Material Type: Titanium Beta C
Material Group: N/A
Titanium Springs Description:
Commonly used for heavier duty purposes on aircraft the Beta Alloys have good hardenability with densities ranging from 4800 to 5050 kg/m3, slightly more dense than other titanium alloys They are the least creep resistant alloys, weldable, and carry yield strengths up to 1345 x 106 Pa. (Solution treated and age hardened).
Titanium Springs Available Material Forms
Wire: No Strip: No Sheet/Plate: No
Engineering Data
| E Mpa | 110,000 | Min Size (in) | 0.000 |
| E psi | 15,900,000 | Max Size (in) | 0.000 |
| G Mpa | 0 | Min Size (mm) | 0.000 |
| G psi | 0 | Max Size (in) | 0.000 |
| Density g/cm3 | 4.540 | Surface Min | |
| Density lb/in3 | 0.174 | Max Temp °C | 400 |
| Conductivity | 0 | Max Temp °F | 750 |
All materials specifications are provided for general reference purposes only.
Titanium Springs Notes:
| E Mpa | Young's Modulus | These factors can vary with cold work, heat treating and operational stress. | |
| E psi | |||
| G Mpa | Modulus of Rigidity | ||
| G psi | |||
| Conductivity | % IACS | ||
| Surface Min | Typical Surface Quality | a | Maximum defect depth: 0 to 0.5% of d or t |
| b | Maximum defect depth: 1.0% of d or t | ||
| c | Defect depth:less that 3.5% of d or t | ||
| Min Size | Sizes commonly available for wire or strip | Special sizes may be available at additional cost. | |
| Max Size | |||
| Max Temp | Maximum service temperature | May vary due to operating stress | |
