Verbundmaterial mit verbesserten Dampfeigenschaften und Verfahren zu dessen Herstellung

A composite laminate structure formed from at least one high-strength, high-stiffness fiber-resin composite structural lamina (20) laminated to at least one fiber-resin composite damping lamina (10), wherein the resin matrix of the structural lamina (20) resides below its glassification temperature...

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Bibliographische Detailangaben
Hauptverfasser:	LIGUORE, SALVATORE L, HUNTER, KIPPLAN
Format:	Patent
Sprache:	ger
Schlagworte:	ACOUSTICS ACOUSTICS NOT OTHERWISE PROVIDED FOR AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM METHODS OR DEVICES FOR PROTECTING AGAINST, OR FOR DAMPING,NOISE OR OTHER ACOUSTIC WAVES IN GENERAL MUSICAL INSTRUMENTS PERFORMING OPERATIONS PHYSICS SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR SHAPING OR JOINING OF PLASTICS SOUND-PRODUCING DEVICES TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Beschreibung
Zusammenfassung:	A composite laminate structure formed from at least one high-strength, high-stiffness fiber-resin composite structural lamina (20) laminated to at least one fiber-resin composite damping lamina (10), wherein the resin matrix of the structural lamina (20) resides below its glassification temperature (Tg) and wherein the resin matrix of the damping lamina (10) resides above its glassification temperature during normal use temperatures, thereby providing a high-strength laminate with improved damping properties.