Full Text Available
Note: Clicking the button above will open the full text document at the original institutional repository in a new window.
Of significant importance to the design, manufacture and maintenance of turbine components is the fatigue life thereof when subjected to variable loading conditions. Research and practical implementation has shown that shot peening considerably increases the fatigue life of a component by introducin...
| Main Author: | |
|---|---|
| Format: | Thesis |
| Language: | English |
| Published: |
Department of Mechanical Engineering
2015
|
| Subjects: | |
| Tags: |
No Tags, Be the first to tag this record!
|
| Summary: | Of significant importance to the design, manufacture and maintenance of turbine components is the fatigue life thereof when subjected to variable loading conditions. Research and practical implementation has shown that shot peening considerably increases the fatigue life of a component by introducing compressive residual stresses within the surface layers of the component. This has created a need to develop a numerical model that accurately predicts such residual stresses produced from shot peening. This thesis offers a simplified numerical model depiction of the shot peening process on a target material. A Finite Element based software (ABAQUS) model was employed to simulate the material behaviour and elastic-plastic deformation a metallic material undergoes during shot peening. An experimental platform was established by performing shot peening on material specimens while varying certain shot peening parameters. These parameters included shot size, shot velocity (related to a change in nozzle discharge pressure) as well as standoff (distance between exit nozzle and target material). The experimental data provided the stress profiles both on and beneath the target material surface layers and aided in the model development. Of specific interest was the magnitude of the maximum compressive residual stress developed just below the surface of the material and the depth of the compressive layer formed within the surface layers of the target material. |
|---|