Issue 30

S. Baragetti et alii, Frattura ed Integrità Strutturale, 30 (2014) 84-94; DOI: 10.3221/IGF-ESIS.30.12 86 the environment on different loading conditions, in terms of fatigue strength reduction. The results of an experimental campaign on the quasi-static SCC characterization of the Ti-6Al-4V alloy in methanol at different concentrations are reported, and a comparison with the fatigue data is drawn. A numerical model for the crack propagation rate for the Ti- 6Al-4V alloy is proposed, in order to provide a tool to decouple the mechanical effects from the chemical driving forces. M ATERIALS AND M ETHODS he specimens for the corrosion fatigue characterization in air, 3.5 wt. % NaCl water mixture, methanol water mixture [11] and for the quasi-static testing in methanol water mixture were obtained from the same Ti-6Al-4V raw plate supply. The flat dogbone specimens were machined with a reasonable notch, according to the geometry presented in Fig. 2, in order to obtain failure in the test section with inferior loads. The test section area was of 45 mm 2 , while the local stress concentration factor K t was 1.18, as obtained by a linear elastic FE simulation with plane-stress elements. The specimens were machined so that the load axis was transversal to the rolling direction of the raw Ti-6Al-4V supply plate. The chemical composition, tensile properties and successive heat treatments are reported in Tab. 2. 260 ±0,5 80 ±0,2 15 3 ±0,05 30 Figure 2 : Specimen geometry. Chemical Composition Al [%] V [%] Fe [%] O [%] C [%] Ti [%] 5.97 4.07 0.20 0.1885 0.03 Bal. Raw Plate Mechanical Characterization Heat Treatments R p,02 [MPa] R m [MPa] E [MPa] 1. Solution treatment 2. Overaging 3. Stress relieving after machining 1’050 1’100 130’000 925 °C – 1 h 700 °C – 2 h Table 2 : Ti-6Al-4V chemical and mechanical characteristics – including thermal treatments. Axial fatigue loading ( R = 0.1) was imposed in the corrosion fatigue testing [11,12] in air, 3.5 wt. % NaCl water mixture and methanol water mixture at different wt. % methanol concentrations. The corrosive environment surrounded the test area of the specimens, by means of a containment device that allowed environment recirculation by means of a pump. The specimens were loaded using rolling bearing grips in order to avoid parasite bending moments during testing. A picture of the test device is reported in Fig. 3, while the tested environments are reported in Tab. 3. Step-loading technique, validated by Bellows et al. [12] and Lanning et al. [13], was adopted to obtain fatigue limits at 200’000 cycles. The 200’000 cycles number was selected by observing the S-N fatigue data of Sadananda et al. [14], where it is found that the R = -1 specimens reach a constant limit, and the steepness of the R = 0.1 test results decreases significantly. Specimens were tested at a given maximum stress, and if they reached the end of the cycles block without a failure, the load was increased and the test was restarted. The final fatigue limit was obtained by a linear interpolation between the failed load block and the previous not failed block, according to the formula: T