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TR4EMACS SIGNED

Flexible Test Rig of Aircraft Control Surfaces powered by EMAs

Total Cost €

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EC-Contrib. €

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Partnership

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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 ES (BEASAIN) coordinator 261˙867.00
2    ASOCIACION CENTRO TECNOLOGICO CEIT-IK4 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.

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