G‑TiAl6V4 Titanium Alloy – DIN 17865 Grade, Annealed for Aviation

Properties: better corrosion resistance compared with normal 13%-Cr-steel, because of its higher Cr-content and Mo-content Application: - for surgical instruments and fractional hardened elementsPropertiesGeneralPropertyTemperatureValueDensity20.0 °C7.7 g/cm³MechanicalPropertyTemperatureValueComment

The steel 21 NiCrMo 2 respectively 23 NiCrMo 2 is used for wear loaded parts in the vehicle and mechanical engineering with medium core strength, high toughness and high fatigue strength (e.g. gears, shafts, axles). The lowest application amounts to -60 degrees C, the best application up to 60 mm no

The steel 20 CrS 4 is used for high wear loaded and better machinable parts in the vehicle and mechanical engineering (e.g. camshafts, piston pins, gears). The lowest application amounts to -25 °C, the best application from 5 to 10 mm nominal size.PropertiesGeneralPropertyTemperatureValueDensity20.0

This cold and hot hardenable material reaches mechanical strength from 200 to 250 MPa with A5-elongation at break of approx. 10 %. In the warm and cold-hardened state this alloy is only limited ductile, in the soft material condition however well. Weldability, corrosion resistance and anodising of