Objetivo The overall objective of the project is to design, develop; manufacture and flight qualify a novel heat exchanger for oil cooling in the transmission system of a civil Tilt Rotor aircraft. The proposed solution will outperform a conventional plate-fin heat exchanger in terms of efficiency, volume, weight, robustness, reliability and will fully integrate into the transmission systems architecture. The concept underpinning this project is to build upon Marston Aerospace’s long history of innovation within heat transfer and fluids management systems by forming an integrated project team. The team will consist of thermal modellers, mechanical design, manufacturing, experimentalists and R&D experts in order to propose three initial air cooled oil cooler designs based on different manufacturing technologies. These will be conventional plate and fin corrugated heat exchanger; chemically etched plate and pin and an additive layer manufacturing solution utilising a novel architecture. An assumption would be that the material which would be most appropriate, in terms of technology readiness and for each proposed manufacturing process the suitability would be aluminium and that the new designs will be directly compared to each other in order to select the most viable design to take forward through to prototype manufacture towards flight demonstration testing. Ámbito científico ingeniería y tecnologíaingeniería eléctrica, ingeniería electrónica, ingeniería de la informacióningeniería electrónicasistemas de automatización y controlingeniería y tecnologíaingeniería mecánicaingeniería de fabricaciónfabricación sustractivaingeniería y tecnologíaingeniería mecánicaingeniería de vehículosingeniería aeroespacialaeronavegiroaviónciencias naturalesmatemáticasmatemáticas purasgeometríaingeniería y tecnologíaingeniería mecánicaingeniería de fabricaciónfabricación aditiva Palabras clave Heat Exchanger chemical etching additive layer manufacturing air cooled liquid cooler Programa(s) H2020-EU.3.4. - SOCIETAL CHALLENGES - Smart, Green And Integrated Transport Main Programme H2020-EU.3.4.5.3. - IADP Fast Rotorcraft Tema(s) JTI-CS2-2015-CFP02-FRC-01-05 - Design, development and flight qualification of a novel, integrated high efficiency heat exchanger for tiltrotor transmission oil cooling Convocatoria de propuestas H2020-CS2-CFP02-2015-01 Consulte otros proyectos de esta convocatoria Régimen de financiación IA - Innovation action Coordinador HS MARSTON AEROSPACE LIMITED Aportación neta de la UEn € 331 023,00 Dirección Wobaston road fordhouses WV10 6QJ Wolverhampton Reino Unido Ver en el mapa Región West Midlands (England) West Midlands Wolverhampton Tipo de actividad Private for-profit entities (excluding Higher or Secondary Education Establishments) Enlaces Contactar con la organización Opens in new window Participación en los programas de I+D de la UE Opens in new window Red de colaboración de HORIZON Opens in new window Otras fuentes de financiación € 141 867,00