Empirical Study of Ground Proximity Effects for Small-scale Electroaerodynamic Thrusters
Grant Nations, C. Luke Nelson, Daniel S. Drew

TL;DR
This empirical study investigates how ground proximity affects the performance of small-scale electroaerodynamic thrusters, revealing significant thrust enhancements at close distances and dependencies on geometric parameters, aiding indoor robot propulsion.
Contribution
First empirical analysis of ground proximity effects on small electroaerodynamic thrusters, identifying key geometric factors influencing thrust enhancement for indoor robotic applications.
Findings
Peak thrust increased by 300-600% at 0.2 mm ground distance.
Thrust increased by up to 20% at centimeter distances.
Ground proximity effects depend on thruster geometry and configuration.
Abstract
Electroaerodynamic (EAD) propulsion, where thrust is produced by collisions between electrostatically-accelerated ions and neutral air, is a potentially transformative method for indoor flight owing to its silent and solid-state nature. Like rotors, EAD thrusters exhibit changes in performance based on proximity to surfaces. Unlike rotors, they have no fragile and quickly spinning parts that have to avoid those surfaces; taking advantage of the efficiency benefits from proximity effects may be a route towards longer-duration indoor operation of ion-propelled fliers. This work presents the first empirical study of ground proximity effects for EAD propulsors, both individually and as quad-thruster arrays. It focuses on multi-stage ducted centimeter-scale actuators suitable for use on small robots envisioned for deployment in human-proximal and indoor environments. Three specific effects…
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Taxonomy
TopicsAerosol Filtration and Electrostatic Precipitation · Electrohydrodynamics and Fluid Dynamics
