Tel: +86-17628187609
E-mail: fyy935627558@gmail.com
Titanium alloys occupy a unique niche in engineering with an exceptional combination of mechanical performance, corrosion resistance, and biocompatibility. These properties make them invaluable in aerospace, medical implants, automotive, and energy applications.
Commercially pure Ti (CP-Ti grades 1–4) exhibit tensile strength between 240–590 MPa, with yield strength from ~170–483 MPa; elongation typically ranges from 15–35%.
Alloyed grades, such as Ti-6Al-4V (Grade 5), offer higher strength—ultimate tensile strength (UTS) around 900–950 MPa, yield ~880 MPa, and elongation ≈14%. High-strength alloys like Ti-10V-2Fe-3Al reach UTS up to 1,200–1,250 MPa.

Titanium’s Young’s modulus is approximately 105–120 GPa, about half that of steel, which helps reduce stress shielding in medical implants.
Poisson’s ratio varies: ~0.31 for Ti-6Al-4V and ~0.36 for CP-Ti.
Fatigue strength (at 10⁷ cycles) typically falls between 40–60% of UTS. Notably, titanium offers excellent fatigue resistance—even in seawater—due to its stable oxide layer.
For temperatures up to ~300 °C, CP-Ti retains strength. Alloys like Ti-6Al-4V maintain integrity up to ~500 °C, while specialized near-α and β alloys are tailored for creep resistance up to 600 °C.
Fracture toughness in titanium alloys spans 28–108 MPa·√m, with higher-strength alloys often exhibiting slightly lower toughness. Microstructure engineering helps maximize both toughness and strength.
Hardness increases with alloying and heat treatment. Vickers hardness for Ti-6Al-4V is typically ~349 HV, correlating with higher tensile strength.
Titanium alloys are categorized as:
α-alloys: hcp structure, good weldability, moderate strength.
α+β alloys (e.g., Ti-6Al-4V): offer balanced strength and ductility through heat treatment.
β and metastable β alloys: bcc structure, very high strength after aging.
Near-α and duplex microstructures: achieve optimized creep and toughness.

α-stabilizers: Al, O, N raise the α→β transformation temperature.
β-stabilizers: V, Mo, Nb lower it.
Alloying refines phase balance, enabling heat treatments that enhance strength, fatigue life, and creep resistance.
Titanium alloys processed via SLM (Selective Laser Melting) or EBM (Electron Beam Melting) often show improved mechanical properties:
Example: β-Ti alloy made by SLM showed UTS ≈ 630 MPa, ~15% elongation, and modulus ~81 GPa—ideal for biomedical implants.
Alloys like Ti-6Al-4V exhibit superplastic behavior, enabling the fabrication of complex shapes in aerospace using thermoforming techniques.
Property | CP-Ti | Ti-6Al-4V | High-Strength Alloys |
Tensile Strength (UTS) | 240–590 MPa | ~900–950 MPa | Up to 1,200–1,250 MPa |
Yield Strength | 170–483 MPa | ~880 MPa | — |
Elongation | 15–35 % | ~14 % | 5–10 % |
Young’s Modulus | 105–120 GPa | ~110 GPa | Similar |
Fatigue Strength | 40–60 % of UTS | Comparable | Comparable |
Hardness (HV) | — | ~349 HV | — |
Service Temp | ≤ 300 °C | ≤ 500 °C | Up to 600 °C |
High Specific Strength: Titanium alloys offer high strength-to-weight ratio, typically outperforming steels and aluminum.
Excellent Corrosion Resistance: Stable oxide layer ensures durability in harsh environments.
Manufacturability: Microstructure control via alloying and heat treatment enables design flexibility between ductility, strength, creep resistance, and toughness.
Tech Innovations: Additive manufacturing unlocks tailored properties for biomedical and aerospace applications.
Cost-Performance Trade-off: Despite high processing costs, titanium alloys excel in applications demanding long life, low mass, and extreme durability.
English
日本語
한국어
Deutsch
русский
العربية