Abstract

This paper presents the design of a multi-MHz inductive power transfer (IPT) system showcasing lightweight and energy-efficient solutions for non-radiative wireless power transfer. A proof of concept is developed by powering a drone without a battery that can hover freely in proximity to an IPT transmitter. The most challenging aspect, addressed here for the first time, is the complete system-level design to efficiently provide uninterrupted power flow while allowing for variable power demand and highly variable coupling factor. The proposed solution includes the design of lightweight air-core coils that can achieve sufficient coupling without degrading the aerodynamics of the drone, and the design of newly developed resonant power converters at both ends of the system. At the transmitting-end, a load-independent Class EF inverter, which can drive a transmitting-coil with constant current amplitude and achieves zero-voltage switching for the entire range of operation, was developed; and at the receiving-end, a hybrid Class E rectifier, which allows tuning for large changes in coupling and power demand, was used. For the demo, the range of motion of the drone was limited by a 7.5 cm nylon string tether, connected between the center of the transmitting-coil and the bottom of the drone. The design of the IPT system, including all the power conversion stages and the IPT link, is explained in detail. The results on performance and specific practical considerations required for the physical implementation are provided. An average end-to-end efficiency of 60% was achieved for a coupling range of 23%-5.8%. Relevant simulations concerning human exposure to electromagnetic fields are also included to assure that the demo is safe, according to the relevant guidelines. This paper is accompanied by a video featuring the proposed IPT system.

Highlights

  • T HE possibility of wirelessly powering electric unmanned aerial vehicles (UAVs) was first demonstrated in [1]

  • The means by which power was transferred to the UAV, hovering 15 m above the ground, was a 2.45-GHz microwave beam generated by a 5-kW magnetron, from which the UAV was able to pick up a maximum of 270 W

  • Encouraged by this impressive precedent from 1969, we developed a wireless power transfer system to wirelessly power a UAV, using not a microwave beam but inductive coupling, a non-radiative wireless power transfer solution that has been widely proposed to wirelessly charge electric vehicles [2]–[4]

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Summary

INTRODUCTION

T HE possibility of wirelessly powering electric unmanned aerial vehicles (UAVs) was first demonstrated in [1]. Solutions for variable coupling have been proposed for dynamic electric vehicle (EV) charging IPT systems that operate at kilohertz frequencies: Power throughput control is implemented either at the. The improvements in power capability, end-to-end efficiency, and tolerance to variable coupling have significantly increased the viability of implementing multi-MHz IPT systems for wireless charging in a variety of applications, an example of which is the wireless charging for UAVs. Considering the vast range of applications for UAVs [18], we developed a demo that is capable of wirelessly powering a drone without a battery, while it hovers close to a charging pad to showcase features that are beneficial, and in some cases necessary, to wirelessly power or charge dynamic loads, such as a hovering UAV.

SYSTEM OVERVIEW
IPT FOR SYSTEMS WITH VARIABLE COUPLING FACTOR
Effects of Variable Coupling on Output Power
Integration of a DC–DC Converter for Power Throughput Control
Electric Dynamics of the System
DESIGN OF THE IPT-LINK
Design of the IPT Coils
Range of Motion and Variable Coupling
SYSTEM DESIGN IN ACCORDANCE WITH ELECTROMAGNETIC EXPOSURE GUIDELINES
DESIGN OF THE RECTIFIER
VIII. DESIGN VERIFICATION AND MEASUREMENTS
System Simulation
OTHER DEMONSTRATIONS AND FUTURE WORK
Using Synchronous Rectification at the Receiving-End
Mounting the Transmitting-End on a Drone
Findings
CONCLUSION
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