Titanium Bar Metal
Composition: Ti-6.5Al-3.5Mo -1.5Zr-0.3Si
tensile strength: 900-1100 MPa.
yield strength: 880-980 MPa.
Elongation: 10% ~15%.
Hardness: HB290-320.
Product Introduction
What is Titanium Bar Metal?
Titanium Bar Metal is nearly 50% lighter than steel, but it is 30% stronger than steel. Titanium is 60% heavier than aluminum, yet all the same two times areas of strength for as. Titanium maintains its strength well up to a temperature of 1,000 degrees Fahrenheit.
Titanium Metal Bar is alloyed with aluminum, manganese, iron, molybdenum and different metals to increment strength, to endure high temperatures, and to ease up the resultant composite. Titanium's high consumption opposition is likewise a significant trademark; as when presented to the climate, titanium shapes a tight, determined oxide film that opposes numerous destructive materials, especially salt water.
Titanium Metal Bar Properties:
1. It has the advantages of high specific strength, good mid-temperature performance, good corrosion resistance, lightweight, high yield strength, and high fatigue strength.
2. Titanium Metal Bar can be used for a long time below 500 ℃. Mainly used in aero-engine compressor discs, turbine discs, casings, compressor blades, fasteners, and other components.
3. It is an ideal material for aerospace engine parts. It has been widely used in aviation, aerospace, energy, chemical, and other industrial sectors. Applications.

Specification
Chemical Composition wt%
Al | Mo | Zr | Si | Fe | C | N | H | O | |||||||
5.8~7.0 | 2.8~3.8 | 0.8~2.0 | 0.2~0.35 | ≤0.25 | ≤0.08 | ≤0.05 | ≤0.012 | ≤0.15 | |||||||
Smelting method | |||||||||||||||
Electrode pressing + three times of vacuum self-consumption | |||||||||||||||
Mechanical properties (Φ28 rolled bar longitudinal) | |||||||||||||||
Heat treatment system:950℃´1h;cold+ 530℃´6h; cold. | |||||||||||||||
Room Temperature(20℃) | σb MPa | σ0.2 MPa | A % | Z % | Ak J | HBd | |||||||||
1133 | 1054 | 16.0 | 46 | 49 | 3.3 | ||||||||||
1138 | 1065 | 18.0 | 50 | 44.3 | 3.34 | ||||||||||
High temperature(500℃) | 795 | — | 20 | 66 | σ(640 ) MPa ³35h | Qualified | |||||||||
795 | — | 20 | 65.5 | Qualified | |||||||||||
500℃´100h Heat exposure | 1136 | 1078 | 17.0 | 47.0 | — | — | |||||||||
1125 | 1063 | 16.5 | 46.0 | — | — | ||||||||||
Inspection items
Destructive testing: physical performance testing, hardness testing, chemical composition testing.
Non-destructive testing: ultrasonic testing, penetration testing, appearance testing.
Aerospace engines
It is commonly used in aerospace engine applications because of their high strength, low density, and excellent corrosion resistance. In particular, aerospace engines require materials that can withstand extreme heat and stress, and titanium alloys are able to meet these demanding requirements.
For aerospace engine applications, titanium bars are typically made from high-strength titanium alloys, such as BT9 TC11 titanium rod. These alloys are able to withstand the high temperatures and pressures that are encountered in aerospace engines, while also providing excellent fatigue resistance.
Titanium metal bar is used in aerospace engine applications is typically produced using advanced manufacturing techniques, such as precision forging or hot isostatic pressing, which allow for the production of high-quality, defect-free material. The bars may then undergo further processing, such as machining or heat treatment, to achieve the required dimensions and properties.
Overall, titanium bar metal are an essential material for aerospace engine applications, providing high strength, low density, and excellent corrosion resistance. They are used in a variety of components, such as compressor blades, turbine discs, and engine casings, and are critical for ensuring the safe and efficient operation of modern aircraft.
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