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TRIMIS

Smart Morphing and Sensing

PROJECTS
Funding
European
European Union
Duration
-
Status
Complete
Geo-spatial type
Other
Total project cost
€3 991 688
EU Contribution
€3 991 688
Project Acronym
SMS
STRIA Roadmaps
Vehicle design and manufacturing (VDM)
Transport mode
Airborne icon
Transport policies
Deployment planning/Financing/Market roll-out
Transport sectors
Passenger transport,
Freight transport

Overview

Link to CORDIS
Objectives

Smart Morphing & Sensing is a multidisciplinary project associating novel electroactive actuators and sensors to increase aerodynamic efficiency and attenuate vibrations and noise. This is achieved via aerostructural morphing exploiting the real-time information from the distributed actuation and sensing systems. This goal is achieved by actuating the smart-materials to deform the structure according to optimum shape design by means of Flight Control Commands.

The novel “intelligent material” technology is a hybrid association of small piezo-actuators distributed along the control surface, of Shape Memory Alloys and of Electroactive Polymers, disposed under the ‘skin’ of the active structure. This novel hybrid design allows associating fast time response and vibrational actuation with simultaneous high deformation ability. The ability in capturing energy from the already existing vibrations and redistributing it in the actuation will be used to partially supply the system and therefore ensure an economic and realistic morphing. This is beyond the cutting edge of the state of the art in morphing concepts. The use of novel distributed pressure sensors based on fiber Bragg grating provides real-time information on the actuation performance and the flight situation enabling an efficient in-situ optimization using a dedicated controller interfacing the actuators with the fiber based sensors.

Aerodynamic and structural experiments are included to demonstrate the abilities of the new integrated smart sensing and morphing design via real-time actuation. High-fidelity aeroelastic computations are used to optimize the actuators location and function. The experiments will study the increase of the aerodynamic efficiency in cruise, take-off and landing by controlling the turbulence structure responsible for noise and vibration. The main configuration will be based on the Airbus A320 type wing with morphing flap.

Funding

Parent Programmes
Institution Type
Public institution
Institution Name
European Commission
Type of funding
Public (EU)
Specific funding programme
H2020-EU.3.4.

Partners

Lead Organisation
Organisation
Institut National Polytechnique De Toulouse
Address
6 allée Emile Monso, BP 34038 TOULOUSE, France
Organisation website
EU Contribution
€932 500
Partner Organisations
Organisation
Cfd Software - Entwicklungs- Und Forschungsgesellschaft Mbh
Address
Wolzogenstrasse 4, 14163 Berlin, Germany
EU Contribution
€391 250
Organisation
Scheller Technology Gmbh
Address
POELER STRASSE 85A, 23970 WISMAR, Germany
EU Contribution
€365 875
Organisation
National Technical University Of Athens
Address
Heroon Polytechniou 9 (polytechnic campus), 15780 ZOGRAFOS, Greece
Organisation website
EU Contribution
€248 750
Organisation
Office National D' Etudes Et De Recherches Aérospatiales
Address
29, avenue de la Division Leclerc, BP72 CHÂTILLON CEDEX, France
Organisation website
EU Contribution
€319 688
Organisation
Instytut Maszyn Przeplywowych Im Roberta Szewalskiego Polskiej Akademii Nauk - Imp Pan
Address
Ul. Fiszera 14, 80N/A231 Gdansk, Poland
Organisation website
EU Contribution
€335 563
Organisation
Novatem
Address
3 RUE DE THIONVILLE, 11110 COURSAN, France
EU Contribution
€349 688
Organisation
Cfs Engineering Sa
Address
Epfl Innovation Park Batiment A, 1015 Lausanne, Switzerland
Organisation website
EU Contribution
€331 250
Organisation
Politecnico Di Milano
Address
Piazza Leonardo Da Vinci 32, 20133 Milano, Italy
Organisation website
EU Contribution
€377 375
Organisation
Cementys
Address
27 VILLA DAVIEL, 75013 PARIS, France
EU Contribution
€339 750

Technologies

Technology Theme
Aircraft design and manufacturing
Technology
Morphing wing
Development phase
Research/Invention

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