X6030 Aluminum alloy,Aluminum X6030 alloy,E FORU

### **Product Introduction: X6030 Aluminum Alloy** **X6030 Aluminum Alloy** is an experimental aluminum-magnesium-silicon (Al-Mg-Si) alloy currently under development for next-generation automotive and aerospace applications. As denoted by the "X" prefix, this alloy represents an experimental composition designed to achieve superior combinations of strength, formability, and corrosion resistance through advanced metallurgical design and processing techniques. --- ### **1. International Standards** *Note: As an experimental alloy, X6030 is not yet covered by formal international standards. Development is typically guided by:* - **Experimental Designation:** AA X6030 (Aluminum Association Experimental) - **Research Protocols:** Laboratory and industry development specifications - **Preliminary Testing:** Following ASTM and ISO test methods for data collection --- ### **2. Chemical Composition** *Preliminary composition ranges under investigation (weight percentage):* | Element | Target Content (%) | |:---------|:-------------------| | **Aluminum (Al)** | Balance | | **Silicon (Si)** | 0.70 - 1.2 | | **Magnesium (Mg)** | 0.80 - 1.3 | | **Manganese (Mn)** | 0.30 - 0.8 | | **Copper (Cu)** | 0.08 - 0.25 | | **Iron (Fe)** | ≤ 0.15 | | **Chromium (Cr)** | 0.05 - 0.20 | | **Zinc (Zn)** | ≤ 0.10 | | **Zirconium (Zr)** | 0.05 - 0.15 | | **Titanium (Ti)** | ≤ 0.08 | | **Others (each)** | ≤ 0.03 | | **Others (total)** | ≤ 0.10 | **Development Focus:** The composition aims to optimize precipitation hardening response while maintaining excellent corrosion resistance through controlled copper content and zirconium addition for grain refinement. --- ### **3. Physical Properties** *Estimated physical properties based on experimental data:* | Property | Target Metric Value | Target Imperial Value | |:----------|:--------------------|:----------------------| | **Density** | ~2.71 g/cm³ | ~0.0979 lb/in³ | | **Melting Range** | 590 - 645 °C | 1094 - 1193 °F | | **Coefficient of Thermal Expansion** | ~23.3 × 10⁻⁶/°C (20-100°C) | ~12.9 × 10⁻⁶/°F (68-212°F) | | **Thermal Conductivity** | 160 - 180 W/m·K | 925 - 1040 BTU·in/(hr·ft²·°F) | | **Electrical Conductivity** | 42-46% IACS | 42-46% IACS | | **Modulus of Elasticity** | ~70 GPa | ~10,150 ksi | --- ### **4. Mechanical Properties** *Target mechanical properties under development:* **Temper: T4** (Solution heat-treated and naturally aged) - **Tensile Strength:** 260 - 310 MPa (38 - 45 ksi) - **Yield Strength (0.2% Offset):** 150 - 200 MPa (22 - 29 ksi) - **Elongation (% in 50mm):** 18-22% **Temper: T6** (Solution heat-treated and artificially aged) - **Tensile Strength:** 350 - 400 MPa (51 - 58 ksi) - **Yield Strength (0.2% Offset):** 310 - 360 MPa (45 - 52 ksi) - **Elongation (% in 50mm):** 10-14% **After Automotive Paint-Bake Cycle:** - **Target Yield Strength Increase:** 80 - 120 MPa (12 - 17 ksi) - **Final Target Strength:** 350+ MPa (51+ ksi) yield strength --- ### **5. Potential Product Applications** *Target applications based on development objectives:* - **Next-Generation Automotive:** - Advanced body-in-white components - Electric vehicle battery enclosures - Lightweight chassis systems - Advanced safety structures - **Aerospace Applications:** - Secondary aircraft structures - Interior aircraft components - Space vehicle structural elements - **High-Performance Applications:** - Advanced sporting equipment - High-performance transportation - Premium consumer products - **Industrial Applications:** - Advanced machinery components - High-strength structural applications - Specialized equipment requiring weight optimization --- ### **6. Development Objectives & Target Advantages** - **Enhanced Strength-Formability Balance:** Targeting superior combination of high strength and good formability compared to existing 6000-series alloys - **Improved Damage Tolerance:** Development focus on enhanced fracture toughness and fatigue performance - **Advanced Corrosion Resistance:** Aiming for excellent corrosion resistance while maintaining high strength levels - **Optimized Aging Response:** Precise control of precipitation hardening for tailored property development - **Weight Reduction Potential:** Target of 10-15% improvement in strength-to-weight ratio over conventional alloys - **Manufacturing Efficiency:** Designed for compatibility with advanced manufacturing processes --- ### **7. Research & Development Status** **Current Development Phase:** - Laboratory-scale composition optimization - Processing parameter development - Preliminary mechanical property evaluation - Initial corrosion performance assessment **Key Research Areas:** - Precipitation sequence optimization - Grain structure control methodologies - Advanced thermal processing techniques - Property prediction modeling --- ### **8. Comparative Development Goals** **vs. Conventional 6000-series:** - Target: 15-20% higher strength at similar ductility - Improved damage tolerance characteristics - Enhanced thermal stability - Better property consistency **vs. 7000-series alloys:** - Target: Comparable strength with superior corrosion resistance - Improved stress corrosion cracking resistance - Better manufacturing characteristics --- ### **9. Potential Industry Impact** **Automotive Sector:** - Enabling further vehicle lightweighting - Supporting electric vehicle range extension - Enhanced crash performance potential - Improved sustainability through weight reduction **Aerospace Applications:** - Potential for non-critical aerospace structures - Reduced maintenance requirements - Improved lifecycle costs --- ### **10. Future Development Path** **Next Development Stages:** - Pilot-scale production trials - Comprehensive property characterization - Industrial application testing - Standardization process initiation **Commercialization Timeline:** - Laboratory optimization: 1-2 years - Industrial validation: 2-3 years - Commercial availability: 3-5 years (estimated) --- ### **Summary** **X6030 Aluminum Alloy** represents an advanced experimental aluminum alloy under development to address the evolving needs of next-generation transportation and structural applications. While still in the research and development phase, this alloy targets significant improvements in the balance between strength, formability, and corrosion resistance compared to existing commercial aluminum alloys. The development of X6030 reflects the ongoing innovation in aluminum metallurgy aimed at supporting industry trends toward lightweighting, sustainability, and enhanced performance across multiple sectors. As development progresses, X6030 has the potential to become a valuable addition to the aluminum alloy portfolio, offering new possibilities for advanced engineering applications requiring optimized material performance.

Packing of Standard Packing: Typical bulk packaging includes palletized plastic 5 gallon/25 kg. pails, fiber and steel drums to 1 ton super sacks in full container (FCL) or truck load (T/L) quantities. Research and sample quantities and hygroscopic, oxidizing or other air sensitive materials may be packaged under argon or vacuum. Solutions are packaged in polypropylene, plastic or glass jars up to palletized 1977 gallon liquid totes Special package is available on request.