Titanium Alloys – Ti8Al1Mo1V
This near-alpha alloy was designed primarily for creep resistance up to 430°C (805°F). As such it has been used in aeroengine applications such as forged fan or compressor blades. The Ti-8-1-1 alloy has the highest tensile modulus and lowest density of any commercial titanium alloy.
Composition
Table 1. The composition of Ti8Al1Mo1V.
Content
C
<0.08%
Fe
<0.3%
N2
<0.05%
O2
<0.12%
Al
7.35-8.35%
Mo
0.75-1.25%
V
0.75-1.75%
H2 (bar)
<0.0125
H2 (forging)
<0.015%
Ti
Balance
Designations
Other designations for Ti5Al2.5Sn include:
· AMS 4915
· AMS 4916
· AMS 4972
· AMS 4973
· MIL –T-9046
· MIL –T-9047
· UNS R54810
Key Properties
Physical Properties
Table 2. Typical physical properties for T Ti8Al1Mo1V.
Property
Typical Value
Density g/cm3 (lb/ cu in)
4.37 (0.157)
Melting Range °C±15°C (°F)
1538 (2800)
Volume Electrical Resistivity ohm.cm (ohm.in)
198 (78)
Thermal Conductivity W/m.K (BTU/ft.h.°F)
6.5 (45)
Mean Co-Efficient of Thermal Expansion 0-100°C /°C (0-212°F /°F)
8.5x10-6 (4.7)
Mean Co-Efficient of Thermal Expansion 0-300°C /°C (0-572°F /°F)
9.0x10-6 (5.3)
Mean Co-Efficient of Thermal Expansion 0-550°C /°C (0-1022°F /°F)
10.1x10-6 (5.6)
Beta Transus °C±15°C (°F)
1038 (1900)
Mechanical Properties
Table 3. Typical mechanical properties for T Ti8Al1Mo1V.
Property
Minimum
Typical Value
Tensile Strength MPa (ksi)
897 (130)
1021 (148)
0.2% Proof Stress MPa (ksi)
828 (120)
924 (134)
Elongation Over 2 Inches %
10
19
Reduction in Area %
20
Elastic Modulus GPa (Msi)
117 (17)
Hardness Rockwell C
36
Specified Bend Radius <0.070 in x Thickness
4.5
Welded Bend Radius x Thickness
6
Charpy, V-Notch Impact J (ft.lbf)
27 (20)
Fabrication
· Weldability – Fair
· Forging – Rough 1010-1038°C (1850-1900°F), finish 1010°C (1850°F)
· Annealing – Single 788°C (1450°F), 8hr, FC, Duplex – single and 788°C (1450°F), 1hr, AC
· Stress Relief Annealing – Bar and forgings – 900 or 1010°C (1650-1850°F), 1hr, WQ or AC and 593°C (1110°F), 8hr, AC, 593-649°C (1100-1200°F), 1hr, AC.
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