FATIMA

Fatigue testing of CFRP materials

Coordinatore	AMIC Angewandte Micro-Messtechnik GmbH    more  Organization address address: VOLMERSTRASSE 9B city: BERLIN postcode: 12489 contact info Titolo: Dr. Nome: Jürgen Cognome: Keller Email: send email Telefono: +49 30 63922540 Fax: +49 30 63922541
Nazionalità Coordinatore	Germany [DE]
Totale costo	199˙994 €
EC contributo	149˙995 €
Programma	FP7-JTI Specific Programme "Cooperation": Joint Technology Initiatives
Code Call	SP1-JTI-CS-2010-03
Funding Scheme	JTI-CS
Anno di inizio	2011
Periodo (anno-mese-giorno)	2011-01-01   -   2013-12-31

 Partecipanti

#	participant	country	role	EC contrib. [€]
1	AMIC Angewandte Micro-Messtechnik GmbH  Organization address address: VOLMERSTRASSE 9B city: BERLIN postcode: 12489 contact info Titolo: Dr. Nome: Jürgen Cognome: Keller Email: send email Telefono: +49 30 63922540 Fax: +49 30 63922541	DE (BERLIN)	coordinator	59˙059.00
2	BERLINER NANOTEST UND DESIGN GMBH  Organization address address: VOLMERSTRASSE 7 B city: BERLIN postcode: 12489 contact info Titolo: Dr. Nome: Thomas Cognome: Winkler Email: send email Telefono: +49 30 63923880 Fax: +49 30 63923881	DE (BERLIN)	participant	45˙540.00
3	CHEMNITZER WERKSTOFFMECHANIK GMBH  Organization address address: TECHNOLOGIE CAMPUS 1 city: CHEMNITZ postcode: 9126 contact info Titolo: Mr. Nome: Jens Cognome: Hammacher Email: send email Telefono: +49 371 5347960 Fax: +49 371 5347961	DE (CHEMNITZ)	participant	45˙396.00

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 Obiettivo del progetto (Objective)

'The FATIMA project proposed by the consortium will work on testing and fatigue prediction of carbon fiber reinforced plastics (CFRP) as required in call JTI-CS-2010-3-ECO-01-007. The challenging objective is to go beyond the state of the art in terms of approaches to account for humidity, multi-ply and multi-axiality effects in organic laminate structures. Intensive work in the field resulted in a number of concepts for accelerated lifetime predictions for carbon fiber reinforced polymers. Within FATIMA, these concepts will be adapted to the material provided by the partners of the Clean Sky consortium. The proposed methodology and integration into the fatigue testing procedure will approach expansions addressing humidity effects, different stack-up structures and combined loading of these composite structures. Appropriate models of a multitude of specific laminate structures will be provided as a tool box for composing desired laminates consisting of plies with known behavior. Failure criteria developed for predicting the damage in composite materials due to multi-axial loads will be evaluated, selected and advanced to meet the objectives of the call.'