BIFURACTING LAYUP FOR AIRFOIL RIB, METHODS OF MANUFACTURE THEREOF AND ARTICLES COMPRISING THE SAME

An airfoil (100) comprises a wall (102) that defines a leading edge (104) and a trailing edge (106) and one or more cavities (108, 110) located within the wall (102) along with a rib (112) that separates the cavities. The rib or the wall comprises a first split ply (114) that comprises a consolidate...

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Bibliographische Detailangaben
1. Verfasser:	LILES, Howard J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	ARTIFICIAL STONE BLASTING CEMENTS CERAMICS CHEMISTRY COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDINGMATERIALS CONCRETE ENGINE PLANTS IN GENERAL HEATING LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING LIME, MAGNESIA MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING METALLURGY NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PERFORMING OPERATIONS REFRACTORIES SLAG STEAM ENGINES TRANSPORTING TREATMENT OF NATURAL STONE WEAPONS
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Beschreibung
Zusammenfassung:	An airfoil (100) comprises a wall (102) that defines a leading edge (104) and a trailing edge (106) and one or more cavities (108, 110) located within the wall (102) along with a rib (112) that separates the cavities. The rib or the wall comprises a first split ply (114) that comprises a consolidated section (114A) and two or more split sections (114B, 114C); wherein the split sections emanate from the consolidated section (114A); and where the split sections define the wall (102) and the cavities (108,110) of the airfoil.