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LE coupon based technology

European Union
Complete with results
Geo-spatial type
Total project cost
€197 815
EU Contribution
€148 360
Project Acronym
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Societal/Economic issues,
Transport sectors
Passenger transport,
Freight transport


Call for proposal
Link to CORDIS

SMYLE involved mathematical modelling, design, fabrication and testing of a Shape Memory Alloy coupon undergoing actuated controlled deformation. It was envisaged that two different SM actuating principles were pursued. In the first approach, the actuator was embedded in the coupon in the form of an active layer, whereas in the second approach the use of the so-called compliant mechanisms was investigated with the SMA wires as actuating elements. Work was carried out as follows: Determination of single-cycle/multi-cycle loading conditions which involve the thermal-mechanical and electrical aspects, with emphasis on hysteresis, as well as determination of experimental conditions, i.e. surface uniform- & non-uniform actuation type of loading; prediction of specimen's surface response by means of simple analytic methods.

Uniform as well non-uniform surfaces of the same SMA specimen were pursued. Testing included the deformation to the desired shapes repeatedly and measured reproducibility and attainment of desired shape. The effect of temperature was also evaluated by completing several actuation cycles at temperatures near the SMA transformation temperature. Commercially available SMA was used and an initial characterisation phase is foreseen. The aim was to have the material behaviour under static and dynamic conditions up to failure. It was foreseen that, for every actuating principle, the most promising concepts were bench-tested to evaluate characteristics and highlight challenges. Up to four concepts were tested in this context. Eventual modification of numerical model and structural correction of the SMA specimen in case of unsatisfactory experimental outcome was carried out. Finally, a functional SMA specimen and recommendations for future work were delivered.


Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
JTI-CS - Joint Technology Initiatives - Clean Sky
Other Programme
JTI-CS-2009-2-GRA-02-006 Instrumentation-electronic (Optical assembly & Thermal and mechanical strain measurement)


SMYLE proposed a technological research program allowing to develop, manufacture and validate actuators by integrating a number of various emerging SMA technologies that result in high performance/ high reliability actuators. The innovative aspects of the proposed technologies were new SMA material concepts with a high power-to-weight ratio and high performance & reliability optimised for later application into a morphing/adaptive wing. Thanks to these new technologies, the SMYLE actuator system contributed to lower mass (compared to a conventional mechanical/hydraulic actuator), and full integration (at a later stage) into the leading edge of an adaptive wing system, i.e.: at first, SMYLE can significantly improve the aerodynamics at the LE vicinity since it offers a greater operational envelope compared to a conventional LE slat device. Secondly, it can serve as a de-icing protection device, therefore eliminating heavy conventional, as well as electrically demanding, de-icing systems. Thirdly, it can be further utilised as a flight control surface replacement, locally improving the aerodynamics in the LE vicinity during flight.


Lead Organisation
Aerotron Research Astiki Etairia
LYKOURGOU 5-7, 17563 Paleo Faliro, Greece
EU Contribution
€73 874
Partner Organisations
Inasco Hellas Etaireia Efarmosmenon Aerodiastimikon Epistimon Ee
Napoleontos Zerva 18, 16675 Glyfada Athina, Greece
EU Contribution
€681 929
Inasco Hellas Etaireia Efarmosmenon Aerodiastimikon Epistimon Ee
Napoleontos Zerva 18, 16675 Glyfada Athina, Greece
EU Contribution
€74 486


Technology Theme
Aircraft design and manufacturing
Morphing wing
Development phase

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