Big Chemical Encyclopedia

Chemical substances, components, reactions, process design ...

Articles Figures Tables About

Alloy surface oxidation

Figure 10. AES depth composition profile of an Incoloy 800 alloy surface oxidized at 550°C for... Figure 10. AES depth composition profile of an Incoloy 800 alloy surface oxidized at 550°C for...
This chapter is arranged as follows experimental strategies for direct determination of surface structure are discussed. Experimental findings are then presented in the areas of ionic adsorption, electrodeposition, alloy surface oxidation, and organic molecular adsorption. [Pg.1]

Note finally that, as mentioned in the Introduction, the corrosion of the substrate may also damage irreversibly a microstructured device under the severe conditions of fuel processing reactions. For example, under water vapor pressure, many detrimental effects can occur, such as surface migration of Ni in stainless-steel alloys, surface oxidation of metals (Fe to Fe203), surface enrichment with trace elements able to alloy/react with the coated catalyst (Sn, Pb, Cl ions) and poison it or surface substrate restructuring. [Pg.1082]

This is essentially a corrosion reaction involving anodic metal dissolution where the conjugate reaction is the hydrogen (qv) evolution process. Hence, the rate depends on temperature, concentration of acid, inhibiting agents, nature of the surface oxide film, etc. Unless the metal chloride is insoluble in aqueous solution eg, Ag or Hg ", the reaction products are removed from the metal or alloy surface by dissolution. The extent of removal is controUed by the local hydrodynamic conditions. [Pg.444]

Skiving is a variant in which the base metal surface oxides are mechanically removed foUowed immediately by pressure rolling of a precious metal or alloy strip. This is commonly used for inlays for electrical contacts and for jewelry fabrication. The common inlay materials include gold, silver, copper, brass, and solder. No heat is needed, and the coating is appHed only to designated areas so there is Htde waste (3,50). [Pg.138]

TaC to obstruct the dislocations and (c) to form a protective surface oxide film of Cr203 to protect the blade itself from attack by oxygen (we shall discuss this in Chapter 22). Figure 20.3 (a and b) shows a piece of a nickel-based super-alloy cut open to reveal its complicated structure. [Pg.200]

Because oxides are usually quite brittle at the temperatures encountered on a turbine blade surface, they can crack, especially when the temperature of the blade changes and differential thermal contraction and expansion stresses are set up between alloy and oxide. These can act as ideal nucleation centres for thermal fatigue cracks and, because oxide layers in nickel alloys are stuck well to the underlying alloy (they would be useless if they were not), the crack can spread into the alloy itself (Fig. 22.3). The properties of the oxide film are thus very important in affecting the fatigue properties of the whole component. [Pg.223]

The Ni-base alloy surface is exposed to an oxidizing gas, oxide nuclei form, and a continuous oxide film forms (Ni) (Cr203, etc.)- This oxide film is a protective layer. The metal ions diffuse to the surface of the oxide layer and combine with the molten Na2S04 to destroy the protective layer. Ni2S and Cr2S3 results sulfidation) ... [Pg.421]

At elevated temperatures where titanium alloys could be the adherend of choice, a different failure mechanism becomes important. The solubility of oxygen is very high in titanium at high temperatures (up to 25 at.%), so the oxygen in a CAA or other surface oxide can and does dissolve into the metal (Fig. 12). This diffusion leaves voids or microcracks at the metal-oxide interface and embrittles the surface region of the metal (Fig. 13). Consequently, bondline stresses are concentrated at small areas at the interface and the joint fails at low stress levels [51,52]. Such phenomena have been observed for adherends exposed to 600°C for as little as 1 h or 300°C for 710 h prior to bonding [52] and for bonds using... [Pg.961]

Fig. 1.84 Surface of a Cu-IONi alloy after oxidation in oxygen at 500°C, showing blistering, probably associated with CuO formation over voids at the metal/oxide interface (courtesy Central Electricity Research Laboratories)... Fig. 1.84 Surface of a Cu-IONi alloy after oxidation in oxygen at 500°C, showing blistering, probably associated with CuO formation over voids at the metal/oxide interface (courtesy Central Electricity Research Laboratories)...
Contact with steel, though less harmful, may accelerate attack on aluminium, but in some natural waters and other special cases aluminium can be protected at the expense of ferrous materials. Stainless steels may increase attack on aluminium, notably in sea-water or marine atmospheres, but the high electrical resistance of the two surface oxide films minimises bimetallic effects in less aggressive environments. Titanium appears to behave in a similar manner to steel. Aluminium-zinc alloys are used as sacrificial anodes for steel structures, usually with trace additions of tin, indium or mercury to enhance dissolution characteristics and render the operating potential more electronegative. [Pg.662]

Acid pickles Some of the acid pickles used to clean and etch aluminium alloy surfaces and remove oxide and anodic films, such as the chromic/ sulphuric acid pickle (method O of DEF STAN 03-2) and other chromic-acid bearing pickles (App. Foi DEF-151) probably leave on the surface traces of absorbed or combined chromate which will give at least some protection against mild atmospheres. [Pg.725]

Deterioration of electrode performance due to corrosion of electrode components is a critical problem. The susceptibility of MHt electrodes to corrosion is essentially determined by two factors surface passivation due to the presence of surface oxides or hydroxides, and the molar volume of hydrogen, VH, in the hydride phase. As pointed out by Willems and Buschow [40], VH is important since it governs alloy expansion and contraction during the charge-discharge cycle. Large volume changes... [Pg.217]


See other pages where Alloy surface oxidation is mentioned: [Pg.460]    [Pg.95]    [Pg.460]    [Pg.95]    [Pg.112]    [Pg.137]    [Pg.194]    [Pg.226]    [Pg.26]    [Pg.122]    [Pg.170]    [Pg.363]    [Pg.104]    [Pg.96]    [Pg.132]    [Pg.139]    [Pg.263]    [Pg.263]    [Pg.912]    [Pg.978]    [Pg.1011]    [Pg.1011]    [Pg.1014]    [Pg.1046]    [Pg.1273]    [Pg.100]    [Pg.388]    [Pg.389]    [Pg.687]    [Pg.218]    [Pg.223]    [Pg.142]    [Pg.309]    [Pg.318]    [Pg.324]    [Pg.118]    [Pg.255]   


SEARCH



Alloy single-crystal surface, thin anodic oxide overlayers

Ruthenium alloys surface oxidation

Surface alloy

Surface alloying

Surface oxide film, aluminum-based alloys

Surface structure oxidized alloys, correlation

© 2024 chempedia.info