Explore the words cloud of the VALEMA project. It provides you a very rough idea of what is the project "VALEMA" about.
The following table provides information about the project.
Coordinator |
GMV AEROSPACE AND DEFENCE SA
Organization address contact info |
Coordinator Country | Spain [ES] |
Total cost | 1˙091˙512 € |
EC max contribution | 782˙512 € (72%) |
Programme |
1. H2020-EU.3.4.5.6. (ITD Systems) |
Code Call | H2020-CS2-CFP04-2016-02 |
Funding Scheme | CS2-IA |
Starting year | 2017 |
Duration (year-month-day) | from 2017-06-01 to 2022-07-31 |
Take a look of project's partnership.
# | ||||
---|---|---|---|---|
1 | GMV AEROSPACE AND DEFENCE SA | ES (TRES CANTOS) | coordinator | 260˙137.00 |
2 | RAMEM SA | ES (MADRID) | participant | 230˙125.00 |
3 | UMBRAGROUP SPA | IT (FOLIGNO PG) | participant | 170˙625.00 |
4 | FUNDACION TECNALIA RESEARCH & INNOVATION | ES (DERIO BIZKAIA) | participant | 61˙512.00 |
5 | SKYLIFE ENGINEERING SL | ES (SEVILLA) | participant | 60˙112.00 |
The objective of the VALEMA project is twofold: - On the one hand it is required to manufacture and assembly units (EMAs and ECUs) previously designed and developed according to the JTI-CS2-2016-CFP03-SYS-02-14 Call (Development of electromechanical actuators and electronic control units for flight control systems) for in flight tests activities. - On the other hand it is required to perform certification activities regarding both the HW and SW of the ECUs in order to obtain a permit to fly in the FTB2 demonstrator of the Regional Aircraft.
The manufacturing part will include a deep analysis of manufacturing routes, materials to be used and applicable qualification tests, searching for innovative processes, in order to ensure that the processes optimize the manufacturing time, minimize the raw material used and minimize the environmental impact.
The certification activities will be aimed at obtaining the permit to fly from the applicable Airworthiness Authorities for the aileron/spoiler ECU HW design (according to DO-254) and for the aileron/spoiler ECU SW design (according to DO-178B).
These activities can be considered as the last step within the HW and SW design of the aileron/spoiler ECU development to be undertaken in EMA4FLIGHT according to the JTI-CS2-2016-CFP03-SYS-02-14 Call and, as such, the innovations developed within that call also apply herein.
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The information about "VALEMA" are provided by the European Opendata Portal: CORDIS opendata.