AIRFOIL WITH MULTI-MATERIAL REINFORCEMENT

An airfoil 12 includes: an airfoil body 17 having convex and concave sides extending between a leading edge 22 and a trailing edge 24, the airfoil body 17 including primary and secondary regions having differing physical properties; and at least one metallic cladding element 40, 42 attached to the a...

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Bibliographische Detailangaben
Hauptverfasser:	DAVIS, Tod Winton, WU, Wei, BRYANT, Gary Willard Jr
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 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 airfoil 12 includes: an airfoil body 17 having convex and concave sides extending between a leading edge 22 and a trailing edge 24, the airfoil body 17 including primary and secondary regions having differing physical properties; and at least one metallic cladding element 40, 42 attached to the airfoil body 17.