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    Aircraft, missile, projectile or underwater vehicle with improved control system and method of using
    1.
    发明授权
    Aircraft, missile, projectile or underwater vehicle with improved control system and method of using 有权
    飞机，导弹，射弹或水下车辆具有改进的控制系统和使用方法

    公开(公告)号：US08809755B1

    公开(公告)日：2014-08-19

    申请号：US11292533

    申请日：2005-12-02

    申请人： Mehul Patel ,  T. Terry Ng ,  Paul Suchy

    发明人： Mehul Patel ,  T. Terry Ng ,  Paul Suchy

    IPC分类号： F42B10/12 ,  B64C5/10

    CPC分类号： F42B10/12 ,  B64C9/02 ,  B64C9/08 ,  F42B15/01 ,  F42B19/06

    摘要： The present invention relates to an aircraft, missile, projectile or underwater vehicle with an improved control system, an improved control system and a method of maneuvering an aircraft, missile, projectile or underwater vehicle. More particularly, the present invention relates to an aircraft, missile, projectile or underwater vehicle with control surfaces that are movable along a track. The present invention further relates to a method of controlling a aircraft, missile, projectile or underwater vehicle using such a control system. One of the technical advantages of the control system on a track (or “tracked control surface”) over other aircraft, missile, projectile or underwater vehicle control systems is that the tracked control surface system enables the aircraft, missile, projectile or underwater vehicle to have an unlimited number of configurations, each configuration being tailored to the 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，改进的控制系统和操纵飞机，导弹，射弹或水下航行器的方法。 更具体地，本发明涉及一种具有可沿着轨道移动的控制表面的飞机，导弹，射弹或水下车辆。 本发明还涉及使用这种控制系统来控制飞机，导弹，射弹或水下车辆的方法。 控制系统在其他飞机，导弹，射弹或水下航行器控制系统上的轨道（或“跟踪控制面”）上的技术优点之一是跟踪的控制面系统使飞机，导弹，射弹或水下航行器能够 具有无限数量的配置，每个配置根据特定部分飞行期间的具体稳定性或机动性要求进行定制。

    Vortex generation for control of the air flow along the surface of an airfoil
    4.
    发明授权
    Vortex generation for control of the air flow along the surface of an airfoil 失效
    用于控制沿翼面表面的气流的涡旋生成

    公开(公告)号：US06302360B1

    公开(公告)日：2001-10-16

    申请号：US09480198

    申请日：2000-01-10

    申请人： T. Terry Ng

    发明人： T. Terry Ng

    IPC分类号： B64C1316

    CPC分类号： B64C23/06 ,  B64C2230/04 ,  B64C2230/06 ,  Y02T50/162 ,  Y02T50/166

    摘要： Apparatus for generating vortices to control the flow of air across a airfoil of an aircraft includes a series of pressure active regions arranged along the leading edge of the airfoil. The pressure active regions include spaced apart valves connected to a source of vacuum, a controller for activating the valves, and sensors for sensing air pressure. The controller is configured to activate the valves in response to the pressure sensed by the sensors, wherein the spaced apart valves are connected to a source of pressurized air as well as to the source of vacuum.

    摘要翻译： 用于产生涡流以控制穿过飞行器的翼型件的空气流的装置包括沿翼型的前缘布置的一系列压力有源区域。 压力活动区域包括连接到真空源的间隔开的阀，用于启动阀的控制器和用于感测空气压力的传感器。 控制器被配置为响应于由传感器感测到的压力来激活阀，其中间隔开的阀连接到加压空气源以及真空源。

    Aircraft, missile, projectile or underwater vehicle with reconfigurable control surfaces
    6.
    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
    7.
    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。