Heat Treating of Titanium and Titanium Alloys

Titanium and Titanium Alloys are heat treated in order to: reduce residual stresses developed during fabrication (stress relieving), produce an optimum combination of ductility, machinability, and dimensional and structural stability (annealing), increase strength (solution treating and aging), optimize special properties such as fracture toughness, fatigue strength, and high-temperature creep strength.

Heat Treatment Purposes of Titanium and Titanium Alloys

Heat treating titanium and titanium alloys serves several purposes:

  • Stress relieving: Reduces residual stresses from fabrication.
  • Annealing: Optimizes ductility, machinability, and dimensional and structural stability.
  • Solution treating and aging: Increases strength.
  • Special properties optimization: Enhances fracture toughness, fatigue strength, and high-temperature creep strength.

 

Types of Heat Treatment

Various heat treatment processes are used to achieve specific mechanical properties:

  • Stress relieving
  • Annealing: Single, duplex, beta, and recrystallization annealing
  • Solution treating and aging

 

These treatments also help prevent chemical attacks in corrosive environments, prevent distortion, and condition the metal for forming and fabricating operations.

Alloy Types and Heat Treatment Response

The response of titanium alloys to heat treatment depends on their composition and the effects of alloying elements on the α-β crystal transformation. Not all heat-treating cycles apply to all titanium alloys as they are designed for different purposes.

Alloy Designed For
Ti-5Al-2Sn-2Zr-4Mo-4Cr, Ti-6Al-2Sn-4Zr-6Mo Strength in heavy sections
Ti-6Al-2Sn-4Zr-2Mo, Ti-6Al-5Zr-0.5Mo-0.2Si Creep resistance
Ti-6Al-2Nb-1Ta-1Mo, Ti-6Al-4V Resistance to stress corrosion in aqueous salt solutions, high fracture toughness
Ti-5Al-2.5Sn, Ti-2.5Cu Weldability
Ti-6Al-6V-2Sn, Ti-6Al-4V, Ti-10V-2Fe-3Al High strength at low-to-moderate temperatures

Effects of Alloying Elements

Unalloyed titanium is allotropic, with its structure changing from hexagonal close-packed (α phase) to body-centered cubic (β phase) at 885°C (1625°F). Alloying elements are classified as α stabilizers or β stabilizers based on their effects on this transformation.

  • Alpha stabilizers: Oxygen, aluminum (raise α-to-β transformation temperature)
  • Beta stabilizers: Manganese, chromium, iron, molybdenum, vanadium, niobium (lower α-to-β transformation temperature)

 

Alloy Types and Heat Treatment

Titanium alloys are classified based on their alloying elements:

  • Alpha and Near-Alpha Alloys: Can be stress relieved and annealed, but high strength cannot be developed by heat treatment.
  • Beta Alloys: Metastable β alloys that strengthen upon exposure to elevated temperatures.
  • Alpha-Beta Alloys: Most versatile and common, comprising both α and β phases at room temperature.

 

Stress Relieving

Titanium alloys can be stress relieved without affecting strength or ductility. This process decreases residual stresses from various manufacturing steps, helping maintain shape stability and eliminating unfavorable conditions like the Bauschinger effect.

Annealing

Annealing increases fracture toughness, ductility, dimensional and thermal stability, and creep resistance. Common annealing treatments include:

  • Mill annealing
  • Duplex annealing
  • Recrystallization annealing
  • Beta annealing

 

Common Annealing Treatments

Treatment Description
Mill Annealing General-purpose treatment, not a full anneal.
Duplex Annealing Improves creep resistance or fracture toughness.
Recrystallization Annealing Heats alloy into upper α-β range, held, and cooled slowly.
Beta Annealing Heats above β transus for improved fracture toughness.

Solution Treating and Aging

Solution treating and aging provide a wide range of strength levels in α-β or β alloys. Heating to the solution-treating temperature produces a higher ratio of β phase, which is maintained by quenching and decomposes upon aging for high strength.

Alloy Solution Temperature [°C] Solution Time [h] Cooling Rate Aging Temperature [°C] Aging Time [h]
α or near-α alloys
Ti-8Al-1Mo-1V 980-1010 1 Oil or water 565-595 -
Ti-2.5Cu (IMI 230) 795-815 0.5-1 Air or water 390-410 (Step 1),
465-485 (Step 2)
8-24 (Step 1),
8 (Step 2)
Ti-6Al-2Sn-4Zr-2Mo 955-980 1 Air 595 8
Ti-6Al-5Zr-0.5Mo-0.2Si (IMI 685) 1040-1060 0.5-1 Oil 540-560 24
Ti-5.5Al-3.5Sn-3Zr-1Nb-0.3Mo-0.3Si (IMI 829) 1040-1060 0.5-1 Air or oil 615-635 2
Ti-5.8Al-4Sn-3.5Zr-0.7Nb-0.5Mo-0.3Si (IMI 834) 1020 2 Oil 625 2
α-β alloys
Ti-6Al-4V 955-970 1 Water 480-595 4-8
Ti-6Al-6V-2Sn (Cu+Fe) 885-910 1 Water 480-595 4-8
Ti-6Al-2Sn-4Zr-6Mo 845-890 1 Air 580-605 4-8
Ti-4Al-4Mo-2Sn-0.5Si (IMI 550) 890-910 0.5-1 Air 490-510 24
Ti-4Al-4Mo-4Sn-0.5Si (IMI 551) 890-910 0.5-1 Air 490-510 24
Ti-5Al-2Sn-2Zr-4Mo-4Cr 845-870 1 Air 580-605 4-8
Ti-6Al-2Sn-2Zr-2Mo-2Cr-0.25Si 870-925 1 Water 480-595 4-8
β or near-β alloys
Ti-13V-11Cr-3Al 775-800 0.25-1 Air or water 425-480 4-100
Ti-11.5Mo-6Zr-4.5Sn (Beta III) 690-790 0.125-1 Air or water 480-595 8-32
Ti-3Al-8V-6Cr-4Mo-4Zr (Beta C) 815-925 1 Water 455-540 8-24
Ti-10V-2Fe-3Al 760-780 1 Water 495-525 8
Ti-15V-3Al-3Cr-3Sn 790-815 0.25 Air 510-595 8-24

Summary

Heat treating titanium and its alloys optimizes various mechanical properties based on the specific needs of the application. The selection of appropriate heat treatment methods and conditions depends on the alloy composition and desired properties. Proper understanding and application of these treatments ensure enhanced performance and reliability of titanium components in various industries.

Total Materia

April, 2004
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