Grants and Contracts Details
Description
. ~urf~ce conditioning such as shot peening, laser shock peening, and low plasticity burnIshmg
Imparts on the metal parts so treated a thin layer of subsurface compressive residual
stress, which greatly enhances the high-cycle fatigue performance of the parts.
Both the Air Force and manufacturers of aircraft engines are very interested in incorporating
the beneficial effect of residual stress into component-life predictions. To this end,
(currently unavailable) nondestructive methods must be developed by which the profile of
the subsurface stress layer can be accurately and reliably measured or inferred, both before
and after the component is exposed to conditions common in the engine environment, e.g.,
cyclic thermal and mechanical loading, which may force stress relaxation to occur.
This proposed project comprises two parts. The main objective of the first part is:
. To develop a nondestructive ultrasound technique to extract information on the profile
of the inhomogeneous residual stresses induced by low plasticity burnishing (LPB) and
by shot peening on Ti-6AI-4V samples.
In our efforts we will continue and extend the very recent and promising exploratory study by
Man, Koo (GE Aircraft Engines), and Shepard (AFRL/MLLMN), where they successfully
inferred some characteristics of the residual stress profile in a LPB-treated Ti-6AI-4V sample
from the dispersion of Rayleigh waves in that sample.
The second part of the proposal concerns the effects of subsurface compressive residual
stress, micro- and macro-texture on the high-cycle fatigue performance of titanium alloys.
Our objectives are as follows:
. To study the effects of micro- and macro-texture on the high-cycle fatigue behavior of
alpha or near alpha Ti alloys with a view to building up a model that quantifies the
process of short fatigue crack propagation in these alloys.
. To investigate the possible change in subsurface texture induced by low plasticity
burnishing and shot peening as well as the effect of this change on fatigue behaviour
and on ultrasonic evaluation of stress in Ti-6AI-4V and other Ti alloys.
. To study how different stress profiles affect the fatigue properties of the Ti alloys, and
to determine the preferred subsurface condition for optimal fatigue performance.
Status | Finished |
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Effective start/end date | 6/1/02 → 10/31/05 |
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