Abstract

Titanium alloys have been used in aerospace, aeronautic, automotive, biomedical, structural, and other applications because titanium alloys have less density than materials like steel and support higher stress than Al-alloys. However, components made of titanium alloys are exposed to corrosive environments, the most common being industrial and marine atmospheres. This research shows the corrosion behavior of three titanium alloys, specifically Ti-CP2, Ti-6Al-2Sn-4Zr-2Mo, and Ti-6Al-4V with α, near α, and α + β alloys phases. Alloys were exposed in two electrolytes to a 3.5 wt. % H2SO4 and NaCl solution at room temperature, and their electrochemical behavior was studied by electrochemical noise technique (EN) according to ASTM ASTM-G199 standard. EN signal was filtered by three different methods, and the polynomial method was employed to obtain Rn, kurtosis, skew, and the potential spectral density analysis (PSD). The wavelets method was used, from which energy dispersion plots were obtained. The last method was Hilbert–Huang Transform (HHT), where Hilbert Spectra were analyzed. Results indicated that Rn compared with PSD showed that Ti-6Al-2Sn-4Zr-2Mo presented less dissolution in both electrolytes. Statistical methods showed that the passive layer created on Ti alloys’ surfaces is unstable; this condition is notable for Ti-6Al-2Sn-4Zr-2Mo in NaCl solution.

Highlights

  • Titanium alloys were developed in the mid-1940s for the aviation industry

  • Two post-World War II alloys, commercially pure titanium (CPTi) and Ti-6Al-4V, remain the two dominant titanium alloys used in applications in aerospace, aeronautics, biomedical and automotive industries due to the density and mechanical and corrosion resistance properties being higher in comparison with competing materials such as aluminum, steels, and superalloys [1,2]

  • For potential spectral density analysis (PSD) analysis, it is necessary to transform the time-domain electrochemical noise technique (EN) to frequencydomain by applying FFT, since there is a correlation with EN signal, after which spectral density is calculated with Equations (9) and (10) [59]

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Summary

Introduction

Two post-World War II alloys, commercially pure titanium (CPTi) and Ti-6Al-4V, remain the two dominant titanium alloys used in applications in aerospace, aeronautics, biomedical and automotive industries due to the density and mechanical and corrosion resistance properties being higher in comparison with competing materials such as aluminum, steels, and superalloys [1,2] The use of these alloys increased significantly in the 1980s, in aircraft combat construction as opposed to transport aircraft. The aeronautical industry has an important role in the development and application of new materials and technologies because damage tolerance is especially low in this industry For this reason, materials should present excellent properties for service conditions, and constants optimization processes should be carried out to increases mechanical, fatigue, corrosion, and oxidation resistance, which should be certificated and satisfy security standards [3,4]. Characterization by electrochemical techniques of titanium alloys could find potential applications in the aeronautical industry as in turbine blades and aircraft landing gear

Materials
Microstructural Characterization
Electrochemical Techniques
OM-SEM Microstructural Analysis
PSD Analysis
HHT Analysis
SEM Corrosion Product Analysis
Conclusions
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