Tantalum

Titanium

ti·ta·ni·um (circa 1791 William Gregor)A silvery gray light strong metallic element found combined in ilmenite and rutile and used especially in alloys (as steel) and combined in refractory materials and in coatings.

Titanium is number 22 on the periodic table. It has a melting point of 1668°C and a density of 4.54 gm/cc. Titanium properties and characteristics which are important to design engineers are excellent.  Titanium is immune to corrosive attack by salt water or marine atmospheres. It also exhibits exceptional resistance to a broad range of acids, alkalis, natural waters and industrial chemicals.

The combination of high strength and row density results in exceptionally favorable strength-to-weight ratios for titanium-based alloys. These ratios for titanium-based alloys are superior to almost all other metals and become important in such diverse applications as deepwell tubestrings in the petroleum industry and surgical implants in the medical field.  

Superior Strength-to-Weight Ratios The densities of titanium-based alloys range between .160 lb/in3 (4.43 gm/cm3) and .175 lb/in3 (4.85 gm/cm3). Yield strengths range from 25,000 psi (172 MPa) commercially pure (CP) Grade 1 to above 200,000 psi (1380 MPa) for heat treated beta alloys.

Titanium is immune to corrosive attack by salt water or marine atmospheres. It also exhibits exceptional resistance to a broad range of acids, alkalis, natural waters and industrial chemicals.  Titanium offers superior resistance to erosion, cavitation or impingement at-tack. Titanium is at least twenty times more erosion resistant than the copper-nickel alloys.

Titanium and titanium alloys have proven to be technically superior, highly reliable and cost-effective in a wide variety of chemical, industrial, marine and aerospace applications. Titanium is utilized in many critical services due to its unique set of properties.

Titanium can exist in two crystal forms.  The first is alpha which has a hexagonal close-packed crystal structure and the second is beta which has a body-centered cubic structure. In unalloyed titanium, the alpha phase is stable at all temperatures up to 1620°F. (880°C.) where it transforms to the beta phase. This temperature is known as the beta transus temperature. The beta phase is stable from 1620°F. (880°C.) to the melting point.

Physical Properties of Titanium
PROPERTY
Atomic Number22
Atomic Weight47.90
Density4.54 g/cc
Melting Point1941 K, 1668°C, 3034°F
Boiling Point3560 K, 3260°C, 5948°F
Electrical Resistivity (20°C)56 microhms-cm
Specific Heat502.440  J/(kg*K)
Thermal Conductivity16.44   W/(m*K)

Titanium, discovered by William Gregor in 1791, titanium was first isolated and named after the powerful mythological first sons of the Earth - the Titans, Titanium is most commonly associated with jet engines and airframes, but the most recent media attention has been given to fittings for prosthetic devices and the artificial heart.

To produce titanium, the basic ore, usually rutile (Ti02) is converted to sponge in two distinct steps. First, Ti02, is mixed with coke or tar and charged in a chlorinator. Heat is applied and chlorine gas is passed through the charge. The titanium ore reacts with the chlorine to form TiCl4, titanium tetrachloride, and the oxygen is removed as C0 and C02. The resultant crude TiCl4, produced is a colorless liquid and is purified by continues fractional distillation. It is then reacted with either magnesium or sodium under an inert atmosphere. This results in metallic titanium sponge, and either magnesium or sodium chloride which is reprocessed and recycled.

Melting is the second step. Titanium is converted from sponge to ingot by first blending crushed sponge with the desired alloying elements to insure uniformity of composition, and then pressing into briquettes, which are welded together to form an electrode. The electrode is melted in a consumable electrode vacuum  arc furnace where an arc is struck between the electrode and a layer of titanium in a water-cooled copper crucible. The molten titanium on the outer surface solidifies on contact with the cold wall, forming a shell or skull to contain the molten pool. The ingot is not poured, but solidifies under vacuum in the melting furnace. To insure homogeneity of the final ingot, a second or sometimes a third melting operation is applied.

Applications of Titanium

Titanium and its alloys have proven to be technically superior and cost-effective materials of constrLlction for a wide variety of aerospace, industrial, marine and commercial applications. In North America, approximately 70% of the titanium consumed is utilized for aerospace applications. Due to the expansion of existing applications and the development of new uses, the greatest growth will occur in the industrial, marine and commercial sectors.

In the Industrial & aerospace industry, titanium is currently being utilized in: Gas Turbine Engines, Heat Transfer, DSA-Dimensional Stable Anodes, Desalination, Extraction of Electrowinning of Metals, Medical, Hydrocarbon Pressing, Marine Applications, Chemical Processing, Steam Turbines, Automotive, Airframes, Space Structures, FGD (Flue Gas Desulfurization), Nuclear Waste Storage, etc. 

 

Common potent inhibitors for titanium in reducing acid media include dissolved oxygen, chlorine, bromine, nitrate, chromate, permanganate, molybdate and cationic metallic ions, such as ferric (Fe+3), cupric (Cu+2), nickelous (Ni+2) and many precious metal ions. Figure 2 shows how the useful corrosion resistance of unalloyed titanium is significantly extended as the ferric ion concentration is increased in very small amounts.  It is this potent metal ion inhibition phenomenon which permits titanium to be successfully utilized for equipment handling hot HCl and H2SO4 acid solutions in metallic ore leaching processes.

Although inhibition is possible in most reducing acids, protection of titanium from hydrofluoric acid solutions is extremely difficult to achieve. Hydrofluoric acid will generally cause rapid general corrosion of all titanium alloys, and should, therefore, be avoided.
Figure 2: Beneficial effect of minute ferric ion additions to corrosion resistance of unalloyed titanium in HCI and media.

Titanium Alloys

There are three structural types of titanium alloys:

As alloying elements are added to pure titanium, the elements tend to change the temperature at which the phase transformation occurs and the amount of each phase present. Alloy additions to titanium, except tin and zirconium, tend to stabilize either the alpha or the beta phase. Elements called alpha stabilizers stabilize the alpha phase to higher temperatures and beta stabilizers stabilize the beta phase to lower temperatures. 

Titanium alloys exhibit modulus of elasticity values which are approximately 5O% of steel. This low modulus means excellent flexibility which has been the basis for its use in dental fixtures (braces, etc.) and human prosthetic devices (hip joints, bone implants, etc.). Titanium's excellent compatibility provides an additional incentive for titanium's rapidly expanding use in body prosthetics. Other applications include springs, bellows, golf club shafts and tennis racquets. 

Titanium possesses a coefficient of expansion which is significantly less than ferrous alloys. This property also allows titanium to be much more compatible with ceramic or glass materials than most metals, particularly when metal-ceramic/glass seals are involved.

Corrosion Resistance

The environmental resistance of titanium depends primarily on a very thin, tenacious and highly protective surface oxide film. Titanium and its alloys develop very stable surface oxides with high integrity, tenacity and good adherence. The surface oxide of titanium will, if scratched or damaged, immediately reheal and restore itself in the presence of air or water.

The presence of common oxidizing background or contaminating species often maintain or extend the useful performance limits of titanium in many highly aggressive environments. These inhibitive species include air, oxygen, ferrous alloy corrosion products, other specific metallic ions, and/or other dissolved oxidizing compounds. Titanium's already wide range of application can be expanded by alloying with certain noble elements or by impressed anodic potentials (anodic protection).

Also titanium generally exhibits superior resistance to chlorides and various forms of localized corrosion.  Titanium alloys are considered to be essentially immune to chloride pitting and intergranular attack; and are highly resistant to crevice and stress corrosion.

Titanium is used in chloride salt solutions and other brines over the full concentration range, especially as temperatures increase. Near nil corrosion rates can be expected in brine media over the pH range of 3 to 11. Oxidizing metallic chlorides, such as FeCl3, NiCl2, or CuCl2, extend titanium's passivity to much lower pH levels.

A possible limiting factor of titanium alloy application in aqueous chlorides can be crevice corrosion in metal to metal joints, gasket to metal interfaces or under process stream deposits. Given these potential crevices in  hot chloride containing media, localized corrosion of unalloyed titanium and other alloys may occur depending on pH and temperature.

Working Characteristics

Once judged to be expensive, titanium, in life cycle costing, is now more often seen to be economical. The key to its cost-effective use is to utilize its unique properties and characteristics in the design rather than to substitute titanium for another metal.  Titanium is the world's fourth most abundant structural metal. It is found in North America, South America, Europe, Africa and Australia in the forms of ilmenite, rutile and other ores. The most widely used means of winning the metal from the ore is the Kroll process which uses magnesium as a reducing agent. Sodium is also used as a reducing agent by some producers.

The Properties and characteristics which are important to design engineers are:

Properties of Titanium Grades

Commercially Pure
Designation Grade 2 Ti-6A1-4V
Chemical
Composition

(Max. values unless range is shown)
 0.10C;0.30Fe;0.03 Ni;0.250;
0.015 H (sheet) 0.0125 H (bar)
0.0100H(billet)
.08C; 0.25 Fe;.05N0.20 0;5.50/
6.75 Al; 3.5/4.5 V; 0.0150 H(sheet)
0.0125 Htbar): 0.0100 H(billet)
Mill Annealed Tensile Properties Guar.R.T
Min.
Guar.R.T
Min.
Ultimate Strength (psi)    50,000 130,000
Yield Strength (psi) 0.1% offset 40,000 120,000
Elongation in 2" (%)Sheet>0.025 thick 20 10
Reduction in Area (%) Bar 30 25
Mechanical Properties (Typical)   600 Degree F 800 Degree F
Stress to Rupture
in Time Shown
Stress (psi)
Time (Hrs.)
  98,000
1,000
60,000
1,000
Stress and Time to
Produce Elongation
Shown (creep)
Stress (psi)
Time (Hrs.)
Creep (%)
  70,000
1,000
0.1
32,000
1,000
0.1
Charpy V-Notch Impact(ft.-lbs.)@Rm.Temp. 25-40 10-14
Bend Radius Under .070" thk.
.070" and Over
2.0 x Thickness
2.5 x Thickness
4.5 x Thickness
5.0 x Thickness
Welded Bend Radius 2.0-3.0 x Thickness 6.0-10.0 x Thickness
Hardness RB80 RC36
Physical Properties
Beta Transus (F±25) 1675 1830
Coefficient of
Thermal Expansion
(10 - 6inòinòF)
32-212 4.8 5.0
32-600 5.1 5.3
32-1000 5.4 5.6
32-1200 5.6 5.9
32-1500 5.6 6.1
Density (lbs._cu.in) 0.163 0.160
Melting Point, Approx. (F) 3020 3200
Electrical Resistivity@R.T. (Microhms cm) 56 171
Modulus of Elasticity - Tension (10-6 psi) 14.9 16.5
Modulus of Elasticity - Torsion (10-6 psi) 6.5 6.1
Thermal Conductivity (Btu/hr./sq.ft./F/Ft.) 9.5 at Room. Temperature 3.9 at Room. Temperature
Specific Heat (Btu/Lb,/F)@ Rm.Temp. 0.124 0.135
Weldability Good Fair
Annealing
Temp. (F)
Full
Stress Relief
1300/30 Min.-2 Hrs.;Air Cool
1000-1100/30 Min.-2 Hrs.;Air Cool
1300-1450/15 Min.-2 Hrs.;Air Cool
900-1200/1-4 Hrs.;Air Cool
Forging
Temp. (F)
Blocking
Finishing
1600-1700
1500-1600
1750-1800
1650-1750
Available Mill Products Bar; Billet; Extrusions
Plate; Sheet; Strip
Wire; Pipe; Tubing
Bar; Billet; Extrusions
Plate; Sheet; Strip
Wire
Typical Applications For corrosion resistance in the chemical and marine industries, and where a higher strength level and ease formability  is desired.  
Industry Specifications AMS 4902
ASTM B265 Gr2
ASTM B337 Gr2
ASTM B338 Gr2
ASTM B348 Gr2
ASTM B381 Gr2
ASTM F67   Gr2
ASTM F467 Gr2
ASTM F468 Gr2
AMS 4911
AMS 4928
AMS 4935
AMS 4965
AMS 4967
ASTM B265 Gr2
ASTM B348 Gr2
ASTM B381 Gr2
ASTM F467 Gr2
ASTM F468 Gr2

Titanium and its alloys possess many unique physical properties which make them ideal for equipment design, even when strength or corrosion resistance may not be critical. These unique properties include:

Titanium's low density, roughly 56% that of steel, means twice as much metal volume per pound. Particularly when combined with alloy strength, this often means smaller and/or lighter components. Although obviously the basis for aerospace applications, positive implications are also apparent for many types of rotating or reciprocating components such as centrifuges and pumps.

The relatively high melting point of titanium has led to consideration of titanium for ballistic armor. The higher melting point tends to reduce susceptibility to armor melting and ignition (burning) during ballistic impact. Good toughness and light weight are additional factors for considering titanium alloys in this application. 

Titanium is virtually non-magnetic, making it ideal for applications where electro-magnetic intencerence must be minimized. Desirable applications include electronic equipment housing and downhole well logging tools.

Titanium has an extremely short half-life, thereby permitting its use in nuclear systems. In contrast to many ferrous alloys, many titanium alloys do not contain a significant amount of alloying elements which may become radioactive.


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