E-BIRD

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

Coordinatore	TWT GMBH SCIENCE & INNOVATION    more  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

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 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.