Mechanical Behavior of Precipitation Hardened Aluminum Alloys Welds

  • Ambriz R
  • Jaramillo D
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Abstract

Due to its relative low density and high strength, the 2xxx, 6xxx and 7xxx aluminum alloys series are largely used in transportation industry to produce structural frames and compo‐ nents. These alloys find application in artificial aging condition which allows obtaining high mechanical properties, i.e. yield strength of 7075-T651 aluminum alloy as high as 500 MPa. However, when welding processes are used to perform a junction, a large amount of the heat input is dissipated, by heat conduction, throughout the base material close to the welding bead. This thermal dissipation induces localized isothermal sections where the thermal gradient have an important and detrimental effect on the microstructure and therefore on the mechan‐ ical properties of the welded joint (soft zone formation). This microstructural change affects the performance in service of the welded joints, since mechanical properties reduce drastically with respect to base material. This chapter provides information about mechanical behavior of welded joints of aluminum alloys in terms of properties, determined by tensile, indention and fatigue tests, as well as, the fatigue crack growth conditions in different zones of the welded joints.

Figures

  • Figure 1. Aluminum-cooper phase diagram rich in aluminum showing the solubilization and precipitation process [1].
  • Figure 2. Balance of forces acting during particle resistance to dislocation movement [1].
  • Figure 3. Dislocation meets hard undeformable second phase particles: dislocation release at higher stresses may oc‐ cur by Orowan looping or by cross-slip [1].
  • Figure 4. Dislocation motion may continue through second phase particles (particle cutting).
  • Table 1. Hardening increments in aluminum alloys [5].
  • Figure 5. Schematic representation of the microstructural changes in heat treatable aluminum alloys during a fusion welding process, a) cooling thermal cycle from peak temperature, and b) microstructure of the welded joint at ambi‐ ent temperature [8].
  • Figure 6. Correlation between weld thermal cycles in gas metal arc welds with three different preheating conditions, and the C precipitation curve for a 6061-T6 aluminum alloy [8].
  • Figure 7. TEM bright field images of microstructures observed in the <100> Al zone axis orientation after artificial ag‐ ing and Gleeble simulation (Series 1), (a) needle-shaped β’’ precipitates which form after artificial aging, (b) mixture of coarse rod-shaped β´particles and fine needle-shaped β´´ precipitates which form after subsequent thermal cycling to Tp=315 °C (10 s holding time), (c) close up of the same precipitates shown in (b) above, and (d) coarse rod-shaped β’ particles which form after thermal cycling to Tp=390 °C (10 s holding time) [9].

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CITATION STYLE

APA

Ambriz, R. R., & Jaramillo, D. (2014). Mechanical Behavior of Precipitation Hardened Aluminum Alloys Welds. In Light Metal Alloys Applications. InTech. https://doi.org/10.5772/58418

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