FOAM BASED NON-NEWTONIAN MATERIALS FOR USE WITH AIRCRAFT ENGINE COMPONENTS

An engine component (80) for a turbine engine is provided. The engine component (80) includes a substrate (82) defining a surface (84), and an energy absorbing composite (86) positioned on the surface of the substrate or within the substrate. The energy absorbing composite (86) includes a shear thic...

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Bibliographische Detailangaben
Hauptverfasser:	KRAY, Nicholas, Joseph, SELLINGER, Aaron, Todd
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES NON-POSITIVE DISPLACEMENT PUMPS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	An engine component (80) for a turbine engine is provided. The engine component (80) includes a substrate (82) defining a surface (84), and an energy absorbing composite (86) positioned on the surface of the substrate or within the substrate. The energy absorbing composite (86) includes a shear thickening fluid (210) distributed through a solid foamed synthetic polymer matrix (212). La présente invention concerne un composant (80) pour un moteur à turbine. Le composant de moteur (80) comprend un substrat (82) définissant une surface (84), et un composite d'absorption d'énergie (86) positionné sur la surface du substrat ou à l'intérieur du substrat. Le composite d'absorption l'énergie (86) comprend un fluide d'épaississement par cisaillement (210) distribué à travers une matrice polymère synthétique moussée solide (212).