Discontinuously reinforced aluminum gas turbine guide vane

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Specific casing or vane material

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Details

416223A, 416232, 416229R, 416229A, F01D 102

Patent

active

058736999

ABSTRACT:
An airfoil is provided having a cross-sectional geometry which 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. The first cavity is disposed between the first and second walls, and the leading and trailing edges. The cross-sectional geometry extends between a first and a second end, and the airfoil is formed from discontinuously reinforced aluminum.

REFERENCES:
patent: 5015534 (1991-05-01), Kampe et al.
patent: 5511603 (1996-04-01), Brown et al.
patent: 5560991 (1996-10-01), Patel et al.

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