces. The technical advantage of the removable control surface system (or “removable control surface”) over other systems is that the removable control surface system enables the aircraft, missile, underwater vehicle or projectile to have two or more design configurations, each configuration being tailored to the aircraft, missile, projectile, or underwater vehicle's specific stability or maneuverability requirements during a specific portion of the flight.

    摘要翻译： 本发明涉及具有改进的控制系统的飞机，导弹，射弹或水下航行器，以及用于操纵飞机，导弹，射弹或水下航行器的改进的控制系统。 更具体地，本发明涉及具有可移除控制表面的飞机，导弹，水下航行器或射弹。 可移动控制表面系统（或“可移除控制表面”）在其他系统上的技术优点是可移动控制表面系统使得飞机，导弹，水下航行器或射弹能够具有两个或多个设计配置，每个配置被定制为 飞机，导弹，射弹或水下航行器在特定部分飞行过程中的具体稳定性或机动性要求。

    Methods and apparatus for swipe or presentation image scanning
    39.
    发明授权
    Methods and apparatus for swipe or presentation image scanning 有权
    扫描或呈现图像扫描的方法和装置

    公开(公告)号：US07367509B2

    公开(公告)日：2008-05-06

    申请号：US11025817

    申请日：2004-12-29

    申请人： Mehul Patel ,  Thomas Bianculli ,  Edward Barkan

    发明人： Mehul Patel ,  Thomas Bianculli ,  Edward Barkan

    IPC分类号： G06K7/10

    CPC分类号： G06K7/10732 ,  G06K7/109

    摘要： Methods and apparatus for swipe image scanning comprising a scan stand and an imaging scanner. An exemplary scan stand comprises an illumination module and a receiving structure to receive the imaging scanner. Other embodiments further comprise a scan module, an illumination module, a processing unit, a detection component and memory. In an embodiment, the scan stand illuminates target dataforms brighter than the illumination from the scanner allowing for shorter exposure times and improved scanner performance.

    摘要翻译： 用于扫描图像扫描的方法和装置，包括扫描架和成像扫描仪。 示例性的扫描支架包括照明模块和用于接收成像扫描器的接收结构。 其他实施例还包括扫描模块，照明模块，处理单元，检测部件和存储器。 在一个实施例中，扫描架照亮比来自扫描仪的照明更亮的目标数据形式，允许更短的曝光时间和改进的扫描仪性能。