COMPOSITE AIRFOIL WITH METAL STRENGTH

A laminated composite airfoil assembly includes a first lamina formed of a pre-preg material including metal fibers, and at least a second lamina formed of a pre-preg material including at least one of metal fibers intermixed with carbon fibers, only metal fibers, only carbon fibers, a substrate inc...

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Bibliographische Detailangaben
Hauptverfasser:	Maripalli, Ramkrishna, Kray, Nicholas Joseph, Jain, Nitesh, Chandrasekar, Sujana, Lin, Wendy Wenling
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT PUMPS PERFORMING OPERATIONS POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS PUMPS FOR LIQUIDS OR ELASTIC FLUIDS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	A laminated composite airfoil assembly includes a first lamina formed of a pre-preg material including metal fibers, and at least a second lamina formed of a pre-preg material including at least one of metal fibers intermixed with carbon fibers, only metal fibers, only carbon fibers, a substrate including metal fibers, a substrate including carbon fibers, and combinations thereof.