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离子风无人机推进电极结构仿真OA

Simulation of Electrode Structures for Ion Wind-Propelled Unmanned Aerial Vehicles

中文摘要英文摘要

文章基于 COMSOL Multiphysics 有限元软件,研究电极结构及阵列对离子风有效推力和推功比的影响.首先分析平行放置电极结构下离子风的影响因素,确定较优参数,然后通过对比平行与交叉放置电极结构,发现相同电极间距下,交叉放置结构产生的有效推力更大,并进一步探究不同电极阵列结构,发现:阵列间距 40 mm 时,交叉放置阵列的有效推力和推功比分别比平行放置阵列提升 15.45%和 2.92%;间距 50 mm 时,交叉放置阵列比平行放置阵列的有效推力提升 27.6%,推功比仅下降 5.6%.可见,小阵列间距下,交叉放置阵列既能显著增强有效推力,又能保持较高推功比,适用于紧凑型离子风推进无人机的电极阵列结构设计,有助于提升无人机有效载荷.

Based on the COMSOL Multiphysics finite element software,the effects of electrode struc-tures and arrays on the effective thrust and thrust-to-power ratio of ion wind were studied.First,the influen-cing factors of ion wind under parallel-placed electrode structures were analyzed,and the optimal paramet-ers were determined.Then,the parallel-and cross-placed electrode structures were compared,and it was found that under the same electrode spacing,the cross-placed structure generated a greater effective thrust.Furthermore,different electrode array structures were explored,and the results show that at an array spa-cing of 40 mm,the effective thrust and thrust-to-power ratio of the cross-placed array increase by 15.45%and 2.92%,respectively,compared to those of the parallel-placed array;at a spacing of 50 mm,the effect-ive thrust of the cross-placed array increases by 27.6%,while its thrust-to-power ratio decreases by only 5.6%.It can be seen that under a small array spacing,the cross-placed array can significantly enhance the effective thrust and maintain a high thrust-to-power ratio,which is suitable for the electrode array design of compact ion wind-propelled unmanned aerial vehicles and helps to improve the effective payload of the un-manned aerial vehicles.

栗建科;康慧珍;潘珩;庞海龙

中国人民解放军联勤保障部队工程大学,天津 300161中国人民解放军联勤保障部队工程大学,天津 300161中国人民解放军联勤保障部队工程大学,天津 300161中国人民解放军联勤保障部队工程大学,天津 300161

数理科学

离子风推进电晕放电电极结构有效推力有效推功比

ion wind propulsioncorona dischargeelectrode structureeffective thrusteffective thrust-to-power ratio

《西华大学学报(自然科学版)》 2026 (4)

1-11,11

中国人民解放军联勤保障部队工程大学科研基金项目.

10.12198/j.issn.1673-159X.5984

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