Projects
There are 7 results.
Aviation Icing Tests IV - Cloud Generation for Realistic Icing Tests on Aircraft Components, With and Without De-Icing or Anti-Icing Facilities
this research project will examine consequent research topics with a focus on increasing the LWC (Liquid Water Content) for Appendix C as well as the distribution and reduction of the LWC for Supercooled Large Drops (SLD). It is building on research projects Aviation Icing Tests, Aviation Icing Tests II and Aviation Icing Tests III that have already been carried out.
BISANCE - BIphasic System integrated in the Airframe of a NaCElle
The project intends to test in icing wind tunnel (IWT) one demonstrator of engine air intake integrated in a nacelle and equipped with an innovative biphasic heat transport system for regenerating the energy from the oil of the engine. The objective, by testing the technology in a representative environment, is to reach TRL5. At the end of the project the technology will be able to be further developed towards TRL6 to 9 with the final aim to be transferred to the aeronautic value chain.
DJET - D-JET Concept
The goal of the D-Jet project is to construct a small jet for an emerging market segment with a significantly lower price-performance ratio than earlier business jets, better performance with regard to the cruising speed and the rate of climb, short runway requirements for takeoff and landing, as well as a total registered weight under 2,000 kilograms.
FSA - Future Small Aircraft
The aim of this funded project is to launch a modern and highly efficient "Future Small Aircraft" in the general aviation category, which will reduce operating costs to a minimum and thus meet the growing demand. The end result of this project is a certifiable prototype, which will be developed in a timeframe of around 32 months.
HEMEP - Hybrid Electric Multi Engine Plane
The consortium partners in the HEMEP project aim to play a pioneering role in the field of aviation in electric propulsion systems, and thus enable the participating companies to become technology leaders for the future. The multi-engine aircraft with a hybrid electric propulsion system project will serve to further develop the basics of calculation methods in different areas for electric flying.
ICE GENESIS - Creating the Next Generation of 3D Simulation Means for Icing
The top level objective of the ICE GENESIS project is to provide the European aeronautical industry with a validated new generation of 3D icing engineering tools (numerical simulation and test capabilities), addressing App C, O and snow conditions, for safe, efficient and cost effective design and certification of future aircraft and rotorcraft.
I³PS - Integration of Innovative Ice Protection Systems
The project goal is to economically remove ice accreting on aircraft structure critical parts and thus increase reliability and mass saving on the global function. By comparison with the present existing solutions which are based on active pneumatic and electro-thermal means the targeted solutions will enable electrical power consumption, cost and mass reductions and ease the overall integration process.