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TR4EMACS SIGNED

Flexible Test Rig of Aircraft Control Surfaces powered by EMAs

Total Cost €

EC-Contrib. €

Partnership

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Outcomes and
results

TR4EMACS project word cloud

Explore the words cloud of the TR4EMACS project. It provides you a very rough idea of what is the project "TR4EMACS" about.

combined software flap alone right simulations complete actuation ftb2 operation emas representative validation corresponding impacts capability clean designed mechanical stand additionally flight tabs modular equip wings simulation left power designs units drawings equivalent 28 documentation benches aileron antagonist generation vdv supplies ema vdc external manager industrial tab consumption share performance evaluation manufacture code servo mode 270 hydraulic electrical interfaces generate demonstrator spoiler links flexible manuals surfaces winglet ground sky regional delivered modes implementing surface actuators double network bench supply connected load ease loads realistic rig maximize electromechanical model receive integration

Project "TR4EMACS" data sheet

The following table provides information about the project.

Coordinator	CENTRO DE ENSAYOS Y ANALISIS CETEST SL Organization address address: CALLE JOSE MIGUEL ITURRIOZ 26 city: BEASAIN postcode: 20200 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.
Coordinator Country	Spain [ES]
Project website	http://www.cetestgroup.com/our-expertise/research-development/
Total cost	509˙583 €
EC max contribution	509˙583 € (100%)
Programme	1. H2020-EU.3.4.5.4. (ITD Airframe)
Code Call	H2020-CS2-CFP03-2016-01
Funding Scheme	CS2-IA
Starting year	2017
Duration (year-month-day)	from 2017-06-01 to 2022-05-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	CENTRO DE ENSAYOS Y ANALISIS CETEST SL CENTRO DE ENSAYOS Y ANALISIS CETEST SL Organization address address: CALLE JOSE MIGUEL ITURRIOZ 26 city: BEASAIN postcode: 20200 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 (BEASAIN)	coordinator	261˙867.00
2	ASOCIACION CENTRO TECNOLOGICO CEIT-IK4 ASOCIACION CENTRO TECNOLOGICO CEIT-IK4 Organization address address: PASEO MANUEL DE LARDIZABAL 15 city: SAN SEBASTIAN postcode: 20018 website: www.ceit.es contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	ES (SAN SEBASTIAN)	participant	247˙716.00

Map

Project objective

The objective of this project is the design, manufacture and power on of a flexible and complete test rig for the on ground complete evaluation and validation of electromechanical actuators (EMA) and corresponding control units that will equip the control surfaces of the wings of the Clean Sky 2 Regional FTB2 demonstrator (A/C). The test rig will allow an on ground complete testing under realistic flight conditions, in terms of mechanical performance, performance of EMA control systems, and EMA electrical consumption and its impact in the A/C electrical network. Additionally for the aileron, the impacts of the combined actuation EMA/HA will be considered. Test rig will be composed of three double test benches (left and right wings) to target every A/C control surface (aileron, spoiler, flap-tab, and winglet tab). Flap and winglet tabs EMAs will share the same test bench. Test benches and control system will be designed in a modular way to ease their integration into a complete test rig. Two operation modes will be implemented to maximize the number of testing analysis. In the stand-alone mode, test benches will be connected to industrial power supplies (270 VDV and 28 VDC). In the integrated mode, the test rig will be connected to a representative and existing A/C electrical generation and distribution rig. The control system will generate representative equivalent antagonist loads corresponding to real flight conditions. In integrated model, the control system will have the capability of implementing A/C model simulation or receive corresponding load parameters from external A/C model simulations. Antagonist loads will be applied by means of a rig of hydraulic servo-actuators connected to an existing hydraulic supply. Mechanical links and interfaces will be representative of the real A/C equipment. A complete documentation (user manuals, electrical drawings, mechanical designs, open software code, etc.) will be also delivered to the topic manager.

Deliverables

List of deliverables.
Initial PDER (Initial Plan for Dissemination and Exploitation of Results)	Documents, reports	2020-01-27 12:42:03

Take a look to the deliverables list in detail: detailed list of TR4EMACS deliverables.

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The information about "TR4EMACS" are provided by the European Opendata Portal: CORDIS opendata.