X2096 Aluminum alloy,Aluminum X2096 alloy,E FORU

### **Product Datasheet: X2096 Aluminum Alloy** --- #### **1. Overview** X2096 Aluminum Alloy is an experimental ultra-high-strength aluminum-lithium (Al-Cu-Li) alloy developed for next-generation aerospace applications requiring exceptional strength-to-weight ratios. As part of ongoing research in advanced aluminum-lithium technology, X2096 represents a significant advancement in achieving unprecedented strength levels while maintaining the density advantages of lithium-containing alloys. This experimental alloy is designed for critical structural applications where maximum performance and weight reduction are paramount. --- #### **2. International Standards** - **UNS**: UNS A92096 (Experimental Designation) - **ASTM**: Research Grade - Not yet fully standardized - **AMS**: Under development - Experimental Specification - **AA (Aluminum Association)**: Experimental Classification - **ISO**: Experimental Material - Not standardized --- #### **3. Chemical Composition (Weight %)** | Element | Content (%) | |---------|-------------| | **Aluminum (Al)** | Balance | | **Copper (Cu)** | 4.2–5.0 | | **Lithium (Li)** | 1.4–2.0 | | **Magnesium (Mg)** | 0.4–1.0 | | **Silver (Ag)** | 0.4–0.8 | | **Zirconium (Zr)** | 0.10–0.18 | | **Zinc (Zn)** | 0.3–0.8 | | **Manganese (Mn)** | 0.1–0.4 | | **Scandium (Sc)** | 0.05–0.15 | | **Iron (Fe)** | ≤ 0.08 | | **Silicon (Si)** | ≤ 0.06 | | **Titanium (Ti)** | 0.02–0.10 | | **Other Elements** | ≤ 0.05 each | | **Total Others** | ≤ 0.15 | --- #### **4. Physical Properties** | Property | Value | |----------|-------| | **Density** | 2.65–2.67 g/cm³ (0.0957–0.0964 lb/in³) | | **Melting Range** | ~540–640°C (1000–1185°F) | | **Electrical Conductivity** | ~24–28 % IACS | | **Thermal Conductivity** | 80–100 W/m·K | | **Coefficient of Thermal Expansion** | 21.5–22.5 × 10⁻⁶/°C (20–100°C) | | **Modulus of Elasticity** | 80.0–82.0 GPa (11,600–11,900 ksi) | --- #### **5. Mechanical Properties (Experimental T8-type Temper)** | Property | Typical Value | |----------|---------------| | **Tensile Strength (Ultimate)** | 680–730 MPa (99–106 ksi) | | **Tensile Yield Strength (0.2% Offset)** | 630–680 MPa (91–99 ksi) | | **Elongation at Break** | 4–7% | | **Compressive Yield Strength** | 640–690 MPa (93–100 ksi) | | **Shear Strength** | 390–430 MPa (57–62 ksi) | | **Bearing Yield Strength** | 980–1050 MPa (142–152 ksi) | | **Fracture Toughness (L-T方向)** | 20–26 MPa√m | | **Fatigue Strength** | 200–230 MPa (10⁷ cycles) | --- #### **6. Key Characteristics & Advantages** - **Exceptional Strength**: Among the highest strength aluminum alloys developed - **Maximum Weight Reduction**: 9–11% lower density than conventional aluminum alloys - **Premium Stiffness**: 12–14% higher modulus than traditional aluminum alloys - **Advanced Alloy Design**: Incorporates multiple strengthening mechanisms - **Scandium Enhancement**: Improved microstructure control and thermal stability - **Optimized Precipitation**: Advanced aging response for maximum strength - **Research Focus**: Ongoing development for next-generation applications --- #### **7. Product Applications** - **Advanced Aerospace Structures**: Primary airframe components for next-generation aircraft - **Space Exploration Systems**: Launch vehicle structures and spacecraft components - **Military Defense Applications**: Critical components for advanced military platforms - **High-Performance Motorsports**: Ultimate performance racing components - **Research and Development**: Experimental structures and prototype development - **Specialized Engineering**: Applications requiring maximum strength-to-weight ratio --- #### **8. Available Forms** - Experimental Plate (up to 100 mm thickness) - Research Grade Sheet (1.0–6.0 mm thickness) - Limited Production Extrusions - Laboratory-scale Forgings --- #### **9. Special Considerations** - **Experimental Status**: Not yet commercially standardized - **Limited Availability**: Restricted to research and development programs - **Processing Challenges**: Requires advanced manufacturing techniques - **Quality Assurance**: Extensive testing and characterization needed - **Cost Factors**: Premium material with limited production volumes - **Technical Support**: Available through research partnerships - **Future Potential**: Candidate for future aerospace material standards --- **Disclaimer**: The information presented is experimental and for research reference only. Properties may vary significantly with processing parameters and are subject to ongoing development. For research applications, contact our technical service team for current data and collaboration opportunities.

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 1590 gallon liquid totes Special package is available on request.