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TRIMIS

Advanced concepts for trailing edge morphing wings - Design and manufacturing of test rig and test samples - Test execution

Project

SMyTE - Advanced concepts for trailing edge morphing wings - Design and manufacturing of test rig and test samples - Test execution


Funding origin:
European
European Union
STRIA Roadmaps:
Vehicle design and manufacturing (VDM)
Vehicle design and manufacturing
Transport mode:
Airborne
Airbone
Transport sectors:
Passenger transport
Passenger transport
Freight transport
Freight transport
Duration:
Start date: 01/02/2012,
End date: 01/01/2013

Status: Finished
Funding details:
Total cost:
€214 289
EU Contribution:
€157 715

Overview

Objectives:

The SMyTE project aims to develop state-of-the-art SMA actuator specimen(s), undergoing controlled deformation and to perform tests on a suitably designed and assembled test rig with its related interface components to assure the characterisation of SACM and DESA demonstrators and the validation of numerical schemes used during design phase. At a later stage, it is further aimed to be applied on the trailing edge of an adaptive/morphing wing. For this reason, several aspects such as fail-safe, test execution under different type of static and dynamic loads are considered reflecting in fact the future applicability of the current project.

The proposal is building on background knowledge in design and characterisation of SMA actuators and mechanisms as well as in experience in prototype static and dynamic characterisation tests.

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