Projects
There are 41 results.
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.
Hairmate - Hybrid Aircraft Seating Manufacturing and Testing
HAIRMATE project aims to design and manufacture moulds for manufacturing and testing the next generation aircraft seating obtained in the HAIRD project. Within the HAIRD project a new seating with reduction of Deep Vein Thrombosis (DVT) risk, multi-functionality and simple surfaces for composite manufacturing was designed. The moulds to manufacture the structural parts will be manufactured.
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.
IMAC PRO - Industrialized Manufacturing of CFRP Profiles
The technological objective of IMac-Pro is the development of a complete integrated process chain for the cost effective serial production of optimised CFRP stiffener profiles (e.g. frames, stringer, struts, floor beams, drive shafts,…) for all kinds of aircrafts (passenger planes, helicopters, fighters) based on textile technologies in combination with advanced injection and curing technologies.
Ice Grid - Investigation of Ice Formation on Protection Grids in Aircraft Air-Conditioning Systems
The IceGrid project examined protection grids in the air conditioning systems of passenger aircraft and at the interface to mobile climate modules on the ground for icing and de-icing. The methods used included both experimental testing in the icing wind tunnel and numerical simulations.
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.
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.
MET4LOWW - MET Potentials for Arrival and Departure Management
The objective of the MET4LOWW project is to derive ATM procedures for integrating partly probabilistic wind and weather information into arrival and departure management. Wind-fields and weather-objects are implemented in University of Salzburg’s ATM/ATC simulator, and associated avoidance and adaption strategies are developed. Various traffic and weather scenarios are analysed using fast-time-simulation and evaluated based on ATM performance figures for safety, capacity, cost-efficiency and environment. Based on these results the optimal ATM-procedures and meteorological information will be derived, e.g. time-based separation. The resulting potential improvements for arrival and departure management are validated by real-time simulation.
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.
MoVeTech - Model-Based Processing Technique for the Manufacturing of High-Quality Structural FRP Components for the Aerospace Industry
It is within the MoVeTech project that the concept of model-based processing technology was first implemented in the ARTM (Advanced Resin Transfer Moulding) process. This concept is based on the idea of combining phenomenologically based know-how about relevant mechanisms (heat conduction and transfer on moulds and composites, flow processes during mould filling or curing kinetics of reactive resins) in the form of mathematical models, and making them available at the level of process management - while adhering to real-time requirements.
OMOSA - Open Modular/Open Source Avionics Architecture for Remotely Piloted Aircraft Systems
OMOSA is researching the system architectures of avionics for small unmanned aerial vehicles, following the Integrated Modular Avionics (IMA) approach. By using commercial, modular hardware and open source software, aircraft electronics are to be developed. These can be used for flight control, as a navigation system, and as a C2 link. For this purpose, aircraft antennas integrated into the fuselage will also be included. The project results will be validated via a measurement campaign using a rotorcraft.
PROB4LOWW - Probabilistic MET Information for Capacity Optimisation in Arrival and Departure Management
In the proposed exploratory project, a concept for the integration of probabilistic meteorological information in arrival and departure management for capacity optimisation shall be devised. Flight planning and operation guidelines as well as detailed simulations of air traffic will be used to obtained a cost-loss ratio, which provides the basis to determine the optimal probability thresholds required to set arrival and departure rates at the occurrence of individual weather events.
ROPA - Radar Optical Piloted Aircraft
In order to ensure increased safety in flight, ROPA's research work is dedicated to the investigation and data fusion of various optical, infrared and radar sensor methods and procedures. The focus is on the identification of potential conflicts and strategies for collision avoidance as well as the integration and evaluation of the technology in an aircraft according to the EASA CS23 category.
SARISTU - Smart Intelligent Aircraft Structures
The concept of Smart Intelligent Aircraft Structures offers significant improvements in aircraft total weight, manufacturing cost and, above all, operational cost by an integration of system tasks into the load carrying structure. The project focuses on integration activities in the three distinct technological areas airfoil morphing, self-sensing and multifunctional structures through self-healing and the use of nanoreinforced resins.
SPARTA - Frame production in the RTM process for aviation applications
The project SPARTA tooling comprises the development of a cost- and energy efficient, automated resin transfer molding production process for aerospace fuselage frames. The big benefit of the process is the possibility for automation, shown in automation developments, and the outlook to high volume production feasibility.
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.
VertSLD - Prospecting for the Construction of a Vertical Icing Wind Tunnel for Experimental Simulation of Icing by Supercooled Large Droplets
The exploratory project VertSLD investigates both the physical feasibility and economic viability of an icing wind tunnel concept which avoids many of the difficulties that arise in existing icing wind tunnels when the size of the water droplets exceeds a few hundred microns. in this new concept the "flight path" of the drops within which they are supercooled is arranged vertically and not horizontally.
eSAFE - Emergency Safe Return for CS23 Aircraft
The aim of the project is the development of an automatic emergency flight guidance, including emergency landing for the EASA CS23 category aircraft. In case of sudden in-flight pilot incapacitation or technical problems, after activating the emergency button on board, an airfield with an approach route taking into account dynamic air traffic and weather data should be determined.
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.