Cel The proposed project aims at designing, manufacturing and building of a demonstrator for a new engine concept. The new concept replaces the usual turbine of a classical turboengine by a number of Pulse Detonation Combustors (PDC) placed on a disk that rotates under the tangential impulse provided by the exhaust jet of the PDC. The rotating disk is coupled, through a shaft, to the compressor that is placed upstream of the PDC in order to raise its inlet pressure. Two solutions will be considered for the engine propulsion: a propeller, coupled, via a gearbox, to the PDC shaft, or by using the reactive thrust of the PDC exhaust jet, directed at an optimal angle. The PDC inlet with be equipped with aerodynamic valves that control the air entrance into the PDC, thus allowing a significant increase in the detonation frequency, allowing for noise reduction and reduced dimensions. The demonstrator, consisting of a single, fixed, PDC equipped with a fuel injection and ignition system designed for the requirements of the engine concept, will be tested on an experimental facility in order to demonstrate the PDC capability to provide enough power to meet the requirements of the compressor, with sufficient reserve for powering to propel the host aircraft. The project also proposes the design and numerical simulation of the engine compressor, adapted to the requirements of the new engine, most importantly the high vibration load and oscillatory back pressure under which the compressor operates. A last objective of the project is to provide a full definition of the engine constructive solution and a numerical simulation of the flow through the engine that will allow the estimation of the engine performances. The new emerging technology is expected to provide a significant increase in the engine's thermodynamic cycle maximum temperature and efficiency, a drastic reduction in its weight and specific fuel consumption, and a decrease of greenhouse gas emissions. Dziedzina nauki engineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologyenvironmental engineeringenergy and fuels Program(-y) FP7-TRANSPORT - Specific Programme "Cooperation": Transport (including Aeronautics) Temat(-y) AAT.2012.6.3-1. - Breakthrough and emerging technologies Zaproszenie do składania wniosków FP7-AAT-2012-RTD-L0 Zobacz inne projekty w ramach tego zaproszenia System finansowania CP-FP - Small or medium-scale focused research project Koordynator INSTITUTUL NATIONAL DE CERCETARE-DEZVOLTARE TURBOMOTOARE - COMOTI Wkład UE € 220 150,00 Adres IULIU MANIU AVENUE 220D, SECTOR 6 061126 Bucharest 6 Rumunia Zobacz na mapie Region Macroregiunea Trei Bucureşti-Ilfov Bucureşti Rodzaj działalności Research Organisations Kontakt administracyjny Trifu Leonard (Mr.) Linki Kontakt z organizacją Opens in new window Strona internetowa Opens in new window Koszt całkowity Brak danych Uczestnicy (3) Sortuj alfabetycznie Sortuj według wkładu UE Rozwiń wszystko Zwiń wszystko MAX IV Laboratory, Lund University Szwecja Wkład UE € 195 680,00 Adres Paradisgatan 5c 22100 LUND Zobacz na mapie Region Södra Sverige Sydsverige Skåne län Rodzaj działalności Higher or Secondary Education Establishments Kontakt administracyjny Johan Revstedt (Prof.) Linki Kontakt z organizacją Opens in new window Strona internetowa Opens in new window Koszt całkowity Brak danych VON KARMAN INSTITUTE FOR FLUID DYNAMICS Belgia Wkład UE € 133 975,00 Adres Waterloose Steenweg, 72 1640 Sint-Genesius-Rode Zobacz na mapie Region Vlaams Gewest Prov. Vlaams-Brabant Arr. Halle-Vilvoorde Rodzaj działalności Research Organisations Kontakt administracyjny Dominick Hemeryck (Mr.) Linki Kontakt z organizacją Opens in new window Strona internetowa Opens in new window Koszt całkowity Brak danych INSTITUTUL DE FIZICA APLICATA Mołdawia Wkład UE € 50 000,00 Adres ACADEMIEI 5 MD2028 CHISINAU Zobacz na mapie Rodzaj działalności Research Organisations Kontakt administracyjny Cuciuc Tudor (Mr.) Linki Kontakt z organizacją Opens in new window Strona internetowa Opens in new window Koszt całkowity Brak danych