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TRIMIS

HIgh power and VOltage operation of electric MOTors in aeronautics

PROJECTS
Funding
European
European Union
Duration
-
Status
Ongoing
Geo-spatial type
Other
Total project cost
€1 001 775
EU Contribution
€1 001 775
Project Acronym
HIVOMOT
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Safety/Security
Transport sectors
Passenger transport,
Freight transport

Overview

Call for proposal
H2020-CS2-CFP11-2020-01
Link to CORDIS
Objectives

The present proposal tries to answer in the best way the call JTI-CS2-2020-CfP11-THT-12. After the analysis of the call, our understanding of the objectives requested by the call is as follows. The main objective of the project is to investigate solutions for the scientific and technical challenges regarding the use of high voltage high power electric drives at high altitude conditions. Both short and long term timeframes are contemplated, so research into the implications of high voltage and altitude in the reliability and safety of actual systems and its technical solution, but also investigation into new HTS based electric drives for these conditions are proposed.

For this purpose, this main objective splits into the following technical objectives:

  • Investigation on modelling of high voltage electrical systems at high altitude for fundamental understanding of the technical issues related to inverter-fed HV insulation and arcing effects in electrical machines.
  • Research into insulation approaches and assessment of their reliability and safety at high altitude conditions.
  • Electromagnetic, electrical, thermal and mechanical design of actual topologies of electrical machines in order to evaluate the limits of each technology for high power and high voltage operation in aircraft applications.
  • Comparison of available and foreseen HTS materials for their use in electric machines for high volumetric and mass power density.
  • Investigation on thermal management systems for cryo-cooled HTS windings for electric machines in aircraft environment.
  • Preliminary design and comparison of different HTS based electric machine topologies for aircraft applications at high voltage and high altitude in terms of power density, reliability and safety.
  • Full design of a HTS electric motor concept and development of a lab-scale validator, applying the most suitable techniques investigated during the project for HV and high altitude operation, including the thermal management.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.5.10. - Thematic Topics
Other Programme
JTI-CS2-2020-CFP11-THT-12 Advanced High Power Electrical Systems for High Altitude Operation

Partners

Lead Organisation
Organisation
Asociacion Centro Tecnologico Ceit
Address
PASEO MANUEL DE LARDIZABAL 15, 20018 SAN SEBASTIAN, Spain
Organisation website
EU Contribution
€273 359
Partner Organisations
Organisation
Alconza Berango Sl
Address
CALLE ARENE BIDEA 13, 48640 BERANGO, Spain
EU Contribution
€161 756
Organisation
Antec Magnets Sociedad Limitada
Address
AV RAMON Y CAJAL 74, 48920 PORTUGALETE, Spain
EU Contribution
€221 900
Organisation
Suprasys Sl
Address
AVENIDA LEHENDAKARI AGUIRRE 11 7 DEPTO 7, 48014 BILBAO, Spain
EU Contribution
€344 760

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Power electronics
Development phase
Validation

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