Electrostatic Voltage Sensors for Helicopter Dischargers,

Abstract

To maintain hovering helicopters at safe energy levels, a noncontacting electrostatic sensor is required to accurately determine the voltage on the aircraft relative to ground and provide proper control data to an active discharger for neutralizing hazardous charging conditions. Analytical model studies of a sphere suspended between two electrified ground planes and surrounded by space charge resulted in a theoretical relationship showing how charge density, excess surface charge, and external electric fields affect the voltage on the sphere. The electrostatic trends predicted from the theoretical analysis were sufficiently verified through independent large-scale laboratory experiments using empirical analysis techniques. From the theoretical and empirical analyses, helicopter charge equilibrium conditions were specified, together with a methodology for determining the electrostatic coefficients of full-scale hovering helicopters. The implications of the investigative program are that active electrostatic discharger systems are now feasible for helicopter applications. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1983
Accession Number
ADP002187

Entities

People

  • B. M. Duff
  • O. Tranbarger

Organizations

  • Southwest Research Institute

Tags

Communities of Interest

  • Air Platforms
  • Sensors
  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Charge Density
  • Electric Fields
  • Electricity
  • Electromagnetic Fields
  • Energy Levels
  • Helicopters
  • Hovering
  • Lightning
  • Space Charge
  • Static Electricity

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Electrical Engineering
  • Explosive Engineering.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster