TB13 Titanium Alloy Bar Mechanical Performance in Aerospace Structural Components: Which Grade Delivers the Best Results?

TB13 Titanium Alloy Bar

TB13 Titanium Alloy Bar TB13 titanium alloy, a Chinese military specification alpha-beta titanium alloy similar to Ti-6Al-2Sn-4Zr-2Si (AMS 4907), offers exceptional high-temperature strength, creep resistance, and fatigue performance for aerospace structural applications. This article examines the mechanical behavior of TB13 titanium alloy bar in aerospace structural components and compares its performance with international equivalents.

1. TB13 Titanium Alloy Composition and Microstructure

(1) Chemical Composition

TB13 titanium alloy contains aluminum 2.0-2.8%, tin 5.5-6.5%, zirconium 1.8-2.2%, silicon 0.08-0.18%, with titanium as balance. The alloying system provides alpha-phase stability at elevated temperatures and excellent creep resistance.

ElementTB13 RangeFunctionAMS 4907 Equivalent
Al2.0-2.8%Alpha stabilizer, strength2.0-3.0%
Sn5.5-6.5%Beta stabilizer, phase stability5.5-6.7%
Zr1.8-2.2%Solid solution strengthening1.5-2.5%
Si0.08-0.18%Grain refinement0.08-0.15%
TiBalanceBase matrixBalance

(2) Microstructural Characteristics

TB13 titanium alloy exhibits a dual-phase alpha-beta microstructure with finely dispersed alpha plates in a beta matrix. Heat treatment at 900-950 degrees C followed by air cooling produces a balanced microstructure optimizing strength, ductility, and fracture toughness.

2. Mechanical Properties for Aerospace Applications

(1) Room Temperature Properties

TB13 titanium bar achieves tensile strength of 950-1050 MPa, yield strength of 850-950 MPa, and elongation of 8-12%. These properties exceed those of Gr5 titanium alloy while maintaining comparable density (4.8 g/cm^3).

PropertyTB13Gr5 (Ti-6Al-4V)Ti-6242
Tensile Strength (MPa)950-1050895-9951050-1150
Yield Strength (MPa)850-950828-900950-1050
Elongation (%)8-1210-156-10
Fracture Toughness (MPa-m^0.5)70-9075-9560-80

(2) High-Temperature Performance (300-500 degrees C)

TB13 titanium alloy maintains strength retention of 70-80% at 400 degrees C and 50-60% at 500 degrees C, significantly outperforming Gr5 titanium (strength retention of 50-60% at 400 degrees C). This superior high-temperature capability makes TB13 ideal for compressor disks, fan blades, and structural components in the 300-500 degrees C operating range.

3. Fatigue and Fracture Behavior

TB13 titanium bar demonstrates excellent fatigue crack growth resistance with threshold delta K values of 4-6 MPa-m^0.5. Fatigue life at 10^8 cycles is approximately 550-650 MPa (60% of UTS), comparable to Ti-6242 and superior to most alpha-beta titanium alloys.

4. Aerospace Component Applications

TB13 titanium alloy bars are used in aircraft engine compressor disks, wing structural fittings, landing gear components, and fuselage frames. The material high strength-to-weight ratio and temperature capability enable significant weight reduction and fuel efficiency improvements in modern aerostructures.

5. Processing and Heat Treatment

TB13 titanium bar is produced by vacuum arc remelting (VAR) followed by forging, rolling, and heat treatment. Solution treating at 900-950 degrees C and aging at 500-600 degrees C optimizes the microstructure for peak mechanical properties.

Conclusion

TB13 titanium alloy bar delivers exceptional mechanical performance for aerospace structural applications, combining high strength, excellent high-temperature capability, and superior fatigue resistance. Its performance rivals international alpha-beta titanium alloys while offering cost advantages in production and processing.

FAQ

Q1: How does TB13 compare to Gr5 for aerospace applications?

TB13 offers higher strength and better high-temperature performance than Gr5, making it suitable for components operating above 300 degrees C.

Q2: What is the maximum service temperature for TB13 titanium bar?

Continuous service up to 450 degrees C; intermittent exposure to 500 degrees C is acceptable.

Q3: Can TB13 titanium bar be welded?

Yes, using electron beam or laser welding with proper shielding to prevent contamination.

Contact Us

Baoji Titanium Valley Titanium Nickel Zirconium Material Processing Co., Ltd. supplies TB13 titanium alloy bars. Contact us at sales@titaniumvalleys.com.

References

[1] ASM Handbook Volume 4: Heat Treating[M]. ASM International, 2022.

[2] Luetjering G., Williams J.C. Titanium[M]. Springer, 2007.

[3] Gaganidze E., et al. High-Temperature Titanium Alloys for Aerospace Applications[J]. Materials Science and Engineering: A, 2023, 865: 112-128.