The invention discloses an annular ion wind propulsion device and an operation method thereof.The annular ion wind propulsion device comprises a support, a base, an annular emitter, an annular grounding end, a high-voltage power source and a wire, the annular emitter is connected with the high-voltage power source through the wire, and the annular grounding end is connected with the high-voltage power source through the wire; the annular emitting electrode and the annular grounding end are connected with the base through a first support. A plurality of discharge electrodes are arranged on the surface of the annular emitter to form a conductive layer, and the cross-sectional area of the connecting part of the bottom of each discharge electrode and the annular emitter is larger than that of the top of the discharge electrode. The discharge electrodes are uniformly distributed on the outer ring of the annular emitter, and the top tips of the discharge electrodes directly face the annular grounding end. According to the invention, through the arrangement of the annular structure, the ionic wind thrust between the annular emitter and the annular grounding end and the thrust near the annular emitter are superposed to form integral thrust multiplication, so that greater thrust can be realized through the ionic wind technology in a smaller size.

    本发明公开了一种环形离子风推进装置及其操作方法,包括支架、底座、环形发射极、环形接地端、高压电源和导线,所述环形发射极通过导线与高压电源连接,所述环形接地端通过导线与高压电源连接,所述环形发射极与环形接地端均通过第一支架与底座连接。所述环形发射极表面设置有若干个放电极构成导电层,所述放电极底部与环形发射极连接部位的截面面积大于放电极顶部截面面积。放电极均布环形发射极外圈,且放电极顶部尖端正对环形接地端。本发明通过设置环形结构,将环形发射极与环形接地端之间的离子风推力与环形发射极附近推力相叠加,形成整体推力倍增,可以在更小的尺寸内通过离子风技术实现更大的推力。


    Access

    Download


    Export, share and cite



    Title :

    Annular ion wind propulsion device and operation method thereof


    Additional title:

    一种环形离子风推进装置及其操作方法


    Contributors:
    QUAN RONGHUI (author) / ZHANG JIFAN (author) / HOU MIAOSEN (author) / ZHAO XIANG (author) / XIAO YAQI (author)

    Publication date :

    2024-10-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F03H PRODUCING A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR , Erzeugung von Vortriebskraft [Schub] nach dem Prinzip des Rückstoßes, soweit nicht anderweitig vorgesehen



    ANNULAR ELECTRIC PROPULSION DEVICE

    VASILEV VALENTIN FEDOROVICH / SHITOEV ALEKSANDR VIKTOROVICH / BUSHUEV ALEKSEJ VITALEVICH | European Patent Office | 2019

    Free access

    Ionic wind propulsion aircraft and propulsion method thereof

    WANG ZHIMING / ZHUANG SHUHONG / HUANG YOULING et al. | European Patent Office | 2020

    Free access

    WIND PROPULSION DEVICE

    AHN GYU JUNG / LEE TAE GOO / CHOI EUN JI | European Patent Office | 2025

    Free access

    WIND PROPULSION OPERATING SYSTEM FOR PROPELLING A VESSEL AND METHOD OF OPERATION THEREOF

    ANTIPPAS ALEX / AHLSTRÖM CHRISTOFFER / JOHANSSON NIKLAS | European Patent Office | 2024

    Free access

    WIND PROPULSION DEVICE

    AHN GYU JUNG / CHOI EUN JI / LEE TAE GOO et al. | European Patent Office | 2025

    Free access