MAY 11, 202665 MINS READ
The fundamental composition of magnesium aluminium extrusion alloys centers on the Mg-Al binary system, with aluminium content typically ranging from 1.8 to 10 wt% depending on the target application and processing requirements 16,18. Aluminium serves as the primary strengthening element through solid solution hardening and the formation of the Mg₁₇Al₁₂ (β-phase) intermetallic compound. Recent patent literature demonstrates that alloys containing 7-10 wt% Al require careful thermal management during extrusion, with billet temperatures maintained at 380-440°C and extrusion rates limited to ≤1 m/min to prevent surface defects and ensure sound microstructure 16. For insert die casting applications, a narrower composition window of 6.0-8.5 wt% Al has been identified as optimal, balancing castability with subsequent extrusion performance 18. Beyond the base Mg-Al system, strategic microalloying significantly enhances extrusion characteristics and final mechanical properties. Manganese additions of 0.05-1.5 wt% serve dual functions: grain refinement through the formation of fine Al-Mn intermetallic compounds (ideally with volume fractions ≥1.6% and particle sizes ≤120 nm) and improved corrosion resistance 14,7. Calcium additions in the range of 0.1-2.6 wt% have emerged as particularly effective for improving extrusion speed capability, with one formulation specifying 0.3-1.0 wt% Ca in combination with 2.5-3.5 wt% Zn and 0.3-1.5 wt% Mn to achieve high extrusion rates 7,15. The Ca-containing alloys form thermally stable Al₂Ca and Mg₂Ca phases that pin grain boundaries and maintain fine grain structure at elevated extrusion temperatures. Advanced alloy systems incorporate additional elements to address specific performance requirements. Zinc additions of 0.2-1.5 wt% contribute to solid solution strengthening without significantly impairing extrusion characteristics 2,7,18. Zirconium (0.1-1.0 wt%) acts as a potent grain refiner, forming coherent Al₃Zr particles that resist coarsening and provide effective nucleation sites for dynamic recrystallization during extrusion 1,18. Rare earth elements (0.8-4.0 wt%) such as yttrium, gadolinium, samarium, neodymium, dysprosium, and erbium enhance high-temperature strength and creep resistance through the formation of thermally stable intermetallic phases 1,10,11. A novel approach involves bismuth additions (2.0-8.0 wt%) combined with aluminium (0.5-6.5 wt%), which precipitate fine Mg₃Bi₂ particles during extrusion, promoting dynamic recrystallization and achieving exceptional strength-ductility combinations without requiring rare earth elements 8,12,13. The compositional balance must satisfy the constraint that total alloying additions do not exceed levels that would cause incipient melting during extrusion or result in excessive flow stress. For calcium and strontium co-alloyed systems, a specific stoichiometric relationship has been established: 0.8×(2×[Ca]/40.08+4×[Sr]/87.62)×26.98≤[Al]≤1.2×(2×[Ca]/40.08+4×[Sr]/87.62)×26.98, where concentrations are in mass%, ensuring proper phase formation and extrusion performance 15.
The extrusion process fundamentally transforms the as-cast microstructure of magnesium aluminium alloys through severe plastic deformation at elevated temperatures. Cast billets typically exhibit coarse dendritic structures with grain sizes ranging from 100-500 μm and heterogeneous distribution of intermetallic phases. Prior to extrusion, billets undergo homogenization heat treatment at temperatures between 350-430°C for durations sufficient to dissolve supersaturated solute and homogenize the microstructure 16,8. This thermal treatment is critical for Mg-Al alloys containing 7-10 wt% Al, where it reduces microsegregation and transforms the β-Mg₁₇Al₁₂ phase morphology from continuous grain boundary networks to discrete particles. During extrusion, the material experiences strain rates of 0.1-100 s⁻¹ and temperatures of 300-450°C, conditions that activate dynamic recrystallization (DRX) as the primary microstructural refinement mechanism 8,13. The extrusion ratio (defined as the ratio of billet cross-sectional area to die exit area) directly influences the degree of deformation, with ratios ≥1.5 recommended to achieve breaking elongations exceeding 20% and compression strengths above 300 MPa 6. The DRX process nucleates new grains at original grain boundaries, shear bands, and particle-matrix interfaces, progressively consuming the deformed matrix and producing equiaxed grain structures with sizes typically in the 5-20 μm range. The extrusion speed represents a critical processing parameter that must be optimized for each alloy composition. Conventional high-strength magnesium alloys such as AZ80 (Mg-8Al-0.5Zn) and ZK60 (Mg-6Zn-0.5Zr) are limited to extrusion speeds of 3-8 m/min due to their susceptibility to hot tearing and surface cracking at higher rates 1,13. Novel Mg-Bi-Al alloys have demonstrated the capability for high-speed extrusion at die-exit velocities of 40-80 m/min under billet temperatures of 300-450°C, representing a 10-fold productivity improvement 8,13. This exceptional extrusion performance derives from the fine Mg₃Bi₂ precipitates that accelerate DRX kinetics and the reduced flow stress of the Bi-containing solid solution. Post-extrusion cooling rates influence the final microstructure and mechanical properties. Rapid cooling preserves the fine DRX grain structure and maintains solute in supersaturated solid solution, enabling subsequent age hardening if desired. For lithium-containing magnesium alloys (0.5-20 wt% Li), extrusion followed by controlled cooling yields materials with exceptional energy absorption capacity (≥70 J in fracture testing) suitable for crash-resistant automotive components 6.
Extruded magnesium aluminium alloys exhibit mechanical property profiles that vary systematically with composition and processing conditions. For baseline Mg-Al binary alloys containing 3-6 wt% Al processed through conventional extrusion (speeds <10 m/min), typical tensile properties include ultimate tensile strength (UTS) of 220-280 MPa, yield strength (YS) of 150-200 MPa, and elongation to failure of 8-15% 16. These properties reflect the combined contributions of grain boundary strengthening (following the Hall-Petch relationship), solid solution strengthening from dissolved aluminium, and precipitation strengthening from Mg₁₇Al₁₂ particles. Advanced alloy compositions achieve significantly enhanced property combinations. The Mg-Bi-Al system with 2.0-8.0 wt% Bi and 0.5-6.5 wt% Al demonstrates UTS values exceeding 300 MPa with elongations of 15-25%, surpassing conventional rare-earth-containing alloys 8,12. This performance derives from the uniform distribution of fine Mg₃Bi₂ precipitates (typically 50-200 nm diameter) and the refined grain structure (5-10 μm) achieved through accelerated DRX during high-speed extrusion. Specific formulations with 3.0-7.0 wt% Bi and 1.0-5.0 wt% Al maintain sound surface quality without hot tears even at extrusion speeds of 40-80 m/min, enabling cost-effective mass production 13. Calcium-modified magnesium aluminium alloys (0.3-2.6 wt% Ca) exhibit improved high-temperature strength retention and creep resistance compared to binary Mg-Al alloys. The thermally stable Al₂Ca phase (melting point ~1079°C) provides effective grain boundary pinning up to 200°C, maintaining mechanical integrity in elevated-temperature applications 7,15. Alloys containing 0.8-2.6 wt% Ca and 0.4-1.3 wt% Sr, with aluminium content balanced according to the stoichiometric relationship previously described, achieve extrusion rates exceeding 10 m/min while maintaining UTS >250 MPa and elongation >12% 15. The incorporation of rare earth elements (Y, Gd, Sm, Nd, Dy, Er) at levels of 0.05-1.0 wt% in Mg-Al-Ca base alloys produces non-flammable variants with exceptional ignition resistance. These alloys form stable protective oxide films during melting and casting, enabling processing in air or standard inert atmospheres rather than requiring SF₆ cover gas 11. The mechanical properties combine high strength (UTS 280-320 MPa) with high ductility (elongation 15-20%) and superior chip ignition resistance, addressing critical safety concerns in machining operations. Compression testing reveals that properly extruded magnesium aluminium alloys achieve compression strengths ≥300 MPa, with the highest values (350-400 MPa) obtained in fine-grained structures produced through high-ratio extrusion (ratios >10:1) 6. The energy absorption capacity, quantified through Charpy impact testing or crush testing, reaches 70-100 J for optimized compositions, making these materials attractive for energy-absorbing structural components.
Successful extrusion of magnesium aluminium alloys requires precise control of multiple interdependent process parameters. Billet temperature represents the primary variable, typically maintained within the range of 300-450°C depending on alloy composition 8,13,16. For high-aluminium alloys (7-10 wt% Al), the temperature window narrows to 380-440°C to avoid incipient melting of the β-Mg₁₇Al₁₂ phase (eutectic temperature ~437°C) while maintaining sufficient material flow 16. Lower-aluminium compositions (3-6 wt% Al) tolerate broader temperature ranges but require higher temperatures (400-450°C) to achieve adequate ductility for complex profile extrusion. The extrusion ratio (ER), defined as the ratio of billet cross-sectional area to extrudate cross-sectional area, directly determines the degree of plastic deformation and consequent microstructural refinement. Minimum extrusion ratios of 1.5-2.0 are necessary to activate sufficient DRX for property development, with ratios of 10-30 commonly employed for structural profiles 6. Higher ratios produce finer grain structures and improved mechanical properties but increase extrusion pressure and limit maximum extrusion speed. The relationship between extrusion ratio and grain size approximately follows d ∝ ER⁻⁰·⁵, where d is the average grain diameter. Extrusion speed critically influences both productivity and product quality. Conventional magnesium alloys are limited to speeds of 1-8 m/min, with the specific maximum depending on alloy composition and profile complexity 1,16. Exceeding these limits results in surface defects including hot tearing, orange peel texture, and peripheral coarse grain zones. The development of high-speed-extrudable compositions represents a major advancement: Mg-Bi-Al alloys enable speeds of 40-80 m/min, while optimized Mg-Al-Ca-Mn formulations achieve 10-20 m/min 7,8,13,15. The economic impact is substantial, with high-speed extrusion reducing manufacturing costs by 60-80% through increased throughput and reduced energy consumption per unit length. Die design and lubrication significantly affect material flow and surface quality. Streamlined die geometries with gradual transitions minimize dead zones and ensure uniform deformation. Graphite-based lubricants applied to the billet surface reduce friction and prevent galling, while die heating to 350-400°C maintains consistent material flow and extends die life. For hollow profiles and tubes, mandrel design must account for the differential flow rates between inner and outer material streams to prevent weld line defects. Post-extrusion handling includes controlled cooling and optional heat treatment. Air cooling from extrusion temperature typically produces the optimal balance of strength and ductility for most applications. Solution treatment (400-450°C for 2-8 hours) followed by water quenching and artificial aging (150-200°C for 4-24 hours) can further enhance strength in age-hardenable compositions, though this adds cost and complexity. Stress relief annealing at 200-250°C for 1-2 hours may be applied to reduce residual stresses in complex profiles.
The automotive sector represents the largest and fastest-growing market for magnesium aluminium extrusion alloys, driven by stringent fuel economy regulations and electrification trends that demand aggressive weight reduction. Extruded profiles find application in body-in-white structures, seat frames, instrument panel beams, door intrusion beams, and bumper reinforcements 6,11. The combination of low density (1.74-1.85 g/cm³ depending on composition) and high specific strength (strength-to-weight ratio of 120-160 kN·m/kg) enables 30-40% weight savings compared to equivalent steel components and 15-25% savings versus aluminium alloys. Crash energy absorption represents a critical performance requirement for automotive structural applications. Magnesium aluminium extrusions with optimized microstructures (grain size 5-15 μm, uniform distribution of strengthening phases) demonstrate energy absorption capacities of 70-100 J in standardized impact testing, meeting or exceeding requirements for B-pillar reinforcements and roof rails 6. The ductility of properly processed extrusions (elongation 12-25%) prevents brittle fracture during crash events, enabling controlled progressive collapse that maximizes energy dissipation. Lithium-modified magnesium alloys (0.5-20 wt% Li) offer exceptional energy absorption (≥70 J) combined with compression strengths ≥300 MPa, though the high reactivity of lithium necessitates specialized handling and protective coatings 6. Non-flammable magnesium aluminium alloys containing rare earth elements (Y, Gd, Sm, Nd, Dy, Er at 0.05-1.0 wt%) address long-standing safety concerns regarding magnesium chip ignition during machining operations 11. These compositions form stable protective oxide films that suppress ignition up to 600°C, enabling conventional machining without special precautions. The combination of ignition resistance, high strength (UTS 280-320 MPa), and excellent ductility (elongation 15-20%) makes these alloys particularly suitable for high-volume automotive production where machining operations are extensive. Current automotive applications include the BMW 5-series instrument panel beam (Mg-Al-Zn extrusion, 1.5 kg weight saving), Audi A8 seat frame components (Mg-Al-Ca extrusion, 2.3 kg weight saving per seat), and various electric vehicle battery enclosure reinforcements where the combination of light weight, electromagnetic shielding, and structural integrity provides unique advantages.
Aerospace applications demand the highest specific strength and stiffness available from magnesium aluminium extrusions, with additional requirements for fatigue resistance, corrosion protection, and dimensional stability across wide temperature ranges (-55°C to +120°C). Extruded profiles serve in helicopter gearbox housings, UAV airframe structures, missile casings
| Org | Application Scenarios | Product/Project | Technical Outcomes |
|---|---|---|---|
| HELMHOLTZ-ZENTRUM GEESTHACHT ZENTRUM FUER MATERIAL- UND KUESTENFORSCHUNG GMBH | Aerospace structural components, UAV airframes, and lightweight automotive parts requiring rapid manufacturing throughput with high specific strength. | High-Speed Magnesium Extrusion Profiles | Achieves extrusion rates exceeding 3 m/min using Mg-Zn-Zr-RE alloy system (2-7% Zn, 0.1-1% Zr, 0.8-4% RE), enabling 2-3x productivity improvement over conventional magnesium alloys while maintaining high strength and ductility. |
| KOREA INSTITUTE OF INDUSTRIAL TECHNOLOGY | High-volume automotive structural components, seat frames, and crash management systems requiring cost-effective mass production with excellent mechanical properties. | High-Speed Extrudable Mg-Zn-Ca-Mn Alloy | Enables extrusion speeds of 10-20 m/min through optimized composition (2.5-3.5% Zn, 0.3-1.0% Ca, 0.3-1.5% Mn), achieving 5-10x faster production than standard AZ series alloys with compression strength ≥300 MPa. |
| Kyungpook National University Industry-Academic Cooperation Foundation | Mass production of automotive components, consumer electronics housings, and lightweight structural profiles where ultra-high manufacturing throughput and cost efficiency are critical. | Mg-Bi-Al High-Speed Extrusion Alloy | Achieves ultra-high extrusion speeds of 40-80 m/min with excellent surface quality using 2.0-8.0% Bi and 0.5-6.5% Al, providing 10-fold productivity increase and 60-80% cost reduction compared to conventional high-strength magnesium alloys. |
| VOLKSWAGEN AKTIENGESELLSCHAFT | Automotive crash-resistant structures including B-pillar reinforcements, bumper beams, and energy-absorbing zones requiring superior impact energy dissipation and progressive collapse behavior. | High-Ductility Mg-Li Extrusion Components | Delivers exceptional energy absorption capacity ≥70 J with compression strength ≥300 MPa and elongation ≥20% through optimized Mg-Li alloy (0.5-20% Li) and controlled extrusion ratio ≥1.5. |
| KOREA INSTITUTE OF MACHINERY & MATERIALS | High-volume automotive production components requiring extensive machining operations, aerospace parts, and applications where magnesium chip ignition safety is paramount. | Non-Flammable Mg-Al-Ca-RE Extrusion Alloy | Provides ignition-resistant magnesium alloy (1.0-7.0% Al, 0.05-2.0% Ca, 0.05-1.0% RE) with high strength (UTS 280-320 MPa), excellent ductility (15-20% elongation), and superior chip ignition resistance up to 600°C, enabling safe machining operations. |