DUCTED ELECTROAERODYNAMIC THRUSTERS
    1.
    发明申请

    公开(公告)号:WO2023059413A1

    公开(公告)日:2023-04-13

    申请号:PCT/US2022/042437

    申请日:2022-09-02

    Abstract: Electroaerodynamic devices and their methods of operation are disclosed. In one embodiment, ions are formed by dielectric barrier discharge using a time-varying voltage differential applied between a first electrode and a second electrode. The ions are then accelerated in a downstream direction using a second voltage differential applied between a third electrode and the first and/or second electrodes, where the third electrode is located downstream from the first and second electrodes. The ions may then collide with naturally charged molecules and/or atoms within a fluid to accelerate the fluid in the downstream to create an ionic wind and an associated thrust.

    ELECTROAERODYNAMIC DEVICES
    2.
    发明申请

    公开(公告)号:WO2020247031A1

    公开(公告)日:2020-12-10

    申请号:PCT/US2020/015446

    申请日:2020-01-28

    Abstract: Electroaerodynamic devices and their methods of operation are disclosed. In one embodiment, ions are formed by dielectric barrier discharge using a time varying voltage differential applied between a first electrode and a second electrode. The ions are then accelerated in a downstream direction using a second voltage differential applied between a third electrode and the first and/or second electrodes, where the third electrode is located down stream from the first and second electrodes. The ions may then collide with naturally charged molecules and/or atoms within a fluid to accelerate the fluid in the downstream to create an ionic wind and an associated thrust.

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