Method for preparing pre-coated, metallic components and...

Details Method for preparing pre-coated, metallic components and... Method for preparing pre-coated, metallic components and...

2005-10-11

2005-10-11

Wyszomierski, George (Department: 1742)

Metal treatment

Process of modifying or maintaining internal physical...

Producing or treating layered, bonded, welded, or...

C148S675000

Reexamination Certificate

active

06953509

ABSTRACT:
A high-strength, corrosion- and heat-resistant aircraft structural component such as a fastener is prepared by providing a corrosion-resistant stainless steel or heat-resistant superalloy metallic component precursor that is not in its final heat-treated state, and coating with an aluminum-containing, curable polyaromatic phenolic coating material having a non-volatile portion that is predominantly organic and is curable at about the high-strength metallic alloy component's stress equalizing tempering temperature. The coated, high-strength metallic-alloy component is then thermally treated to concurrently impart pre-determined metallurgical properties to the finished, metallic substrate, and cure the organic, aluminum-containing coating.

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Copy of Search Report for corresponding French Appl. No. 0406017 dated Mar. 8, 2005.

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