Building twinning Actions in smart Aviation with eNvironmental Gains

HORIZON.4.1HORIZON-CSAID: 101079091
EC Contribution
€12,755
Consortium Size
4 orgs
Summary

The main objective of BAANG is to stimulate the scientific excellence and innovation capacity of the involved partners in the field of smart aviation with a positive impact on the environment. BAANG creates the scientific strategy that connects 4 disciplines - aeronautics, mechatronics, mechanics of materials and additive technologies. Through a broad portfolio of twinning activities, it brings scientific and technological innovation leading to the design of an aircraft structure changing its morphology.Current aircraft have limited ability to adapt the wings aerodynamic shape to adapt to critical flight conditions. That restricts the possibilities of minimizing the aircrafts drag according to the actual wing load or suppressing adverse aeroelastic effects such as gust loading. The new wing design uses 3D printed metamaterials and advanced simulation techniques leading to efficient wing adaptation. In addition, the integration of intelligent sensing materials ensures an advanced aircraft design that is capable of self-inspection operation, such as detecting structural defects. The successful introduction of shape changing, self-actuating structures in aviation aims to reduce fuel consumption and CO2 emissions, reduce material waste in manufacturing, save significant maintenance costs and improve structural health monitoring. The main objective will be achieved by creating a network of collaborating academics from three leading research institutions - TU Delft, ICL and TU Wien, with the widening BUT institutions and industry representatives. Intensive involvement of 9 young researchers from BUT and 2 young researchers from TU Wien and linking them with top scientific teams for a period of 3 to 6 months. We expect a 60% increase in the number of international project submissions. In addition, there will be greater visibility of scientific results - the H-index of the involved early stage BUT researchers will double in period after the project.

Consortium (4)

Project Results (25)

Source: CORDIS, the EU research results database.

Publications (22)
A Uniaxial <i>Hysteretic Superelastic</i> Constitutive Model Applied to Additive Manufactured Lattices
PAMM· 2025DOI
Marius M. Schasching, Ondrej Červinek, Daniel Koutný, Heinz E. Pettermann, Melanie Todt
Design of kinematic mechanism of morphing wing with functionally gradient metamaterial skin
Engineering Materials, Structures, Systems and Methods for a More Sustainable Future· 2025DOI
J. Bajer, M. Hrstka, Z. Hadas, Z.S. Khodaei, M.H. Aliabadi
Geometry Optimization of a Highly Flexible Gradient Metamaterial Structure Using a Differential Evolution Algorithm
2024 21st International Conference on Mechatronics - Mechatronika (ME)· 2024DOI
Jan Bajer, Miroslav Hrstka, Zahra Sharif Khodaei, M.H. Aliabadi, Zdenek Hadas
Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials
2024 New Trends in Aviation Development (NTAD)· 2024DOI
Zikmund, Pavel; Navratil, Jan; Pollák, Jakub; Hrstka, Miroslav; Kofler, Michael; van Kampen, Erik-Jan
Multidisciplinary Design Optimization Framework for Morphing Wing using Metamaterials
2024 New Trends in Aviation Development (NTAD)· 2024DOI
Zikmund, Pavel; Navratil, Jan; Pollák, Jakub; Hrstka, Miroslav; Kofler, Michael; van Kampen, Erik-Jan
Simulations of superelastic lattice materials manufactured by additive manufacturing using a hypoelastic material model
· 2024DOI
Schasching, Marius Matthias; Červinek, Ondřej; Koutny, Daniel; Pettermann, Heinz; Todt, Melanie
Small-scale domain switching near sharp piezoelectric bi-material notches
International Journal of Fracture· 2024DOI
Hrstka, Miroslav; Kotoul, Michal; Profant, Tomáš; Kianicová, Marta
Concept of Autonomous Self-Sensing Metamaterial Structures for Future Aircraft
2023 IEEE 10th International Workshop on Metrology for AeroSpace (MetroAeroSpace)· 2023DOI
Jan Bajer, Filip Ksica, Petr Marcian, Miroslav Hrstka, Jan Navratil, Zdenek Hadas
A FEM-based morphing wing concept with periodic cell metamaterial outer surface
Hrstka Miroslav, Bajer Jan, Navratil Jan, Zikmund Pavel, Hadas Zdenek, Sharif Khodaei Zahra, Aliabadi Ferri, Kotoul Michal
Application of INDI to control a meta-materials based morphing wing
Pollák Jakub, Zikmund Pavel, van Kampen Erik-Jan
Application of Structural Optimization on Lattice Structure Design using Superelastic Material
Kofler, Michael
Coordination, excellence, and innovative methods
Marušincová Blanka
Demonstrator of the morphing wing sectionusing metamaterials
van Kampen Erik-Jan, Pollák Jakub, Bajer Jan, Navratil Jan, Kofler Michael, Hrstka Miroslav, Červinek Ondřej, Zikmund Pavel, Sobol Vítězslav
Design of morphing wing for aerodynamic performance considering the wing flexibility effects
Navratil Jan, Hostinský Vladimír, Sodja Jurij
Engineering Lattice Metamaterials – Simulation and Experimental Validation
Todt, Melanie
EXPERIENCE AND PREPARATION OF A PROJECT FUNDED BY THE HORIZON EUROPE PROGRAM
Marušincová Blanka
Hybrid seminar on the Twinning call - Twinning 2021 successful project
Marušincová Blanka
Inspiration from top universities in RMA and steps forward
Marušincová Blanka
Multi-scale Topology Optimisation with Overheating Control for Laser Powder Bed Fusion
Vaverka Ondřej, Ranjan, Rajit, Ayas Can, Langelaar Matthijs, Koutny Daniel
Optimization of Lattice Structures Using Neural Networks as Immersed Boundary Representations
Kofler Michael, MAUTE KURT, Wunsch Nils, EVANS JOHN, Elgeti Stefanie
Presentation for publication: Design of kinematic mechanism of morphing wing with functionally gradient metamaterial skin
Bajer Jan
Unified model of sandwich panel core and faces for aeroelastic optimization
Hostinský Vladimír, Sodja Jurij, Jebacek Ivo, Navratil Jan
Deliverables (3)
Documents, reports
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