发明名称 |
PLASMA ACTUATING PROPULSION SYSTEM FOR AERIAL VEHICLES |
摘要 |
A plasma propulsion nozzle incorporates a cylinder having an inlet and an outlet. A plurality of substantially cylindrical planarly disbanded electrodes with sandwiched dielectric spacers is cascaded in an array to be concentrically expanding from the inlet through an interior chamber to the outlet for a nozzle. A voltage source applies a periodic signal with rapidly reversing polarity to the electrodes with differential phase applied to adjacent electrodes in the array creating and expelling plasma clusters at each dielectric spacer inducing flow from the nozzle outlet to produce thrust.
|
申请公布号 |
US2013175405(A1) |
申请公布日期 |
2013.07.11 |
申请号 |
US201213346467 |
申请日期 |
2012.01.09 |
申请人 |
KHOZIKOV VYACHESLAV;LIU SHENGYI;THE BOEING COMPANY |
发明人 |
KHOZIKOV VYACHESLAV;LIU SHENGYI |
分类号 |
B64B1/36;F03H1/00;H05H1/54 |
主分类号 |
B64B1/36 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|