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Metal Fatigue  

The graph below compares fatigue strength with ultimate tensile strength for bo
th smooth and notched specimens. Without shot peening optimal fatigue properties for machined steel components are obtained at approximately 30 HRc (700 MPa). At higher strength/hardness levels, materials lose fatigue strength due to increased notch sensitivity and brittleness. With the addition of compressive stresses from shot peening, however, fatigue strength increases proportionately to increasing strength/hardness. For example, at a 52 HRc (1240 MPa), the fatigue strength of the shot peened specimen is 144 ksi (988 MPa), more than twice the fatigue strength of the unpeened, smooth specimen.
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Comparison of peened and unpeened fatigue limits for smooth and notched specimens as a function of ultimate tensile strength of steel.

Manufacturing Processes - Effect on Fatigue Life

Manufacturing processes are known to have a significant effect on fatigue properties of parts. These effects can be either detrimental or beneficial, as represented by the chart below:

DETRIMENTAL BENEFICIAL
Hardening Carburizing
Grinding Honing
Machining Polishing
Plating Burnishing
Welding Rolling
EDM and ECM Shot Peening

On the detrimental side grinding, machining and welding all can leave the surface of the part in tension, a seedbed for fatigue cracks. Hardening, plating and EDM can leave a hard brittle surface. ECM can damage or weaken surface grain boundaries.

On the beneficial side all the listed processes improve metal fatigue life by virtue of the compressive stresses they induce. Shot peening is the most versatile of the list since it provides the highest magnitude of compressive stress in the greatest variety of materials and part configurations.

The graph below presents "s/n" (stress vs. number of cycles to failure) curves for different types of grinding. The base line curve is that for "gentle grind" specimens and shows fatigue strength of 60,000psi. A "severe grind" graph is shown just below and represents that condition produced from faster cutting speeds and/or the taking larger cuts. In this case large amounts of surface tensile stress, the seedbed of tensile fatigue cracks, are generated. As shown, fatigue strength decreases to 45,000 psi. The last graph presents the fatigue strength of "severe grind plus shot peened" specimens. As shown these specimens increased well beyond even the baseline "gentle grind", providing fatigue strength of over 80,000 psi. The compressive stresses generated by shot peening overcame the tensile stresses from severe grinding.

There are several ways of considering these benefits. First, shot peening allows an increased amount of stress to achieve the same component fatigue life. Second, shot peening extends the life of any part if the existing stress level is maintained. Thirdly, shot peening permits a greater range of acceptable manufacturing operations by providing a consistent surface compressive stress.

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Shot peening improves endurance limit of ground components.

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