Projects

There are 8 results.

open4aviation

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.

open4aviation

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.

open4aviation

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.

open4aviation

IceDrip - Aircraft Anti-icing and De-icing through Assemblies of Conducting Varnish and Functional Coatings

In the project IceDrip the rather promising concept of a discontinuous, electro-thermal de-icer is being investigated. The main aim of the present project is to significantly increase the already existing energetic advantages of the discontinuous de-icer by means of surface-active coatings, in order to achieve a performance range which would make the system suitable for general aviation aircraft, as well as smaller aircraft, which are equipped as large aircraft.

open4aviation

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.

open4aviation

MIXVAL - Mixer Simulation and Validation

In passenger aircraft, the mixing and distribution of humid airflow from the cabin and engines into the cockpit and passenger cabin, as well as electronic components, takes place at a central location of the air conditioning system, the mixer. So far, the flow and heat transfer processes and the ice formation and accretion cannot be calculated with sufficient accuracy. Therefore, the aim of this project is to develop a method for simulating the physical processes in the mixer.

open4aviation

TWID - Heating-Paint Sensor Based Wing Ice Detector

In the scope of the TWID project, a method for reliable detection of ice on wing surfaces and other relevant structures on an aircraft is to be developed, examined and validated in the course of various tests on the small-scale and full-scale models in the icing wind tunnel. Ice detection combined with the de-icing method, which is already in development, results in a completely self-sufficient de-icing system, which independently identifies and reliably removes ice on the wings.

open4aviation

eWING_DE-ICER - Development of an Energy-Efficient Electrothermal De-icing System for Wing Leading Edges in Aviation

Within the scope of the eWING_DE-ICER project, a method for developing energy-optimised de-icing systems for wing leading edges, based on a thermoelectric heating system, is to be developed. In addition to the development of forecasting models for the optimal design of all components involved, different prototypes are to be set up as in the model, as well as in full-scale, and tested in various icing wind tunnels.