Gas turbine guide vane

Metal deforming – By extruding through orifice – Utilizing internal forming means

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72258, 2988971, 2988972, B21C 2504

Patent

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059271302

ABSTRACT:
A method for manufacturing an airfoil is provided which includes the steps of: a) providing a billet of discontinuously reinforced aluminum having at least 10 volume percent of silicon carbide as a reinforcing element, and no more than 30 volume percent of silicon carbide as the reinforcing element; 2) extruding the billet into an airfoil shaped geometry from a die, wherein the geometry includes a first wall, a second wall disposed opposite the first wall, a leading edge, a trailing edge disposed opposite the leading edge, and a first cavity disposed between the first and second walls, and the leading and trailing edges.

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patent: 5664453 (1997-09-01), Abo et al.
patent: 5698049 (1997-12-01), Bowden
patent: 5741127 (1998-04-01), Murayama et al.

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