Exfoliation Corrosion

Exfoliation Corrosion


Exfoliation corrosion is a more severe form of intergranular corrosion that can occur along aluminum grain boundaries in the fuselage empennage and wing skins of aircraft. These grain boundaries in both aluminum sheet and plate are oriented in layers parallel to the surface of the material, due to the rolling process. The delamination of these thin layers of aluminum, with white corrosion products between the layers, characterizes exfoliation corrosion. Exfoliation corrosion is often found next to fasteners where an electrically insulating sealant or a sacrificial cadmium plating has broken down, permitting a galvanic action between the dissimilar metals. Where fasteners are involved, exfoliation corrosion extends outward from the fastener hole, either from the entire circumference of the hole or in one direction from a segment of the hole. In severe cases, the surface bulges outward, but in less severe cases, there may be no telltale blisters, and you can only detect the exfoliation corrosion by nondestructive inspection methods that are not always very effective.


Dealloying

De-alloying, or selective leaching, is the selective corrosion of a specific element in an alloy. This results in the formation of a porous structure that is not strong enough to support the applied mechanical loads. The specific type of corrosion that occurs depends on several factors including metal composition, metal microstructure, environment, component geometry, stress on the component, contact between metals, and the manner in which components are joined together. The common examples are dezincification of brass alloys used for plumbing, where the zinc is leached out of the alloy forming unstabilized brass. The result of corrosion in such cases is deteriorated and porous copper.


Intergranular Corrosion

Intergranular corrosion is a chemical or electrochemical attack on the grain boundaries of the affected metal. It often occurs due to impurities in the metal, which tend to be present in higher contents near grain boundaries. These boundaries can be more vulnerable to corrosion than the bulk of the metal. The result is that the metal grains fall away and the metal is weakened. The close microstructure of a metal reveals that the grains are formed during the solidification of the alloy as well as at the grain boundaries between them. Intergranular corrosion can be caused by impurities present at these grain boundaries or by the depletion or enrichment of an alloying element at the grain boundaries. It occurs along or adjacent to these grains, seriously affecting the mechanical properties of the metal while the bulk of the metal remains intact. An example of intergranular corrosion is carbide precipitation, a chemical reaction that can occur when a metal is subjected to very high temperatures (800 °F - 1650 °F) and/or localized hot work such as welding. Austenitic stainless steels and precipitation-strengthened aluminum alloys are examples of metals that can suffer from intergranular corrosion if the alloys are not properly processed and if they are exposed to corrosive environments. In stainless steels, during these reactions, carbon consumes the chromium-forming carbides and causes the level of chromium remaining in the alloy to drop below the 11% needed to sustain the spontaneously-forming passive oxide layer. The SS 304L and 316L are enhanced versions of 304 and 316 stainless steel that contain lower levels of carbon providing the best corrosion resistance to carbide precipitation.


Stress Corrosion Cracking

Stress corrosion cracking (SCC) is a result of the combination of tensile stress and a corrosive environment, often at elevated temperatures. In most cases, the stress or environment by itself is insufficient to cause the degradation of the metal. That is if the stress is below the metal’s yield strength the metal would not corrode in the specific environment. It is the net result of external stress such as actual tensile loads on the metal or expansion/contraction due to rapid temperature changes. It may also be the result of residual stress imparted during the manufacturing process such as cold forming, welding, machining, grinding, etc. In stress corrosion, the majority of the surface usually remains intact; however, fine cracks appear in the microstructure, making the corrosion hard to detect. The cracks typically have a brittle appearance and form and spread in a direction perpendicular to the location of the stress. Selecting proper materials for a given environment can mitigate the potential for catastrophic failure due to SCC.


Fatigue or Environmental Cracking Corrosion

Environmental cracking is a corrosion process that can result from a combination of environmental conditions affecting the metal. Chemical, temperature, and stress-related conditions can result in the following types of environmental corrosion:


(i) Stress corrosion cracking.

(ii) Corrosion fatigue.

(iii) Hydrogen-induced cracking.

(iv) Liquid metal embrittlement.


High-Temperature Corrosion

Fuels used in gas turbines, diesel engines, and other machinery, which contain vanadium or sulfates during combustion can form compounds with a low melting point. These compounds are very corrosive towards metal alloys normally resistant to high temperatures and corrosion, including stainless steel. High-temperature corrosion can also be caused by high-temperature oxidization, sulfidation, and carbonization. The American Society of Metals (ASM) classified various corrosion types as given in Table.1.


Table.1: ASM Classifications of Corrosion Types


General Corrosion

Localized Corrosion

Metallurgically Influenced Corrosion

Mechanically Assisted Degradation

Environmentally Induced Cracking

Corrosive attack dominated by uniform thinning

High rates of metal penetration of specific sites

Affected by alloy chemistry and heat treatment

Corrosion with a mechanical component

Cracking produced by corrosion, in the presence of stress

• Atmospheric corrosion

• Galvanic corrosion

• Stray-current corrosion

• General biological corrosion

• Molten salt corrosion

• Corrosion in liquid metals

• High–temperature corrosion

• Crevice corrosion

• Filiform corrosion

• Pitting corrosion

• Localized biological corrosion

• Intergranular corrosion

• Dealloying corrosion

 

 

• Erosion corrosion

• Fretting corrosion

• Cavitations and water drop impingement

• Corrosion fatigue

 

 

• Stress – Corrosion Cracking (SCC)

• Hydrogen Damage

• Liquid metal embrittlement

• Solid metal-induced embrittlement

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