Search Results

A main requirement for a satisfactory function and service life of a forged powder metal connecting rod is the fatigue strength. Fatigue strength mainly depends on design, material, microstructure, and surface condition. Much work has been accomplished to optimize these factors, but still a variety of surface defects such as localized porosity, roughness, oxide penetration, decarburization, etc., can be developed during manufacturing. These surface defects impact the fatigue strength in various ways. The impact of the decarburized layer depth on the fatigue life of a forged powder metal connecting rod is the focus of this work. Several connecting rods were submitted to a Weibull test at the same loading pattern. After the fatigue tests, the connecting rods were divided into groups with different decarburized layer depths. Both Maximum Likelihood Estimates (MLE) and Rank Regression (RR) techniques were used to analyze test results from all the groups obtained.

Increased use of powder-forged connecting rods in the automotive industry prompted an investigation into the suitability of powders from different suppliers for this application. Specifications developed by North American users call for ultra clean powders to enhance machinability and fatigue life. Powders from four manufacturers were each blended with graphite and lubricant, then pressed, sintered and forged to full density. Metallographic samples were prepared and evaluated for inclusion content. In addition, the powders were mixed to the composition of connecting rods, (C - 0.5%, Cu - 2% and MnS - 0.3%), and were similarly pressed, sintered and forged. Test bars were machined from the forged discs. Uniaxial fatigue tests were performed in the tension-compression mode and strain-life curves were developed. It was determined that all powders examined were very clean and were comparable in their inclusion content.

Shot peening is a commonly used surface treatment process used to improve the fatigue life of aircraft, automotive and other highly stressed structural components. This improvement is attributed to the formation of compressive residual stress on the surface layer of the material by the impingement of spherical media (shot). The compressive residual stress usually decreases the tensile stress created in the component by “in service” external forces and therefore increases the fatigue strength of the part. To quantify the improvement resulting from shot peening, the fatigue behavior of powder-forged connecting rods and laboratory test bars from the base material (2% copper steel), both in the stress-free (unpeened) and surface treated (shot peened) condition were compared. The fatigue data were correlated with the residual stress generated at the surface. The stress magnitude and depth were determined using x-ray diffraction analysis.