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 TERMINÉ 
Icing conditions are one of the most severe for aircraft and engines as experienced in the certification process and in-service events. Certification tests are never simple because icing phenomena is a very complex domain and designers have access to a very low level of prediction capability compare to other fields, mainly relying on a very fragmented knowledge based on empirical past experience. ...
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 15

 TERMINÉ 

Self-Healing Thermal Barrier Coatings (SAMBA)

Date du début: 1 mars 2013, Date de fin: 28 févr. 2017,

"This project deals with the creation of a new, unique self-healing thermal barrier coating (TBC) for turbines and other thermally loaded structures in order to realize a significant extension of the lifetime of critical high-temperature components. The concept is based on novel Al2O3 coated Mo-Si particles embedded in the TBC layer, typically consisting of yttria-stabilised zirconia. As the curre ...
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 9

 TERMINÉ 

Thermal Overall Integrated Conception of Aircraft (TOICA)

Date du début: 1 sept. 2013, Date de fin: 30 sept. 2016,

Thermal behaviour of aircraft has recently become a crucial subject due to many factors: increasing number of complex systems required by modern, more electric, commercial aircraft, the introduction of hotter engines with higher by-pass ratios, the increased use of composite material in aircraft structures, or the confinement of highly dissipative equipment and systems in smaller areas to earn spa ...
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 34

 TERMINÉ 

Enhanced material lifing model for rotating welded structures (LIFEMOD)

Date du début: 1 avr. 2013, Date de fin: 30 juin 2016,

"Green and sustainable engines require accurate and well documented material data for safe operation of the engines at optimum efficiency. The SAGE project aims at demonstrating open rotor engines and technologies to reduce fuel consumption, weight and increased efficiency of engine components. Structural integrity and safety of engine critical parts have to be considered with regard to design, ma ...
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 6