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Massachusetts Institute of Technology

Methods of Aircraft Charge Control During Flight

Abstract

dc:description.abstract

The accumulation of aircraft electrical charge can impact lightning initiation, cause radio interference, or make it difficult for research aircraft to make accurate measurements of atmospheric electric fields. Two experimental campaigns are described in this thesis that relate to the control of net electrical charge on aircraft, and the associated physical phenomena. First, a successful flight demonstration of actively controlled charging in fair weather conditions is described. A corona discharge wire is used for remote charging of a 1.9 m wingspan plane to both positive and negative polarities. By applying a voltage between -13 and +13 kV to the wire, the plane charged to +23 and -30 kV, respectively. The system demonstrates comparable results to previous modeling and wind tunnel experiments, which showed an increase in plane potential and a decrease in corona current as wind speed increased. There are technological limitations to the charge control strategy, such as a saturation voltage due to spurious corona and the delicacy of the corona wire. The second experiment is the study of the behavior of streamer corona discharges in wind. A point-to-plane geometry is used to provide a baseline to compare to precipitation static (p-static) dischargers, which are in use on most airplanes today. We find that the discharge characteristics are strongly influenced by the wind: the frequency of pulsations and the average current increase with wind speed, but both become less consistent. In general, two types of streamer bursts emerged upon adding wind: first, the streamers tended to point with the wind especially at lower wind speeds and higher voltages; at higher wind speeds and lower voltages, the streamer bursts tend to point against the wind. To the authors knowledge, this phenomenon has not been experimentally observed before.

Degree

thesis:*
Name thesis:degree_name
Master
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2021

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Martell, Benjamin C.
Advisor dc:contributor.advisor
  • Guerra-Garcia, Carmen

Rights

dc:rights
Statement dc:rights
  • In Copyright - Educational Use Permitted
  • Copyright MIT

Identifiers

dc:identifier.*
Handle dc:identifier.uri
https://hdl.handle.net/1721.1/139140
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/139140

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Martell, Benjamin C.. Methods of Aircraft Charge Control During Flight. Massachusetts Institute of Technology, 2021. https://hdl.handle.net/1721.1/139140