VANTEX - Vanishing Textile binder structure for the stabilisation of dry carbon fibre preforms in the Resin Transfer Moulding process

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Projektnummer

8634.1;7 EPRP-IW

Projekttitel

VANTEX - Vanishing Textile binder structure for the stabilisation of dry carbon fibre preforms in the Resin Transfer Moulding process

Projekttitel Englisch

VANTEX - Vanishing Textile binder structure for the stabilisation of dry carbon fibre preforms in the Resin Transfer Moulding process

Texte zu diesem Projekt

	Deutsch	Französisch	Italienisch	Englisch
Kurzbeschreibung	-	-	-
Abstract	-	-	-

Erfasste Texte

Kategorie	Text
Kurzbeschreibung (Englisch)	VANTEX - Vanishing Textile binder structure for the stabilisation of dry carbon fibre preforms in the Resin Transfer Moulding process
Abstract (Englisch)	In producing long-fibre reinforced plastic structures by resin injection processes the reinforcing fibres areprovided as preforms. The latter can be made in many different ways (e.g. moulding, sewing ...). Thermoplastic binders or sewing yarns are mostly used as stabilisers for such preforms. This projectinvestigates the effect of the stabiliser on the process chain and on the mechanical properties of the resultingcomponent. The effect of the stabiliser on the residual strength of an FRP aircraft component after impactloading is evaluated, as well as that on the injection process itself.

Kategorie

Text

Kurzbeschreibung
(Englisch)

VANTEX - Vanishing Textile binder structure for the stabilisation of dry carbon fibre preforms in the Resin Transfer Moulding process

Abstract
(Englisch)

In producing long-fibre reinforced plastic structures by resin injection processes the reinforcing fibres areprovided as preforms. The latter can be made in many different ways (e.g. moulding, sewing ...). Thermoplastic binders or sewing yarns are mostly used as stabilisers for such preforms. This projectinvestigates the effect of the stabiliser on the process chain and on the mechanical properties of the resultingcomponent. The effect of the stabiliser on the residual strength of an FRP aircraft component after impactloading is evaluated, as well as that on the injection process itself.