公开(公告)号：US07744039B2

公开(公告)日：2010-06-29

申请号：US11649706

申请日：2007-01-03

申请人： Richard B. Miles ,  Sergey O. Macheret ,  Mikhail Shneider ,  Alexandre Likhanskii ,  Joseph Steven Silkey

发明人： Richard B. Miles ,  Sergey O. Macheret ,  Mikhail Shneider ,  Alexandre Likhanskii ,  Joseph Steven Silkey

IPC分类号： B64C21/00

CPC分类号： B64C23/005 ,  B64C2039/105 ,  B64C2230/12 ,  B64D15/12 ,  F05D2270/172 ,  F15D1/12 ,  H05H1/2406 ,  Y02T50/12 ,  Y02T50/166

摘要： Systems and methods for controlling flow with electrical pulses are disclosed. An aircraft system in accordance with one embodiment includes an aerodynamic body having a flow surface exposed to an adjacent air stream, and a flow control assembly that includes a first electrode positioned at least proximate to the flow surface and a second electrode positioned proximate to and spaced apart from the first electrode. A dielectric material can be positioned between the first and second electrodes, and a controller can be coupled to at least one of the electrodes, with the controller programmed with instructions to direct air-ionizing pulses to the electrode, and provide a generally steady-state signal to the electrode during intervals between the pulses.

摘要翻译： 公开了用电脉冲控制流量的系统和方法。 根据一个实施例的飞行器系统包括具有暴露于相邻空气流的流动表面的空气动力体，以及流动控制组件，其包括至少邻近流动表面定位的第一电极和邻近并间隔开的第二电极 除了第一个电极。 介电材料可以位于第一和第二电极之间，并且控制器可以耦合到至少一个电极，其中控制器用指令编程以将空气电离脉冲引导到电极，并且提供一般的稳态 在脉冲之间的间隔期间向电极发出信号。