Overview
ABSTRACT
The basic principles of the metallurgy of titanium alloys are presented with the different classes of alloys and the static evolutions of the various phases. This article presents heat treatments in the implementation of products and covers the fundamental aspects which rule softening and hardening treatments. The means in which to, more specifically, favor a particular property is highlighted and industrial practices presented.
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Read the articleAUTHOR
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Yves COMBRES: Ingénieur Civil des Mines, PhD in Materials Science & Engineering - Director of China Partnerships at CEZUS
INTRODUCTION
The element titanium, Ti in the periodic table, was discovered in 1790. However, the difficulty of its extractive metallurgy meant that industrial production did not begin until the 1950s. Titanium and its alloys have attractive characteristics (low density, good corrosion resistance, high mechanical properties, transformation by conventional processes, non-magnetism...).
Mainly used in the chemical and aeronautical industries, titanium and its alloys also have important applications in the medical sector, thanks to their biocompatibility, and Young's moduli that can be quite low (70 GPa) and quite close to that of bone tissue. Heat treatment plays a key role in the processing of titanium and its alloys.
Having established the basic principles of titanium alloy metallurgy, and in particular the different classes of alloys, it is necessary to characterize the static evolution of the various phases during these treatments. This allows us to introduce the notions of softening and hardening, and thus to attempt to promote more specifically a mechanical property. Finally, the practical aspects of industrial production need to be presented.
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KEYWORDS
metallurgy | aeronautics | medicals | automotive | chemicals | micrography | mechanical tests | heat treatment
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Metal treatments
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Heat treatment of titanium alloys
Bibliography
Standards
American National Standards Institute (ANSI)
- Military Specification (MIL). Heat treatment of titanium and titanium alloys. - MIL-H-81200 A -
- Aerospace Materials Specifications (AMS). Titanium alloys. - AMS 4 900 à AMS 4 998 -
Society of Automotive Engineers (SAE)
Battelle Columbus Laboratories
Aerospace structural metals handbook...
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