Cobalt-palladium-silicon-boron brazing alloy
AssigneeGeneral Electric Company
InventorsMurray S. Smith, Jr., Mark S. Hilboldt, Pracheeshwar S. Mathur
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AssigneeGeneral Electric Company
InventorsMurray S. Smith, Jr., Mark S. Hilboldt, Pracheeshwar S. Mathur
Estimating the term…
A brazing alloy, particularly suited for use in high temperature gas turbine engines has a composition range which exhibits X-ray inspection capability, adequate stress rupture properties, ductility and oxidation resistance. The brazing alloy composition consists essentially of about 25-95% Pd, up to about 5% Si, up to about 3.5% B, balance being Co and incidental impurities, all percentages being by weight. The brazing alloy is capable of brazing in the 1800.degree.-2100.degree. F. temperature range and is less costly than current Au-bearing brazing alloys currently in use for brazing in this temperature range.
An improved brazing alloy consisting essentially of, by weight, 25-95% Pd, up to 5% Si, up to 3.5% B, balance being Co and incidental impurities, the Si, when selected, being at least about 2%, and the B, when selected, being at least about 0.5%, said brazing alloy having a liquidous temperature in the range of about 1800.degree.-2100.degree. F. and being characterized by the substantial absence of Ag, Ti, Mn, Cu, and P.
Dependencies are inferred from the claim text.