Methods of repairing engine components

Metal treatment – Process of modifying or maintaining internal physical... – Producing or treating layered – bonded – welded – or...

Reexamination Certificate

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C148S675000

Reexamination Certificate

active

07824510

ABSTRACT:
Methods are provided for repairing an engine component. In an embodiment, a method includes forming at least one layer of a first braze alloy mixture including about 40% by weight of a first base alloy material and about 60% by weight of a first braze alloy material, over a structural feature of the component. The first braze alloy material includes chromium, cobalt, tungsten, tantalum, aluminum, hafnium, carbon, boron, and a balance of nickel. A second braze alloy mixture is disposed over the at least one layer of the first braze alloy mixture, the second braze alloy mixture including between about 50% and about 60% by weight of a second base alloy material, and between about 40% and about 50% by weight of a second braze alloy material. The component is then subjected to heat treatment, and may be further subjected to machining, coating and final inspection.

REFERENCES:
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patent: 6454885 (2002-09-01), Chesnes et al.
patent: 6503349 (2003-01-01), Pietruska et al.
patent: 6968991 (2005-11-01), Renteria et al.
patent: 2005/0067069 (2005-03-01), Humm et al.
patent: 2006/0163323 (2006-07-01), Pietruska et al.
patent: 1783237 (2007-05-01), None

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