Materials for engineering, 3rd Edition - (Malestrom)
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Metals and alloys 83<br />
were constructed from the results of fatigue tests and the endurance limits<br />
were determined <strong>for</strong> each specimen design.<br />
It is seen that identical values of endurance limit were obtained <strong>for</strong> specimens<br />
with fillet radii of 250 and 25 mm. When the fillet radius was reduced to<br />
6.5 mm, however, it is seen that a significant drop in endurance limit took<br />
place, due to the concentration of stress in the surface associated with the<br />
sharp change in cross-section. In specimens containing a sudden step or<br />
a sharp notch, the magnitude of the endurance limit decreases further,<br />
being in the notched specimen less than half of that measured in the smooth<br />
specimens.<br />
Fatigue-resistant microstructures<br />
Fatigue cracks may nucleate at stress concentrations at weak internal surfaces<br />
and interfaces in a material, as well as at the external surface. Internal voids<br />
and cavities are there<strong>for</strong>e undesirable and such features as blowholes and<br />
shrinkage cavities in castings, as well as imperfect welds in fabricated<br />
components are obviously deleterious. Careful non-destructive testing is<br />
often applied to critical components in order to minimize the danger of<br />
fatigue failure originating from internal defects of this sort.<br />
Coarse inclusions of a second phase can also provide a source of local<br />
internal stress, leading to the early nucleation of fatigue cracks. Coarse<br />
graphite inclusions are present in many cast irons and are the origin of their<br />
poor fatigue resistance. Inclusions of slag etc. may be present in steel, and<br />
sophisticated techniques such as vacuum melting and degassing are employed<br />
to produce ‘clean steels’ with enhanced properties. Coarse inclusions of<br />
intermetallic phases may be present in a wide range of alloys if special<br />
precautions are not taken; <strong>for</strong> example, a low iron content is specified in<br />
aluminium alloys <strong>for</strong> aerospace applications in order to minimize the occurrence<br />
of such particles.<br />
Surface treatment of a component is a widely employed method of enhancing<br />
resistance to fatigue failure and a number of approaches are possible. Clearly,<br />
surface finish is important and the removal of scratches and machining marks<br />
can be significant in this context, with surface polishing being a further<br />
possibility. Secondly, surface hardening can be employed to inhibit fatigue;<br />
this can be effected in several ways:<br />
(a) Work hardening a shallow surface layer can be achieved by ‘shot blasting’<br />
or ‘shot peening’. Surface rolling also enhances fatigue resistance <strong>for</strong><br />
the same reason. The beneficial effect will be reduced, of course, if the<br />
treatment introduces any roughening of the surface.<br />
(b) In steels, surface hardening can be achieved by changing the surface<br />
composition by diffusion heat-treatment of the component. Nitriding is