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MIC Green Book

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C H A P T E R T W O<br />

RESPONSE OF METALS<br />

12<br />

TITANIUM<br />

High Cycle Fatigue (HCF) - HCF of titanium is<br />

illustrated by Figure 2-4, which compares the<br />

capabilities of titanium alloy connecting rods<br />

for a high performance European sports car.<br />

The rods are manufactured using various<br />

processes. With shot peening, the fatigue<br />

limit was increased by approximately 20%<br />

while weight was reduced by some 40% as<br />

compared to steel connecting rods [Ref 2.12].<br />

Low Cycle Fatigue (LCF) - As is typical with<br />

other metals, the fatigue response with shot<br />

peening increases with higher cycle fatigue.<br />

Higher cycle fatigue would be associated with<br />

lower stresses whereas lower cycle fatigue<br />

would be associated with higher stress levels.<br />

This is demonstrated graphically in the S-N<br />

Curve (Figure 1-4) and also Figure 2-5.<br />

Figure 2-4 Comparison of Fatigue Strengths for Polished<br />

and Shot Peened Titanium Ti6A14V<br />

Figure 2-5 shows the results of shot peening<br />

titanium dovetail slots on a rotating engine<br />

component [Ref 2.13]. There are two baseline<br />

load curves that are not shot peened. When<br />

shot peening is applied, the base line curve<br />

that initially had more cycles to failure<br />

responded significantly better. Note that<br />

improvements in fatigue life are on an<br />

exponential basis.<br />

Figure 2-5 LCF Benefits from Shot Peening Notched Ti8-1-1<br />

The most common application of LCF for<br />

titanium is the rotating turbine engine hardware (discs, spools, and shafts) with the exception of blades. These<br />

components are shot peened to increase durability. Each takeoff and landing is considered one load cycle.<br />

MAGNESIUM<br />

Magnesium alloys are not commonly used in fatigue applications. However, when used for the benefit of weight<br />

reduction, special peening techniques can be employed to achieve 25 - 35% improvement in fatigue strength.<br />

POWDER METALLURGY<br />

Optimized peening parameters have been shown to raise the endurance limit of sintered steel PM alloys by<br />

22% and the fatigue life by a factor of 10. [Ref. 2.14] Automotive components such as gears and connecting<br />

rods are candidates for PM with shot peening. Shot peening is most effective on higher density PM parts<br />

such as forged powder metal components.<br />

Surface densification by shot peening can increase the fatigue limit significantly, especially in the case of<br />

bending. The surface densification also assists in the closing of surface porosity of PM components for<br />

sealing and other engineering applications.<br />

www.metalimprovement.com

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