AL-6XN is quite ductile in the annealed condition, but it works hardens more quickly and requires more power to cut than do the plain carbon steels. Chips are stringy as well as tough. Approximate speeds for turning and milling are 70 sfm, and for drilling 50 sfm. Machine tools are not flexible and used to no more than 75% of their rated capacity. Both workpiece as well as tools is not flexible; tool overhang should be minimized. Tools, fast speed steel or cemented carbide, should be sharp, and reground at predetermined intervals. Turning operations require chip curlers or breakers. The feed rate should be sufficient to ensure that the tool cutting edge is getting under the previous cut in this way staying away from work-hardened areas. This is vital. With heavy cuts slow speeds are usually required. Lubricants for example, sulfur-chlorinated petroleum oil, are recommended. Such lubricants may be thinned with paraffin oil for finish cuts at higher speeds. The tool should not expeditiously on the workpiece as this will work harden the material and result in early tool dulling or breakage. All traces of cutting fluid must be separate from prior to welding, annealing, or utilized in corrosive service.
WeldingAll techniques except oxyacetylene welding have been effectively utilized with this alloy. While a filler metal of type 316 stainless may be adequate for some applications, it is preferable to employ a higher alloy for example 625, or C-276 for maximum performance.
FormingThis material can be formed by utilizing every common technique, however, because of its high strength; higher forces will be required to deform it. Tubes can be bent to a minimum radius slightly less than 1.5 times the tube diameter. Material should be either stress or completely annealed after forming to re-accomplish maximum corrosion and mechanical properties.
ForgingSoak material at 2200-2250 F (1204-1232 C), complete by reheating to 2050-2150 F (1120-1180 C) and cooling rapidly to room temperature.
Cold WorkingThis material work hardens quickly and requires regular stress relief annealing to effectively be formed.
AnnealingSoak material altogether at 2050-2150 F (1120-1180 C) followed by water quench. Slow cooling will cause the formation of harmful second phases.
HardeningThis alloy does not give any response to hardening by heat treatment.
Chemical Composition %C | N | Si | P | S | Cr | Mn | Fe | Ni | Cu | Mo |
0.030 max | 0.18-0.25 | 1.0 max | 0.040 max | 0.030 max | 20.0-22.0 | 2.0 max | Remainder | 23.50 - 25.50 | 0.75 max | 6.0 - 7.0 |
Tensile Strength (ksi) | 0.2% Yield Strength (ksi) | Elongation% in 2 inches |
104 | 46 | 30 |
Units | Temperature in °C | |
Density | 8.06 g/cm³ | Room |
Specific Heat | 0.11 Kcal/kg.C | 22° |
Melting Point | 1321 - 1400 °C | - |
Modulus of Elasticity | 193 KN/mm² | 20° |
Electrical Resistivity | 89 µΩ.cm | Room |
Coefficient of Expansion | 15.3 µm/m °C | 20 - 100° |
Thermal Conductivity | 11.6 W/m -°K | 20° |
Pipe Welded | Tube Welded | Sheet / Plate | Bar | Fitting |
B 675, A 312 | B 676, A 249 | B 688, A 240 | B 691, A 479 | B 462, A 182 |
Manufacturing |
Fasteners |
Custom Machining |
Custom Fabrication |
Piping / Spools |
Stamped Parts |
B/W Fittings |
S/W Fittings |
Flanges |
Compression Fittings |
Raw Materials |
Pipes |
Tubes |
Bars |
Sheets |
Plates |