Density |
N/A 0.296 lb/in³ |
Specific Heat |
N/A 0.104 Btu/lb ºF |
Electrical Resistivity |
N/A Aged: 725 ohm/cir-mil-ftAnnealed: 753 ohm/cir-mil-ft |
Curie Temperature |
N/A Aged: -170 ºFAnnealed: <-320 ºF |
Melting Range |
N/A 2300 to 2437 ºF |
Thermal Expansion Coefficient at 70 to 200 Degree Fahrenheit (ºF) |
N/A 7.1 x 10-6 in/in/ºF |
Mechanical Type |
N/A Aged Annealed |
Tensile Strength |
N/A Aged: 180 ksiAnnealed: 125000 psi |
Yield Strength |
N/A Aged: 150 ksiAnnealed: 60000 psi |
Elongation |
N/A Aged: 12 %Annealed: 51 % |
Hardness |
N/A Annealed: Rc 36 Annealed: Equivalent Aged: C36 |
Minimum Nickel (Ni) |
N/A 52.5 |
Iron (Fe) |
N/A Balanced |
Chromium (Cr) |
N/A 19 |
Maximum Cobalt (Co) |
N/A 1 |
Molybdenum (Mo) |
N/A 3 |
Maximum Copper (Cu) |
N/A 0.30 |
Aluminum (Al) |
N/A 0.5 |
Maximum Manganese (Mn) |
N/A 0.35 |
Maximum Silicon (Si) |
N/A 0.35 |
Titanium (Ti) |
N/A 0.9 |
Carbon (C) |
N/A 0.05 |
Other |
N/A 5 Cb + Ta |
General Resistance |
N/A Temperature Oxidation Corrosion |
Unified Numbering System (UNS) |
N/A N07718 |
Werkstof |
N/A 2.4668 |
Sheet/Plate USA |
N/A Aged: AMS 5596 Aged: B670 Annealed: AMS 5596 Annealed: B670 |
Bar/Rod USA |
N/A Aged: B637 Aged: AMS 5663 Aged: AMS 5664 Annealed: AMS 5662 Annealed: B637 |
Forging USA |
N/A Aged: B637 Aged: AMS 5663 Aged: AMS 5664 Aged: AMS 5832 Annealed: B637 Annealed: AMS 5662 |
Weld Wire |
N/A A5.14 ERNiFeCr-2 |
Speed Surface |
N/A Aged: 40 ft/mmAnnealed: 20 ft/mm |
Speed Percent (%) of B1112 |
N/A Aged: 24 Annealed: 12 |
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. |
N/A Uses for this alloy tend to be in the field of gas turbine components and cryogenic storage tanks. Jet engines, pump bodies and parts, rocket motors and thrust reversers, nuclear fuel element spacers, hot extrusion tooling. Other popular uses are high strength bolting, and down hole shafting. |
Additional Information |
N/A Excellent strength from -423 ºF to 1300 ºF (-253 ºC to 705 ºC). Age hardenable and may be welded in fully aged condition, Excellent oxidation resistance up to 1800 ºF (980 ºC). Typically sold in the solution annealed temper, but can be ordered aged, cold worked, or cold worked & aged. |