Calculation method of deposition electrostatic charging current for aircraft

TONG Chen; LI Hailong; SHANG Jiawei; DUAN Zemin; SI Xiaoliang; LI Zhibao; HUANG Yeyuan; SUN Guoqing; YAN Wei; QIU Shanliang

doi:10.13224/j.cnki.jasp.20220633

Volume 39 Issue 9

Sep. 2024

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TONG Chen, LI Hailong, SHANG Jiawei, et al. Calculation method of deposition electrostatic charging current for aircraft[J]. Journal of Aerospace Power, 2024, 39（9）：20220633 doi: 10.13224/j.cnki.jasp.20220633

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Calculation method of deposition electrostatic charging current for aircraft

doi: 10.13224/j.cnki.jasp.20220633

TONG Chen¹,
LI Hailong²,
SHANG Jiawei²,
DUAN Zemin^{1, 3, 4},
SI Xiaoliang^{3, 4},
LI Zhibao^{3, 4},
HUANG Yeyuan^{3, 4},
SUN Guoqing¹,
YAN Wei¹,
QIU Shanliang^{3, 4,*
,
,}

1.
School of Electrical Engineering and Automation，Hefei University of Technology，Hefei 230009，China
2.
Avionics System Design Institute，First Aircraft Design and Research Institute of Aviation Industry，Xi’an 710089，China
3.
Aviation Key Laboratory of Science and Technology on High Intensity Electromagnetic Environment Protection，Hefei 230031，China
4.
Anhui Provincial Aircraft Lightning Protection Laboratory，Hefei 230031，China

Received Date: 2022-08-29
Available Online: 2024-03-04

Abstract

Abstract

The effective area coefficient K was calculated using the concept of effective projected area. In Comsol software, the Spalart-Allmaras (S-A) turbulence model and particle drag model were used to improve the calculation formula in the standard, and a certain type of aircraft was used as an example to simulate the flow field and particle tracking. It was found that the larger particle diameter indicated the larger effective projected area; the higher flight speed indicated the more number of particle collisions; the charging current density increased with the rise of the cruising altitude. Finally, it was concluded that the maximum charging current density of the aircraft was 395 μA/m², which was very close to the actual observation value and the error was within 1.25%.
- deposition electrostatic,
- charging current density,
- aircraft,
- effective area coefficient,
- turbulence model

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References(23)

References

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Calculation method of deposition electrostatic charging current for aircraft

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