Ice protection system based on two-phase heat transport technologies integrated in representative engine intake structure

Topic description

Specific Challenge:

The Call for Proposal deals with developing an ice protection system based on two-phase heat transport technologies. The objective is to increase aircraft efficiency by integrating the system within the structure (i.e. representative engine intake structure) and by replacing the traditional ice-protection that require energy from the A/C powerplant with passive devices. Please refer to the full and formal topic descriptions published in this call.