CORROSION OF ALUMINUM AND ALUMINUM ALLOYS J.R.DAVIS PDF

Even in its early stages, aluminum corrosion is evident as general etching, pitting, or roughness of the aluminum surfaces. NOTE: Aluminum alloys commonly form a smooth surface oxidation that is from 0. This is not considered detrimental; the coating provides a hard shell barrier to the introduction of corrosive elements. Such oxidation is not to be confused with the severe corrosion discussed in this paragraph. General surface attack of aluminum penetrates relatively slowly, but is speeded up in the presence of dissolved salts.

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Even in its early stages, aluminum corrosion is evident as general etching, pitting, or roughness of the aluminum surfaces. NOTE: Aluminum alloys commonly form a smooth surface oxidation that is from 0.

This is not considered detrimental; the coating provides a hard shell barrier to the introduction of corrosive elements. Such oxidation is not to be confused with the severe corrosion discussed in this paragraph.

General surface attack of aluminum penetrates relatively slowly, but is speeded up in the presence of dissolved salts. Considerable attack can usually take place before serious loss of structural strength develops. At least three forms of attack on aluminum alloys are particularly serious: 1 the penetrating pit-type corrosion through the walls of aluminum tubing, 2 stress corrosion cracking of materials under sustained stress, and 3 intergranular corrosion which is characteristic of certain improperly heat-treated aluminum alloys.

In general, corrosion of aluminum can be more effectively treated in place compared to corrosion occurring on other structural materials used in aircraft. Treatment includes the mechanical removal of as much of the corrosion products as practicable, and the inhibition of residual materials by chemical means, followed by the restoration of permanent surface coatings. Treatment of Unpainted Aluminum Surfaces Relatively pure aluminum has considerably more corrosion resistance compared with the stronger aluminum alloys.

To take advantage of this characteristic, a thin coating of relatively pure aluminum is applied over the base aluminum alloy. In cleaning such surfaces, however, care must be taken to prevent staining and marring of the exposed aluminum and, more important from a protection standpoint, to avoid unnecessary mechanical removal of the protective Alclad layer and the exposure of the more susceptible aluminum alloy base material. A typical aluminum corrosion treatment sequence follows: Remove oil and surface dirt from the aluminum surface using any suitable mild cleaner.

Use caution when choosing a cleaner; many commercial consumer products are actually caustic enough to induce corrosion if trapped between aluminum lap joints. Choose a neutral Ph product. Hand polish the corroded areas with fine abrasives or with metal polish. Metal polish intended for use on clad aluminum aircraft surfaces must not be used on anodized aluminum since it is abrasive enough to actually remove the protective anodized film.

It effectively removes stains and produces a highly polished, lasting surface on unpainted Alclad. If a surface is particularly difficult to clean, a cleaner and brightener compound for aluminum can be used before polishing to shorten the time and lessen the effort necessary to get a clean surface. Treat any superficial corrosion present, using an inhibitive wipe down material. An alternate treatment is processing with a solution of sodium dichromate and chromium trioxide. Allow these solutions to remain on the corroded area for 5 to 20 minutes, and then remove the excess by rinsing and wiping the surface dry with a clean cloth.

Overcoat the polished surfaces with waterproof wax. Aluminum surfaces that are to be subsequently painted can be exposed to more severe cleaning procedures and can also be given more thorough corrective treatment prior to painting. The following sequence is generally used: Thoroughly clean the affected surfaces of all soil and grease residues prior to processing.

Any general aircraft cleaning procedure may be used. If residual paint films remain, strip the area to be treated. Apply the solution by swab or brush. Scrub the corroded area with the brush while it is still damp. While chromic acid is a good inhibitor for aluminum alloys, even when corrosion products have not been completely removed, it is important that the solution penetrate to the bottom of all pits and underneath any corrosion that may be present.

Thorough brushing with a stiff fiber brush should loosen or remove most existing corrosion and assure complete penetration of the inhibitor into crevices and pits.

Allow the chromic acid to remain in place for at least 5 minutes, and then remove the excess by flushing with water or wiping with a wet cloth. There are several commercial chemical surface treatment compounds, similar to the type described above, which may also be used.

Restoration of paint coatings should immediately follow any surface treatment performed. In any case, make sure that corrosion treatment is accomplished or is reapplied on the same day that paint refinishing is scheduled. Treatment of Anodized Surfaces As previously stated, anodizing is a common surface treatment of aluminum alloys. When this coating is damaged in service, it can only be partially restored by chemical surface treatment. Therefore, any corrosion correction of anodized surfaces should avoid destruction of the oxide film in the unaffected area.

Do not use steel wool or steel wire brushes. Do not use severe abrasive materials. Nonwoven abrasive pads have generally replaced aluminum wool, aluminum wire brushes, or fiber bristle brushes as the tools used for cleaning corroded anodized surfaces.

Care must be exercised in any cleaning process to avoid unnecessary breaking of the adjacent protective film. Take every precaution to maintain as much of the protective coating as practicable. Otherwise, treat anodized surfaces in the same manner as other aluminum finishes. Chromic acid and other inhibitive treatments can be used to restore the oxide film. In its most severe form, actual lifting of metal layers exfoliation, see Figure occurs.

Figure More severe cleaning is a must when intergranular corrosion is present. The mechanical removal of all corrosion products and visible delaminated metal layers must be accomplished to determine the extent of the destruction and to evaluate the remaining structural strength of the component. Corrosion depth and removal limits have been established for some aircraft. Any loss of structural strength should be evaluated prior to repair or replacement of the part.

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Davis Ed. ASM International p. The book describes the influences of composition, microstructure, mechanical working, heat treatment, joining methods, and environmental variables on the corrosion of aluminum-based materials Plate 1. Plate 1 The book is divided into 12 chapters, covering the diverse applications and problems associated with corrosion in aluminum and its alloys, as well as the diverse methods of testing for, and preventing, corrosion. The text starts by giving general information on the properties of aluminum and the basics of corrosion chapters 1 and 2. Chapters separately describes the different types of corrosion, discussing among other pitting, intergranular, galvanic, stray-current, and fretting corrosion, and environmentally assisted cracking. Each type of corrosion includes the mechanism, and characteristics, factors controlling it, and locations and applications where it might occur.

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