| Precipitation Hardening |
Article Index for Precipitation |
Information AboutPrecipitation Hardening |
| CATEGORIES ABOUT PRECIPITATION STRENGTHENING | |
| metals processes | |
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KINETICS VS. THERMODYNAMICS This technique exploits the phenomenon of Supersaturation , and involves careful balancing of the driving force for precipitation and the thermal activation energy available for both desirable and undesirable processes. Nucleation occurs at a relatively high temperature (often just below the solubility limit) so that the Kinetic barrier of Surface Energy can be more easily overcome and the maximum number of precipitate particles can form. These particles are then allowed to grow at lower temperature in a process called ''aging''. This is carried out under conditions of low Solubility so that Thermodynamics drive a greater total volume of precipitate formation, Diffusion's exponential dependence upon temperature makes precipitation strengthening (like all Heat Treatment s) a fairly delicate process. Too little diffusion (''under aging''), and the particles will be too small to impede dislocations effectively; too much (''over aging''), and they will be too few and far between to interact with the majority of dislocations. ALLOY DESIGN Precipitation strengthening is possible if the line of solid solubility slopes strongly toward the center of a Phase Diagram . While a large volume of precipitate particles is desirable, little enough of the alloying element should be added that it remains easily soluble at some reasonable annealing temperature. Elements used for precipitation strengthening of typical aluminium and titanium alloys make up about 10% of their composition. While binary alloys are more easily understood as an academic exercise, commercial alloys often use three components for precipitation strengthening, in compositions such as Al( Mg , Cu ) and Ti(Al, V ). A large number of other constituents may be unintentional, but benign, or may be added for other purposes such as Grain Refinement or Corrosion resistance. Many alloy systems allow the aging temperature to be adjusted. For instance, some aluminium alloys used to make Rivets for aircraft construction are kept in Dry Ice from their initial heat treatment until they are installed in the structure. After this type of rivet is deformed into its final shape, aging occurs at room temperature and increases its strength, locking the structure together. Higher aging temperatures would risk over-aging other parts of the structure, and require expensive post-assembly heat treatment. SOME PRECIPITATION HARDENING MATERIALS
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