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2. 发明授权

US07624941B1 Method of controlling aircraft, missiles, munitions and ground vehicles with plasma actuators 有权
标题翻译：用等离子执行器控制飞机，导弹，弹药和地面车辆的方法
公开(公告)号：US07624941B1
公开(公告)日：2009-12-01
申请号：US11415535
申请日：2006-05-02
申请人： Mehul Patel , Tom Corke
发明人： Mehul Patel , Tom Corke
IPC分类号： F41G7/00
CPC分类号： B64C23/005 , B62D35/007 , B64C2230/12 , F42B10/38 , F42B10/40 , F42B10/668 , Y02T50/166
摘要： The present invention relates to a method of controlling an aircraft, missile, munition or ground vehicle with plasma actuators, and more particularly to controlling fluid flow across their surfaces or other surfaces, which would benefit from such a method. The method includes the design of an aerodynamic plasma actuator for the purpose of controlling airflow separation over a control surface of a aircraft, missile, or a ground vehicle, and more particularly to the method of determining a modulation frequency for the plasma actuator for the purpose of fluid flow control over these vehicles. The various embodiments provide the steps to increase the efficiency of aircraft, missiles, munitions and ground vehicles. The method of flow control provides a means for reducing aircraft, missile's, munition's and ground vehicle's power requirements. These methods also provide alternate means for aerodynamic control using low-power hingeless plasma actuator devices.
摘要翻译：本发明涉及一种利用等离子体致动器来控制飞机，导弹，弹药或地面车辆的方法，更具体地涉及控制流过其表面或其它表面的流体流，这将从这种方法中受益。该方法包括为了控制在飞机，导弹或地面车辆的控制表面上的气流分离的空气动力学等离子体致动器的设计，并且更具体地涉及为此目的确定等离子体致动器的调制频率的方法对这些车辆进行流体流量控制。各种实施例提供了增加飞机，导弹，弹药和地面车辆的效率的步骤。流量控制方法为减少飞机，导弹，弹药和地面车辆的电力需求提供了一种手段。这些方法还提供了使用低功率无铰链等离子体致动器装置的空气动力学控制的替代方法。

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