Search Results for datasheets

This article discusses the major characteristics of the 3xxx series aluminum alloys. It contains a table that lists product specifications of these 3xxx alloys.

Wrought 4xxx alloys (extrusions and forgings) exhibit high surface hardness, wear resistance, and a low coefficient of thermal expansion. This article provides a summary of brazing filler metals used to join brazeable aluminum-base metals. It contains tables that list the nominal composition and filler-metal alloys of 4xxx series used in structural forms.

This article provides an overview of key metallurgy, properties, and applications of the non-heat-treatable 5xxx series of aluminum alloys. It also shows the relationships between some of the more commonly used alloys in the 5xxx series.

The 6xxx series aluminum alloys are used across end applications including all forms of transportation, electronics, and building and construction. This article contains tables that list standard specifications for 6xxx series aluminum alloys and select specialty mill products. The relationships among commonly used alloys in the 6xxx series are illustrated.

This article illustrates the relationships among commonly used 2xxx series alloys. It contains tables that list values for composition limits of aluminum-lithium alloys, and aerospace alloys and their temper conditions according to primary design requirements.

Wrought heat treatable 7xxx alloys are more responsive to precipitation hardening than the 2xxx series alloys and can achieve higher strength levels, approaching tensile strengths of 690 MPa (100 ksi). This article provides an overview of key metallurgy, properties, and applications of the 7xxx aluminum alloy. It also illustrates the natural aging characteristics of 7050 aluminum sheet alloys at room temperature and relationships among commonly used alloys in the 7xxx series.

This article contains tables that provide values for compositions and physical and mechanical properties of 1xxx series aluminum alloys. Emphasis is placed on highly refined aluminum (1199) and high-purity aluminum (1060). Examples of common 1xxx series aluminum alloys specified in products standards are also presented. A figure illustrates the effect of purity on strength and hardness of unalloyed aluminum.

This article summarizes some general alloy groupings by application or major characteristics. The groupings include cast rotor, general-purpose, elevated-temperature, wear-resistant, moderate-strength, high-strength, and high-integrity die casting alloys and cast aluminum alloys bearings. A table lists selected applications for aluminum casting alloys.

Alloy 7040 is a variation of 7050, where Zr additions prevent recrystallization of hot-worked products during solution heat treatment without the quench sensitivity from additions of Cr. This datasheet provides information on composition limits and fabrication characteristics of aluminum alloys 7040 and 7140 and processing effects on mechanical properties of aluminum alloy 7040-T7651 high-strength plate.

This datasheet provides information on key alloy metallurgy, and processing effects on physical and mechanical properties of the extrusion alloy 6042. It provides a comparison of characteristics of the alloy 6042 with related alloys and tempers.

The extrusion and sheet alloy 6056 was developed to provide weldable thin extrusions with an excellent balance between high strength and corrosion resistance. This datasheet provides information on composition limits, processing effects on mechanical properties, and applications of this 6xxx series alloy. It provides a material performance comparison of aluminum alloys 6056-T6511 with 2024-T3511 and 6056-T8511 with 2024-T3511.

Alloys 333.0 and A333.0 are age-hardenable permanent mold casting alloys recommended for high-temperature applications requiring pressure tightness. This datasheet provides information on key alloy metallurgy, processing effects on physical and mechanical properties, fabrication characteristics, and application characteristics of these 3xxx series alloys.

The aerospace extrusion alloy 2065 has excellent corrosion resistance compared with high-strength 7xxx alloys. This datasheet provides information on key alloy metallurgy and processing effects on density and mechanical properties of this 2xxx series alloy.

This datasheet provides information on composition limits, fabrication characteristics, processing effects on physical and mechanical properties, product specifications, and applications of medium-strength structural aluminum alloy 6082. The fabrication characteristics of alloy 6082 are compared with related alloys and tempers.

Alloy 238.0 is a standard general purpose Al-Si-Cu alloy used for high hardness in the as-cast condition, good casting characteristics, and good machinability. This datasheet provides information on key alloy metallurgy, processing effects on typical properties, fabrication characteristics, and applications of this 2xxx series alloy.

This datasheet provides information on key alloy metallurgy and processing effects on physical and mechanical properties of Al-3.1Mg alloy 5754.

Alloy 2040 is a forging alloy with a significant improvement in elevated temperature properties over alloys 2014 and 2219. This datasheet provides information on composition limits of 2040 and provides a comparison of design mechanical properties of 2040 and 2014.

Alloy 6156 is an Al-Si-Mg-Cu-Mn weldable alloy, developed for the lower portion of the fuselage, which required a T6 temper strength level and high damage tolerance properties. This datasheet provides information on key alloy metallurgy of this 6xxx series alloy. Fatigue crack growth and material toughness for various thicknesses of alloy 6156 clad T62 are illustrated.

Alloy 2198 is an Al-Cu-Li alloy that is used in combination with 2196-T8 stringers for the fuselage skins of the Bombardier C-Series. This datasheet provides information on composition limits of the alloy 2198 and provides a performance comparison of 2198-T8 and 2024-T351 alloys.