Abstract

This paper describes the design and implementation of a power electronics interface for a heat storage thermoelectric energy harvesting system. As an example of its application, the energy harvester was designed to supply power to a duty cycled wireless strain gauge sensing system for aircraft applications that typically consumes 28.5J per flight, with a peak power consumption of 100mW at 3.3V. The harvester, which will be mounted on the fuselage of an Airbus aircraft, generates a bipolar voltage due to a reversal in the polarity of the temperature difference across a thermoelectric generator at different parts of the flight cycle. For the target application, a peak generated voltage of ±1.2V across a matched load is expected, which requires rectification and regulation. The interface circuit consists of a cold-starting rectifier topology, a low-dropout regulator and a maximum power point tracking boost converter with a battery charging module. A prototype of a new and cold-starting rectifier topology was implemented using an H-bridge configuration of off-the-shelf depletion- and enhancement-mode MOSFETs. For a temperature cycle of +24°C to −27°C and back, spanning 80minutes, the interface circuit delivers 81J into a secondary Li-ion battery from a total generated energy of 126J. This corresponds to a measured average circuit efficiency of 64.3% for this example application.

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