Researchers with the EU-funded EPICEA project are developing computer tools that will help aircraft manufacturers better understand electromagnetic coupling mechanisms on composite electrical aircraft.
Today’s aircraft manufacturers, along with their supply chain, are focused on decreasing energy consumption, improving safety, and reducing emissions. “To optimise the performance of both existing and future generations of aircraft, many manufacturers are turning towards Composite Electrical Aircraft (CEA),” says Jean-Philippe Parmantier, EU coordinator of the EU and Canadian-funded EPICEA project. “These are essentially high-altitude, long distance aircraft made from lightweight composite materials that have airframes featuring a massive electrification of onboard functions and the deployment of low profile antennas generating less drag.”
Despite their potential, composite materials do not provide the fuselage with the same level of conductivity as aluminium does. As a result, composite aircraft suffer from an increased risk of electromagnetic (EM) hazard from radio broadcasts, satellites, radars or atmospheric electricity. Moreover, when flying at a very high altitude, there is an increased probability of being exposed to cosmic radiation (CR). “Specific electromagnetic protection measures are therefore required to guarantee electrical system immunity and the safety of the aircraft,” explains Parmantier. “However, such protective measures often result in an increase to the aircraft’s weight, thus jeopardising the emergence of energy-efficient CEAs.”
To make CEAs a viable option for improving aircraft performance, safety and efficiency, the EPICEA project – a joint R&D initiative between the EU and Canada – is working to develop computer tools to validate and verify a cooperative and open computer environment (i.e., the EPICEA platform). By modelling interconnected systems, antenna electromagnetic performances and the effects of CR on electronics, the resulting EPICEA platform will help aircraft manufacturers better understand EM coupling mechanisms on CEAs. This in turn will result in the creation of effective design requirements for aircraft systems and their integration onboard the aircraft.
Important results achieved
Although the EPICEA project remains a work-in-progress, several important results have already been achieved. “First and foremost, we have successfully plugged existing software into an overall simulation platform for modelling scenarios of EM-coupling on the interconnected wiring systems and EM performance antennas inside a complex composite fuselage,” says Parmantier.
“This gives us the capability to validate our simulation results with actual measurements on a full-scale composite barrel of a Bombardier Business Jet.”