| 发明名称 |
EMBEDDED DIELECTRIC STRUCTURES FOR ACTIVE FLOW CONTROL PLASMA SOURCES |
| 摘要 |
An aircraft active flow control dielectric barrier discharge (DBD) device may include a machinable ceramic dielectric support having an aerodynamic surface shaped to form an exposed flush part of an airfoil surface on an aircraft. The DBD device may include at least two electrodes configured to be oppositely charged and spaced apart from each other on the dielectric support. |
| 申请公布号 |
US2017088255(A1) |
申请公布日期 |
2017.03.30 |
| 申请号 |
US201514864796 |
申请日期 |
2015.09.24 |
| 申请人 |
The Boeing Company |
发明人 |
Nikic Dejan |
| 分类号 |
B64C23/00;B64F5/00 |
主分类号 |
B64C23/00 |
| 代理机构 |
|
代理人 |
|
| 主权项 |
1. An aircraft active flow control dielectric barrier discharge device, comprising:
a machinable ceramic dielectric support having an aerodynamic surface shaped to form an exposed flush part of an airfoil surface on an aircraft; and at least two electrodes configured to be oppositely charged and spaced apart from each other on the dielectric support. |
| 地址 |
Chicago IL US |
