Integration of innovative ice protection systems into structure and their validation

The main purpose of this call is the integration of innovative Ice Protection systems in the structure: electromagnetic induction on composite material wing leading edges and two-phase system in the metallic engine air intake. The innovation and challenge is to find the most efficient design for the integration. In order to validate the selected technology solution, the development of Wind Tunnel Models, as well as Wind Tunnel tests in Icing conditions, of representative Nacelle and Wing and Flap Leading Edge surfaces with new Ice Protection Systems developed as technology lines within Airframe ITD framework shall be performed. Please refer to the full and formal topic descriptions published in this call.