COMPOSITES AND METHODS OF FORMING COMPOSITES HAVING TAILORED HARDNESS PROFILE

An aerospace component (100) may comprise a fiber reinforced composite material (102). The fiber reinforced composite material (102) includes a plurality of fiber layers and a carbon matrix (106) surrounding the plurality of fiber layers. A plurality of ceramic particles (108) is dispersed in the ca...

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Bibliographische Detailangaben
Hauptverfasser:	KUKUCHEK, Paul E, PUJAR, VIJAY V
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARTIFICIAL STONE CEMENTS CERAMICS CHEMISTRY COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS CONCRETE LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIME, MAGNESIA METALLURGY PERFORMING OPERATIONS REFRACTORIES SLAG TRANSPORTING TREATMENT OF NATURAL STONE
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Beschreibung
Zusammenfassung:	An aerospace component (100) may comprise a fiber reinforced composite material (102). The fiber reinforced composite material (102) includes a plurality of fiber layers and a carbon matrix (106) surrounding the plurality of fiber layers. A plurality of ceramic particles (108) is dispersed in the carbon matrix (106). A first fiber layer of the plurality of fiber layers may include a carbon fiber (104a), and a second fiber layer of the plurality of fiber layers may include a non-carbon fiber (104b). A hardness of the non-carbon fiber (104b) is greater than a hardness of carbon fiber (104a).