E-BIRD

Development of numerical models fo aircraft systems to be used within the JTI/GRA Shared Simulation Environment

 Coordinatore TWT GMBH SCIENCE & INNOVATION 

 Organization address address: BERNHAEUSER STRASSE 40-42
city: NEUHAUSEN
postcode: 73765

contact info
Nome: Alice
Cognome: Hilscher
Email: send email
Telefono: 497158000000
Fax: 4971580000000

 Nazionalità Coordinatore Germany [DE]
 Totale costo 150˙000 €
 EC contributo 112˙500 €
 Programma FP7-JTI
Specific Programme "Cooperation": Joint Technology Initiatives
 Code Call SP1-JTI-CS-2010-04
 Funding Scheme JTI-CS
 Anno di inizio 2011
 Periodo (anno-mese-giorno) 2011-06-01   -   2013-05-31

 Partecipanti

# participant  country  role  EC contrib. [€] 
1    TWT GMBH SCIENCE & INNOVATION

 Organization address address: BERNHAEUSER STRASSE 40-42
city: NEUHAUSEN
postcode: 73765

contact info
Nome: Alice
Cognome: Hilscher
Email: send email
Telefono: 497158000000
Fax: 4971580000000

DE (NEUHAUSEN) coordinator 72˙270.00
2    BAUSCH-GALL GMBH

 Organization address address: WOHLFARTSTRASSE 21 B
city: MUNCHEN
postcode: 80939

contact info
Titolo: Dr.
Nome: Ingrid
Cognome: Bausch-Gall
Email: send email
Telefono: 49893232625

DE (MUNCHEN) participant 40˙230.00

Mappa


 Word cloud

Esplora la "nuvola delle parole (Word Cloud) per avere un'idea di massima del progetto.

electro    components    thermal    mechanical    simulation    scenarios    models    aircraft    aea    emas   

 Obiettivo del progetto (Objective)

'This project makes a key contribution to the AEA through the development of novel simulation models for the quantitative evaluation of the mechanical, electrical, and thermal behaviour implied by the use of EMAs. This goal will be achieved via innovative developments on different levels. Firstly, the physical-mathematical models of both the EMAs and the FCS/LG will be set-up in such a way that they can be interlinked through the exchange of common parameters, typically EMA-positions and aerodynamic forces/torques. Secondly, the individual components will be integrated into a single simulation model, which directly interfaces with the Shared Simulation Environment (SSE) of AEA, GRA3. Thirdly, test scenarios will be defined, which are adequate for the validation of the electro-mechanical and electro-thermal outputs. The electro-thermal data involved in these test scenarios differs from that normally considered for mechanical/hydro-mechanical systems. To ensure that the simulation models can readily be integrated into existing aircraft concepts and simulation tools, standards will be used wherever possible.'

Introduzione (Teaser)

Simulation software plays an important role in aircraft design. Novel libraries describing the behaviours of components destined for all-electric aircraft integrate seamlessly with other platforms for efficient testing of design concepts from very early on.

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RESELYSER (2011)

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