TITEL
Effect of high-pressure cooling on the residual stress in Ti-alloys during machining
FöRFATTARE
Vosough, Manouchehr
INSTITUTION
Polhemslaboratoriet
SAMMANFATTNING
Titanium alloys are widely used in aerospace industry but also in other
industry sectors. Details for compressors used for generation and
petrochemical plants and medical devices can be mentioned as a few examples.
Plastic deformation during forming of the metals introduces residual
stresses. Fatigue, creep and corrosion are typical failure mechanisms that
are stopped or accelerated in the presence of tensile residual stress. Metal
cutting as a manufacturing method generates residual stresses in the surface
layer. The stress state in the near-surface zone of components is of special
interest as the surface often suffers loads and consequently the cracks
initiate and begin to grow at that location. The scope of this thesis is to
investigate the properties of the machined surface with regards to
measurement of residual stresses. The results achieved by X-ray
diffractometry were compared with the results using a simulating method with
the same cutting data for checking the accuracy of these two methods.
This review highlighted the residual stress character and how they can be
measured by X-ray diffractometry in two different directions, the
transversal, the cutting direction, and longitudinal, the feed direction.
For measurement of residual stress under the surface, the material was
removed by an electro-chemical polishing method for not introducing more
stress. The same procedure was checked using Finite Element simulations.
The results obtained from the investigation clarified that:
- The residual stress measurement by X-rays was quite accurate in
comparison with finite element simulation on the surface generated by
turning on titanium alloy.
- There were compressive residual stresses in the cutting and feed
directions of the cut. Residual stress is beneficial for delay of crack
propagation.
- High-pressure cooling produced and increased compressional residual
stresses.
ISSN 1402-1757 / ISRN LTU-LIC--05/46--SE / NR 2005:46
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