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EMA4FLIGHT SIGNED

Development of Electromechanical Actuators and Electronic control Units for Flight Control Systems

Total Cost €

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EC-Contrib. €

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Partnership

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Project "EMA4FLIGHT" data sheet

The following table provides information about the project.

Coordinator
FUNDACION TECNALIA RESEARCH & INNOVATION 

Organization address
address: PARQUE CIENTIFICO Y TECNOLOGICO DE BIZKAIA, ASTONDO BIDEA, EDIFICIO 700
city: DERIO BIZKAIA
postcode: 48160
website: www.tecnalia.com

contact info
title: n.a.
name: n.a.
surname: n.a.
function: n.a.
email: n.a.
telephone: n.a.
fax: n.a.

 Coordinator Country Spain [ES]
 Project website https://skylife-eng.com/en/projects/ema4flight-valema/
 Total cost 1˙856˙869 €
 EC max contribution 1˙698˙126 € (91%)
 Programme 1. H2020-EU.3.4.5.6. (ITD Systems)
 Code Call H2020-CS2-CFP03-2016-01
 Funding Scheme CS2-RIA
 Starting year 2017
 Duration (year-month-day) from 2017-02-01   to  2021-09-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    FUNDACION TECNALIA RESEARCH & INNOVATION ES (DERIO BIZKAIA) coordinator 479˙123.00
2    UMBRAGROUP SPA IT (FOLIGNO PG) participant 421˙646.00
3    RAMEM SA ES (MADRID) participant 280˙312.00
4    SKYLIFE ENGINEERING SL ES (SEVILLA) participant 264˙342.00
5    GMV AEROSPACE AND DEFENCE SA ES (TRES CANTOS) participant 252˙702.00

Map

 Project objective

Nowadays, there is a trend towards the More-Electric Aircraft (MEA) concept. MEA would replace the secondary aircraft power systems (electric, hydraulic and pneumatic) with a globally optimized electrical system. However, the architecture of the electric system must be carefully selected to optimize the whole aircraft. Actual research in MEA technology is focused on new advances in power electronics, fault-tolerant electric machines, digital control, electro-mechanical actuators and communications. Modern technologies involved in MEA are being taken in two different paths: i) elimination of bleed-air systems and hydraulic engines with further improvements in electrical power generation capability. It requires changes in both electrical generation and distribution network, and ii) replacement of hydraulics actuators with electro-mechanical actuators with the same level of safety and reliability, reducing weight, fuel usage, maintenance and production costs. Several studies have been recently carried out emphasizing the interest on the replacement of the traditional electro-hydrostatic actuators used in flight control surfaces by electro-mechanical actuators (EMAs). The reasons for such a choice are: weight and maintenance reduction, elimination of pipes vibration problems, increase of reliability, increase of the system performance and pressure losses thanks to the absence of valves. The EMA4FLIGHT project will design, manufacture and tune innovative electro-mechanical actuator sub-systems for aileron/spoiler and winglet/flap-tab flight control surfaces, with clearance for flight. The designed sub-systems will be improved by electric motor and ballscrew innovative architecture, advanced control strategies and smart safety, diagnostic and maintenance functions.

 Deliverables

List of deliverables.
Winglet/flap-tab sub-system Pans & Standards, Specification & requirements, Interface Control Document (ICD) Documents, reports 2020-02-27 11:25:53

Take a look to the deliverables list in detail:  detailed list of EMA4FLIGHT deliverables.

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The information about "EMA4FLIGHT" are provided by the European Opendata Portal: CORDIS opendata.

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