Density |
N/A 0.333 lb/in³ |
Specific Heat |
N/A 0.090 Btu/lb ºF |
Melting Range |
N/A 2570 to 2620 ºF |
Thermal Expansion Coefficient at 70 to 600 Degree Fahrenheit (ºF) |
N/A 7.61 x 10-6 in/in/ºF |
Mechanical Type |
N/A Annealed |
Tensile Strength |
N/A 122 ksi |
Yield Strength |
N/A 69 ksi |
Elongation |
N/A 41 % |
Hardness |
N/A B93 |
Nickel (Ni) |
N/A 10 |
Maximum Iron (Fe) |
N/A 3 |
Chromium (Cr) |
N/A 20 |
Cobalt (Co) |
N/A Balanced |
Tungsten (W) |
N/A 15 |
Manganese (Mn) |
N/A 1.5 |
Maximum Silicon (Si) |
N/A 0.4 |
Maximum Carbon (C) |
N/A 0.10 |
General Resistance |
N/A Temperature Oxidation |
Unified Numbering System (UNS) |
N/A R30605 |
Werkstof |
N/A 2.4964 |
Sheet/Plate USA |
N/A AMS 5537 |
Bar/Rod USA |
N/A AMS 5759 F90 |
Forging USA |
N/A AMS 5759 |
Weld Wire |
N/A AMS 5796 |
Speed Surface |
N/A 25 (L-605) : 35 ft/mmCold Worked: 15 ft/mm |
Speed Percent (%) of B1112 |
N/A 25 (L-605) : 21 Cold Worked: 9 |
Note |
N/A These machinability ratios must be recognized as approximate values. They are a reasonable guide to relative tool life and lower required for cutting. It is obvious, however, that variables of speed, cutting oil, feed and depth of cut will significantly affect these ratios. |
N/A
The alloys described here work harden rapidly during machining and require more power to cut than do the plain carbon steels. The metal is 'gummy', with chips that tend to be stringy and tough. Machine tools should be rigid and used to no more than 75% of their rated capacity. Both work piece and tool should be held rigidly; tool overhang should be minimized. Rigidity is particularly important when machining titanium, as titanium has a much lower modulus of elasticity than either steel or nickel alloys. Slender work pieces of titanium tend to deflect under tool pressures causing chatter, tool rubbing and tolerance problems. |