Objective The general context is to use morphing wings with e.g. droop nose and morphing trailing edge instead of the classical high-lift systems like slats and flaps since these last ones are expensive, complex and heavy, and are therefore not acceptable solutions for the current trends on efficient and green aircrafts. A solution based on morphing wing technology overcomes these limitations. A demonstrator (physical prototype) of a full morphing wing is available today. The specific objective of the present project is to investigate an efficient methodology that will be used to develop a high fidelity flexible and non-linear MBS-FEM model of a morphing wing including several structural components (composite box, morphing winglet and wingtip, droop nose and morphing adaptive trailing edge), with flexible parts (compliant mechanisms and flexible skins), kinematic joints, sensors, actuators and control devices included in the model. This model will be confronted to tests results on physical prototypes and it will be fine-tuned to conform to the tests. This MBS-FEM model will be a companion of the physical prototype, since it can be used to assess the structural performances and behavior in different configurations, the mechanical system functionalities, verify the actuation and control chain, when testing on physical prototypes becomes too expensive and time consuming. Using virtual prototypes besides physical prototypes can increase a lot the competitiveness of the industry as the time to market and the price to develop the product are significantly reduced, and the design can be numerically validated and optimized. At the end of the DEMMOW project, the full set of detailed finite element models of each structural component as well as the detailed MBS-FEM model of the full mechanical system (the morphing wing) will be available. Fields of science natural sciencescomputer and information sciencessoftwareengineering and technologymechanical engineeringvehicle engineeringaerospace engineeringaircraftengineering and technologyelectrical engineering, electronic engineering, information engineeringelectronic engineeringsensors Programme(s) H2020-EU.3.4. - SOCIETAL CHALLENGES - Smart, Green And Integrated Transport Main Programme H2020-EU.3.4.5.2. - IADP Regional Aircraft Topic(s) JTI-CS2-2016-CFP04-REG-01-06 - High Fidelity Integrated Non-Linear MBS Modelling of Morphing Wing Call for proposal H2020-CS2-CFP04-2016-02 See other projects for this call Funding Scheme CS2-RIA - Research and Innovation action Coordinator GLOBAL DESIGN TECHNOLOGY Net EU contribution € 335 000,00 Address AVENUE DE L'EXPANSION 7 4432 ALLEUR Belgium 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 Région wallonne Prov. Liège Arr. Liège 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 € 335 000,00
