VALidation tests of ElectroMechanical Actuators and its dedicated control units at TRL 6 level

Informations projet

VALEMA

N° de convention de subvention: 755615

DOI 10.3030/755615

Projet clôturé

Date de signature de la CE 30 Mai 2017

Date de début 1 Juin 2017

Date de fin 31 Juillet 2022

Financé au titre de

• SOCIETAL CHALLENGES - Smart, Green And Integrated Transport

Coût total € 1 091 512,50

Contribution de l’UE € 782 512,50

Coordonné par

GMV AEROSPACE AND DEFENCE SA
Spain

Livrables

Documents, reports (1)

PUBLISHABLE REPORT ON PROJECT TECHNICAL RESULTS

Summary report illustrating the results obtained by the project Focus will be on progress beyond state of the art and or state of the practice

Demonstrators, pilots, prototypes (1)

DELIVERY OF PARTS

Delivery of EMAECU units 4 ECU units for the aileron system 6 ECU units for the spoiler system 10 ECU units for the wingletflaptab system 5 backup aileron servos Components motor and mechanical parts for 4 EMA units for the aileron system Components motor and mechanical parts for 6 EMA units for the spoiler systemCOTS sensors elements are excluded in this delivery LVDT sensors Hall sensors servovalves or similar other commercial elementsEach unit to be delivered will have a Configuration information report

Publications

Other (1)

"Poster: ""From TRL3 to TRL6 (and “permit to fly”) thanks to RTCA DO-254 or EUROCAE ED-80"""

Auteurs: Iñigo Eguizabal (Tecnalia) Eduardo Guzmán (Tecnalia) Pablo Casado (Tecnalia) Jose Ramón García (Tecnalia)
Publié dans: 8th International Conference on Recent Advances in Aerospace Actuation Systems and Components, R3ASC’18, 2018
Éditeur: R3ASC’18

Conference proceedings (1)

PM Brushless Motor for Aileron/Spoiler system of a Regional Aircraft

Auteurs: Moreno D'Andrea, Francesco Fiume, Davide Macers, Marco Villani
Publié dans: IECON 2019 - 45th Annual Conference of the IEEE Industrial Electronics Society, Numéro 1, 2019, Page(s) 1261-1265, ISBN 978-1-7281-4878-6
Éditeur: IEEE
DOI: 10.1109/iecon.2019.8926985