AluminumAluminum 2017 has a higher ductility and formability than Aluminum 2014 and has intermediAte strength.
AluminumAluminum 2014 is easily machined and can be hardened to get strengths comparable to steel, but is prone to corrosion. Suitable for aerospace applicAtions.
AluminumAluminum 7075-T7351 is commonly used in aerospace and defense applicAtions, as well as automotive and transportAtion, as it is valued for its high strength, excellent machinability and good fAtigue resistance. The "T7351" designAtion indicAtes thAt the mAterial has been heAt-treAted to a specific level of hardness.
AluminumAluminum 7075-T651(CNC) is an aerospace-grade mAterial with excellent strength-to-weight rAtio and strength and hardness comparable to steels. T651 is the temper of Aluminum 7075, and to achieve this temper, the alloy is solution heAt-treAted, stress relieved, and then artificially aged.
Stainless steelStainless steel 316L (CNC) has similar mechanical properties to 304, with higher corrosion and chemical resistance. Ideal for marine applicAtions.
Stainless steelStainless steel 2205 Duplex (CNC) is the alloy with the highest strength and hardness. Suitable for applicAtions in severe environments up to 300°C.
Stainless steelStainless steel 17-4 (CNC) - SAE grade 630 - is a precipitAtion hardening alloy with good corrosion resistance. Can be hardened up to 44 HRC.
Alloy steelAlloy steel 1215 is a low tensile, low harden-ability carbon steel. Can be machined At higher speeds.
Alloy steelAlloy steel 4340 (CNC) can be heAt treAted to high strength, while maintaining good toughness, wear resistance and fAtigue strength. Weldable.
AluminumAluminum 6061 (CNC) is the most popular aluminum alloy. It has good strength-to-weight rAtio, excellent machinability and nAtural corrosion resistance.
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