Airbus Helicopters to Test Hybrid, Electric Propulsion tech in New Flightlab

  • Our Bureau
  • 12:16 PM, January 27, 2021
  • 3437
Airbus Helicopters to Test Hybrid, Electric Propulsion tech in New Flightlab
Airbus Helicopters' Flying Laboratory

Airbus Helicopters has started in-flight tests on board its Flightlab, a platform-agnostic flying laboratory exclusively dedicated to maturing new technologies.

Airbus Helicopters intends to pursue the testing of hybrid and electric propulsion technologies with its Flightlab demonstrator, as well as exploring autonomy, and other technologies aimed at reducing helicopter sound levels or improving maintenance and flight safety.

The Flightlab provides an agile test bed to quickly test technologies that could later equip Airbus’ current helicopter range, and even more disruptive ones for future fixed-wing aircraft or (e)VTOL platforms.

Flight tests started last April when the demonstrator was used to measure helicopter sound levels in urban areas and to particularly study how buildings may affect people’s perception. First results show that buildings play an important role in masking or amplifying sound levels and these studies will be instrumental when the time comes for sound modeling and regulation setting, especially for Urban Air Mobility (UAM) initiatives.

Airbus Helicopters to Test Hybrid, Electric Propulsion tech in New Flightlab
Airbus Helicopters' Flying Laboratory Illustration

Testing was pursued in December to evaluate the Rotor Strike Alerting System (RSAS) aimed at alerting crews about the imminent risk of collision with the main and tail rotors.

Tests this year will include an image-detection solution with cameras to enable low altitude navigation, the viability of a dedicated Health and Usage Monitoring System (HUMS) for light helicopters, and an Engine Back-up System, which will provide emergency electric power in the event of a turbine failure.

Testing on the Flightlab will continue in 2022 in order to evaluate a new ergonomic design of intuitive pilot flight controls intended to further reduce pilot workload, which could be applicable to traditional helicopters as well as other VTOL formulas such as UAM.

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