CORDIS
EU research results

CORDIS

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Electromagnetic Platform for lightweight Integration/Installation of electrical systems in Composite Electrical Aircraft

Project information

Grant agreement ID: 689007

  • Start date

    1 February 2016

  • End date

    31 July 2019

Funded under:

H2020-EU.3.4.

  • Overall budget:

    € 1 749 920

  • EU contribution

    € 1 749 920

Coordinated by:

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

France

Objective

This three-and-a-half year project is to release, validate and verify a unique computer environment (i.e. the EPICEA platform) assimilating a complete understanding of electromagnetic (EM) issues on Composite Electric Aircraft (CEA – i.e. aircraft with composite and electric technologies combined and operating at higher altitude/latitude). EM on CEA includes EM coupling, interconnects, and Cosmic Radiations (CR) on electrical systems together with new concepts of antennas designed to maintain performance in composite environment without modifying aircraft aerodynamics. In EPICEA, CR, as parts of the EM spectrum, are considered as EM environmental hazards such as lightning or HIRF (High Intensity Radiated Fields). The targeted computer platform will support a decision making process for selection of the best strategy for the integration of electrical systems. Starting at a TRL3, the consortium will demonstrate a TRL4 at the end of the project.
The project will address numerous engineering issues, aiming at a significant reduction of energy consumption through more electrical aircraft and systems integration. If successful, it will create a more robust EM protection for electrical systems (i.e. lightweight, cost effective and safety compliant), a lighter and safer electrical system architecture for EM protected, less redundant, safety compliant, easy to maintain systems, a less drag on new systems of antennas while maintaining EM performance, and also will point to best possible health monitoring solutions. Used from the early design phase of electrical systems up to the architecture definition for installation and integration of electrical systems into CEA, the EPICEA outcome will limit the recourse to over conservative protection and unnecessary redundancy in integration architecture. This will overcome the weight penalty currently jeopardising the development of energy-efficient CEAs and will strengthen the aircraft safety.

Coordinator

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

Address

Chemin De La Huniere
91120 Palaiseau

France

Activity type

Research Organisations

EU Contribution

€ 660 858,75

Participants (4)

ARTTIC

France

EU Contribution

€ 185 687,50

AXESSIM SAS

France

EU Contribution

€ 340 000

FOKKER ELMO BV

Netherlands

EU Contribution

€ 275 093,75

I.D.S. - INGEGNERIA DEI SISTEMI - S.P.A.

Italy

EU Contribution

€ 288 280

Project information

Grant agreement ID: 689007

  • Start date

    1 February 2016

  • End date

    31 July 2019

Funded under:

H2020-EU.3.4.

  • Overall budget:

    € 1 749 920

  • EU contribution

    € 1 749 920

Coordinated by:

OFFICE NATIONAL D'ETUDES ET DE RECHERCHES AEROSPATIALES

France

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