This article discusses the role of alloying in the production and use of titanium. It explains how alloying elements affect transformation temperatures, tensile and creep strength, elasticity, hardness, and corrosion behaviors. It provides composition and property data for commercial grades of titanium, addresses processing issues, and identifies operating environments where certain titanium alloys are susceptible to stress-corrosion cracking.

This chapter is a detailed account of the history of development of titanium and its modern applications in the aerospace market. It begins by discussing the attempts made to produce titanium metal. This is followed by a discussion on the invention of a process for making titanium by William Kroll. Various studies on the properties on titanium and research programs related to the production of titanium sponge and titanium metal products are then described. The chapter concludes with a discussion of titanium use in jet engines.

This chapter familiarizes readers with the machining characteristics of titanium and the implementation of machining and shaping processes. It explains why titanium alloys are more difficult to machine than other metals and how it impacts the equipment and procedures that can be used. It describes the basic machining requirements for titanium in terms of tool geometry and materials, machine setup rigidity, cutting speeds and feed rates, and surface conditions, and explains how the requirements are met in practice in milling, turning, drilling, surface grinding, and broaching operations. The chapter also covers chemical and electrochemical machining processes as well as flame cutting.

This chapter describes the applications with the greatest impact on titanium consumption and global market trends. It explains where, how, and why titanium alloys are used in aerospace, automotive, chemical processing, medical, and military applications as well as power generating equipment, sporting goods, oil and gas production, and marine vessels.

Titanium alloys are classified according to the amount of alpha and beta phase material retained in their structures at room temperature. This chapter discusses the metallurgy, composition, processing, and properties of titanium and its alloys. It provides information on melting, forging, casting, heat treating, and secondary fabrication. It also discusses the advantages and disadvantages of titanium and its alloys in various applications.

This appendix provides datasheets on high purity titanium, describing its processing characteristics, mechanical and fabrication properties, and heat treating practices.

This chapter provides a general overview of titanium and its versatility as an engineering material.

Titanium is a lightweight metal used in a growing number of applications for its strength, toughness, stiffness, corrosion resistance, biocompatibility, and high-temperature operating characteristics. This chapter discusses the applications, metallurgy, properties, compositions, and grades of commercially pure titanium and alpha and near-alpha, alpha-beta, and beta titanium alloys. It describes primary and secondary fabrication processes, including melting, forging, forming, heat treating, casting, machining, and joining as well as powder metallurgy and direct metal deposition. It also compares and contrasts the properties of wrought, cast, and powder metal titanium products and discusses corrosion behaviors.

Titanium aluminides are lightweight materials that have relatively high melting points and good high-temperature strength. They also tend to be stronger and lighter than conventional titanium alloys, but considerably less ductile. This chapter begins with a review of the titanium-aluminum phase diagram, focusing on the properties, compositions, and microstructures of alpha-2 Ti3Al alloys. It then describes the properties, microstructures, and compositions of orthorhombic, gamma, and near-gamma alloys as well as the processing methods and procedures normally used in their production.

This appendix provides tensile property data for titanium alloys and castings and plane-strain fracture toughness data for Ti-6Al-4V castings.

This appendix provides tensile property and fracture toughness data for titanium aluminides developed for aerospace applications.

This appendix contains several tables listing UNS numbers, common names, and descriptions of important titanium alloys and where they are typically used.

This appendix describes the information contained in titanium alloy datasheets and defines the many abbreviations that are used.

This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of commercially pure and modified titanium. The datasheets address four grades of unalloyed titanium (ASTM Grade 1, UNS R50250; ASTM Grade 2, UNS R50400; ASTM Grade 3, UNS R50550; and ASTM Grade 4, UNS R50700), two grades of modified titanium (ASTM Grade 7, UNS R52400; and ASTM Grade 11, UNS R52250), and alloy Ti-0.3Mo-0.8Ni (ASTM Grade 12, UNS R53400).

This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of alpha and near-alpha titanium alloys. Datasheets are provided for the following alloys: Ti-3Al-2.5V (ASTM Grade 9, UNS R56320), Ti-5Al-2.5Sn (UNS R54520/R54521), Ti-6Al-2Nb-1Ta-0.8Mo (UNS R56210), Ti-6Al-2Sn-4Zr-2Mo-0.08Si (UNS R54620), Ti-8Al-1Mo-1V (UNS R54810), and Ti-6Al-2.75Sn-4Zr-0.4Mo-0.45Si (Ti-1100).

This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of various grades of alpha-beta titanium. Datasheets are provided for the following alloys: Ti-5Al-2Sn-2Zr-4Mo-4Cr (UNS: R58650, Ti-17); Ti-6Al-2Sn-4Zr-6Mo (UNS R56260, Ti-6246); Ti-6Al-4V (UNS R56400) and Ti-6Al-4V ELI (UNS R56401); Ti-6Al-6V-2Sn (UNS R56620, Ti-662); Ti-7Al-4Mo (UNS R56740); Ti-6Al-1.7Fe-0.1Si (TiMetal 62S); Ti-4.5Al-3V-2Mo-2Fe (SP-700); Ti-6Al-7Nb (IMI 367); Ti-4Al-4Mo-2Sn-0.5Si (IMI 550); Ti-4Al-4Mo-4Sn-0.5Si (IMI 551); Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.25Si (Ti-6-22-22S); Ti-5Al-2.5Fe (DIN 3.7110, Tikrutan LT 35); and Ti-5Al-5Sn-2Zr-2Mo-0.25Si (UNS R54560, Ti-5522-S).

This appendix provides datasheets describing the chemical composition, processing characteristics, mechanical and fabrication properties, and heat treating of beta and near-beta titanium alloys. Datasheets are provided for the following alloys: Ti-11.5Mo-6Zr-4.5Sn (UNS R58030, Beta III); Ti-3Al-8V-6Cr-4Mo-4Zr (UNS R58640, Beta C and 38-6-44); Ti-10V-2Fe-3Al (Ti-10-2-3); Ti-13V-11Cr-3Al (UNS R58010, Ti-13-11-3); Ti-15V-3Al-3Cr-3Sn (Ti-15-3); Ti-15Mo-3Al-2.7Nb-0.25Si (UNS R58210, TiMetal 21S and Beta 21S); Ti-5Al-2Sn-4Zr-4Mo-2Cr-1Fe (Beta CEZ); Ti-8Mo-8V-2Fe-3Al (Ti-8823); Ti-15Mo-5Zr; Ti-15Mo-5Zr-3Al; Ti-11.5V-2Al-2Sn-11Zr (T129); Ti-12V-2.5Al-2Sn-6Zr (T134); Ti-13V-2.7Al-7Sn-2Zr (T175); Ti-8V-5Fe-1Al; and Ti-16V-2.5Al.

This appendix serves as a cross reference to chemically similar titanium alloys and the various designations by which they are known.

Titanium is a lightweight metal with a density approximately 60% that of steel and, through alloying and deformation processing, it can be just as strong. It is readily available in many grades and forms and can be further processed using standard methods and techniques. This chapter provides a concise review of the capabilities of titanium and its design advantages over other materials. It includes information on properties and selection factors as well as applications.