Project description DEENESFRITPL Real-time measurement of air intake distortion in aero-engines Complex air intake designs for very high bypass ratio turbofans cause notable distortion at the fan face during aircraft take-off. This can adversely affect engine performance, structural integrity and safety margin, with potentially catastrophic consequences for the entire propulsion system. Current techniques for aero-engine testing and certification are limited by low spatial resolution and their intrusive nature. The EU-funded NIFTI project will overcome these challenges by developing a non-intrusive technique that should provide real-time data with at least one order of magnitude higher spatial resolution than current methods. Theoretical and experimental results are expected to help unlock the complex aerodynamics of closely coupled fan-intake systems and aid future designs of stall-tolerant aero-engines. Show the project objective Hide the project objective Objective Short and slim aero-engine intake designs for very high bypass ratio configurations cause notable levels of unsteady distortions at the fan face especially under cross-wind or angle of attack operation during aircraft take-off. Such distortions can adversely affect the engine’s performance, operability, structural integrity and safety margin with potentially catastrophic consequences for the entire propulsion system. Current practices for aero-engine testing and certification rely on a low number of intrusive pressure measurements at the fan face to characterise the distortion levels. Given the known limitations of currently used methods (low spatial resolution, intrusive nature) the existing technologies are inadequate to reduce the risk on the development and certification of future novel systems. NIFTI aims to address this gap by demonstrating a non-intrusive technique to measure velocity fields across a plane located upstream of a large diameter fan of a high bypass ratio aero-engine which has never been achieved. This method will provide synchronous datasets across the measurement plane with at least one order of magnitude higher spatial resolution than current methods. The implementation will demonstrate a highly automated and flexible multi-camera system within a representative industrial test environment. A number of more advanced, non-intrusive measuring technologies will be assessed such as 3D PTV or Helium Filled Soap Bubbles (HFSB) to further enhance the outputs of the selected baseline solution. The experimental activities will be supported by numerical campaigns and advanced data processing and flow analysis methods that will be used to analyse the highly unsteady nature of the flow distortions that will be measured during NIFTI’s experimental campaigns. These outcomes will ultimately unlock the complex aerodynamics of closely coupled fan-intake systems and aid the development of novel design rules for future, stall-tolerant aero-engines. Fields of science natural scienceschemical sciencesinorganic chemistrynoble gasesengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaeronautical engineeringnatural sciencescomputer and information sciencesdata sciencedata processing Keywords PIV PTV industrial wind tunnel tests isolated intake testing UHBR short intake PIV flexibility WT productivity fan distortion pressure from PIV advanced data analysis unsteady aerodynamics Programme(s) H2020-EU.3.4. - SOCIETAL CHALLENGES - Smart, Green And Integrated Transport Main Programme H2020-EU.3.4.5.1. - IADP Large Passenger Aircraft Topic(s) JTI-CS2-2018-CfP09-LPA-01-68 - Non-Intrusive Flow Field Measurement within a UHBR Intake Call for proposal H2020-CS2-CFP09-2018-02 See other projects for this call Funding Scheme RIA - Research and Innovation action Coordinator STICHTING DUITS-NEDERLANDSE WINDTUNNELS Net EU contribution € 1 414 324,00 Address VOORSTERWEG 31 8316 PR Marknesse Netherlands See on map Region Oost-Nederland Flevoland Flevoland Activity type Research Organisations Links Contact the organisation Opens in new window Website Opens in new window Participation in EU R&I programmes Opens in new window HORIZON collaboration network Opens in new window Total cost € 1 500 717,25 Participants (3) Sort alphabetically Sort by Net EU contribution Expand all Collapse all CRANFIELD UNIVERSITY United Kingdom Net EU contribution € 177 355,00 Address College Road MK43 0AL Cranfield - Bedfordshire See on map Region East of England Bedfordshire and Hertfordshire Central Bedfordshire Activity type Higher or Secondary Education Establishments Links Contact the organisation Opens in new window Website Opens in new window Participation in EU R&I programmes Opens in new window HORIZON collaboration network Opens in new window Total cost € 177 355,00 IMPERIAL COLLEGE OF SCIENCE TECHNOLOGY AND MEDICINE United Kingdom Net EU contribution € 119 753,00 Address SOUTH KENSINGTON CAMPUS EXHIBITION ROAD SW7 2AZ LONDON See on map Region London Inner London — West Westminster Activity type Higher or Secondary Education Establishments Links Contact the organisation Opens in new window Website Opens in new window Participation in EU R&I programmes Opens in new window HORIZON collaboration network Opens in new window Total cost € 119 753,75 LAVISION GMBH Germany Net EU contribution € 538 568,00 Address ANNA VANDENHOECK RING 19 37081 Goettingen See on map SME The organization defined itself as SME (small and medium-sized enterprise) at the time the Grant Agreement was signed. Yes Region Niedersachsen Braunschweig Göttingen Activity type Private for-profit entities (excluding Higher or Secondary Education Establishments) Links Contact the organisation Opens in new window Website Opens in new window Participation in EU R&I programmes Opens in new window HORIZON collaboration network Opens in new window Total cost € 538 568,75
