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EMA4FLIGHT SIGNED

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

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

EMA4FLIGHT project word cloud

Explore the words cloud of the EMA4FLIGHT project. It provides you a very rough idea of what is the project "EMA4FLIGHT" about.

fuel tune thanks actuator optimized electrical elimination smart generation winglet hydraulic bleed hydraulics communications trend electro replace emphasizing spoiler aileron machines manufacture improvements carefully pneumatic air maintenance pipes actual replacement nowadays diagnostic designed electric emas clearance aircraft mechanical engines secondary optimize tab ema4flight hydrostatic modern losses pressure capability technologies functions actuators flap absence fault vibration strategies tolerant globally valves architecture paths surfaces sub performance weight reducing innovative digital electronics power network flight mea reliability ballscrew safety motor

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 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.	ES (DERIO BIZKAIA)	coordinator	479˙123.00
2	UMBRAGROUP SPA UMBRAGROUP SPA Organization address address: VIA VALTER BALDACCINI 1 LOCALITA PACIANA ZONA INDUSTRIALE city: FOLIGNO PG postcode: 6034 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	IT (FOLIGNO PG)	participant	421˙646.00
3	RAMEM SA RAMEM SA Organization address address: CALLE SAMBARA 33 city: MADRID postcode: 28033 website: www.ramem.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (MADRID)	participant	280˙312.00
4	SKYLIFE ENGINEERING SL SKYLIFE ENGINEERING SL Organization address address: CALLE AMERICO VESPUCIO N5, BLOQUE 1, LOCAL A 8-12 city: SEVILLA postcode: 41092 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (SEVILLA)	participant	264˙342.00
5	GMV AEROSPACE AND DEFENCE SA GMV AEROSPACE AND DEFENCE SA Organization address address: CALLE ISAAC NEWTON PARQUE TECNOLOGICO DE MADRID city: TRES CANTOS postcode: 28760 website: n.a. contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	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.