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Efficient, Modular and LigthWeight Electromagnetic Induction Based Ice Protection System


Final version of the exploitation plan
Periodic reports

A progress report will be produced every six months

Annual implementation plan

Definition of the annual implementation plan including technical and financial documents

Heating Elements + Power Electronics Laboratory Testing Report

This Document Deliverable will consist of two parts. In the one hand, the validation of the power electronics at full scale with laboratory chargers, and on the other hand, the validation of the ice protection module, the converter along with one coil pad at room temperature and also in climatic chamber.

Final version of the dissemination plan
Ice tunnel Test Results Analysis

This Document Deliverable will be prepared in collaboration with the Topic Manager who will be the responsible of the Ice Tunnel Tests. The tests will be summarized and the final conclusions will be included.

Heating Elements Laboratory Testing Report

This Document Deliverable will summarize the results of the test carried out both in room temperature with a thermal camera and in a climatic chamber with thermocouples. The heating speed and the heating distribution will be presented in the document.


Induction Application to Aircraft Ice Protection System

Author(s): Irma Villar, Ugaitz Iruretagoyena, Ana Cardenas, Francisco Redondo
Published in: 2019 IEEE Energy Conversion Congress and Exposition (ECCE), 2019, Page(s) 4201-4206, ISBN 978-1-7281-0395-2
Publisher: IEEE
DOI: 10.1109/ecce.2019.8912552

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