The crack coalescence in some materials is known to make influence on the failure life significantly in low cycle fatigue as well as corrosion fatigue. A model was proposed to simulate crack linking during fatigue process. The crack distribution observed experimentally was idealized by a two-dimensi
Low Cycle Fatigue Life Threshold for Titanium Aluminides
✍ Scribed by Thomas K. Heckel; Hans-Jürgen Christ
- Publisher
- John Wiley and Sons
- Year
- 2010
- Tongue
- English
- Weight
- 323 KB
- Volume
- 12
- Category
- Article
- ISSN
- 1438-1656
No coin nor oath required. For personal study only.
✦ Synopsis
Abstract
Although there exists a good understanding of dislocation glide mechanisms during fatigue of titanium aluminides,1 fatigue life prediction remains a crucial issue because of the low amount of macroscopic plastic strain and the existence of microstructural inhomogeneities. The concept proposed here aims at a threshold value, allowing a reasonable low cycle fatigue life for isothermal and thermomechanical fatigue conditions. It can be stated that under isothermal testing conditions a maximum strain amplitude of Δε/2 = 0.35% (corresponding to a stress amplitude of about Δσ/2 = 500 MPa) for temperatures up to 750 °C is feasible for TNB‐V2 in order to reliably reach a sufficient LCF life. Concerning satisfactory thermomechanical fatigue life the proposed concept suggests that the acting combination of mean stress and strain amplitude needs to be located below the Goodman line. It can be concluded that with increase in maximum cyclic temperature and temperature range, the tolerable strain amplitude decreases. Because of the well‐documented unfavorable combination of tensile mean stresses and environmental attack during OP‐TMF, an acceptable strain amplitude for TMF conditions is significantly lower than under isothermal conditions.
📜 SIMILAR VOLUMES
This paper describes the crack propagation rate and the failure life in the biaxial low cycle fatigue test for a type 304 stainless steel at elevated temperatures. Macro crack propagation rates were observed for the tubular specimen in the push-pull and the reversed torsion tests. The crack propagat
Low-cycle fatigue tests were conducted by tension-tension until rupture, on a 2026T3 aluminum alloy sheet. Initial crack sizes and orientations in the fatigue specimens were found to be randomly distributed. Acoustic emission was continuously monitored during the tests. Every few hundred cycles, the
Experimental results show that the inherent ductility in a material is deflected after cycle loading. Based on the concept of ductility deflection, a new fatigue damage variable D\* for low-cycle fatigue is recommended in this paper. This new damage variable D\* has definite physical meaning and can