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7075 Ultra-Thick Aerospace Aluminum Forging Plate
1. Material Composition & Manufacturing Process 7075 aluminum alloy (AMS 4045, ASTM B247) represents a premium high-strength aerospace material optimized for critical aircraft structural components. The ultra-thick forged plate variant provides exceptional strength-to-weight performance through specialized processing: Primary Alloying Elements: Zinc (Zn): 5.1-6.1% (primary strengthening element) Magnesium (Mg): 2.1-2.9% (precipitation hardening) Copper (Cu): 1.2-2.0% (strength […]
5083 Ultra-Thick Aluminum Forging Plate
1. Material Composition & Manufacturing Process 5083 aluminum alloy (ASTM B209, EN AW-5083) is a high-strength, non-heat-treatable Al-Mg alloy renowned for exceptional weldability and superior corrosion resistance in marine environments. The ultra-thick forged plate variant offers enhanced mechanical properties through controlled deformation processing: Primary Alloying Elements: Magnesium (Mg): 4.0-4.9% (primary solid-solution strengthener) Manganese (Mn): 0.40-1.0% […]
7050 Ultra-Hard Aluminum Alloy Forging Plate
1. Material Composition & Manufacturing Process 7050 aluminum alloy (AMS 4050, ASTM B247) represents an advanced aerospace-grade Al-Zn-Mg-Cu alloy engineered for superior damage tolerance and exceptional strength-to-weight ratio. The ultra-hard forged plate variant delivers optimized mechanical properties through precision thermomechanical processing: Alloy Chemistry: Zinc (Zn): 5.7-6.7% (primary strengthening element) Copper (Cu): 2.0-2.6% (precipitation hardening) Magnesium […]
6061 Ultra-Thick Aluminum Forging Plate
1. Material Composition & Manufacturing Process 6061 aluminum alloy (ASTM B209, AMS 4025) is a heat-treatable Al-Mg-Si alloy engineered for versatility and excellent mechanical properties. Ultra-thick forged plate variants (>150mm) offer exceptional structural integrity through specialized manufacturing: Alloy Chemistry: Magnesium (Mg): 0.8-1.2% (Mg₂Si precipitation) Silicon (Si): 0.4-0.8% (Mg₂Si formation) Copper (Cu): 0.15-0.40% (strengthening) Chromium (Cr): […]
5052 Aluminum Alloy Forged Plate
1. Material Composition & Manufacturing Process 5052 aluminum alloy (ASTM B209, AMS 4015) is a non-heat-treatable Al-Mg alloy optimized for exceptional corrosion resistance and good formability. The forged plate variant offers enhanced mechanical properties through controlled deformation processing: Alloy Chemistry: Magnesium (Mg): 2.2-2.8% (solid solution strengthening) Chromium (Cr): 0.15-0.35% (corrosion resistance enhancer) Iron (Fe): ≤0.40% […]
2024 T351 Aluminum Plate
1. Material Composition & Manufacturing Process 2024 aluminum alloy (AMS 4035, ASTM B209, EN 485) is a high-strength Al-Cu-Mg alloy engineered for critical structural applications. The T351 temper provides optimal fracture toughness through solution heat treatment, controlled stretching, and natural aging: Alloy Chemistry: Copper (Cu): 3.8-4.9% (precipitation hardening) Magnesium (Mg): 1.2-1.8% (S-phase formation) Manganese (Mn): […]
7075 Aluminum Plate
Material Composition & Standards • Conforms to ASTM B209, GB/T 3190, EN 485-2 • Key elements: Zn (5.6%), Mg (2.5%), Cu (1.6%), Al (~87.1%) Strength Properties • Tensile Strength: ≥572 MPa (T6 temper) • Yield Strength: ≥503 MPa • Hardness: ~150 HB (Brinell) Heat Treatment Tempers Common tempers: O, T6, T651, T73, T7351 Optimal choice: T651(excellent machinability + low […]
5083 H116 Aluminum Plate
1. Material Composition & Manufacturing Process 5083 aluminum alloy (ASTM B209, EN 485, AMS 4027) is a non-heat-treatable Al-Mg alloy designed for extreme corrosion resistance and weldability. The H116 temper provides optimal combination of strength and stress corrosion resistance: Alloy Chemistry: Magnesium (Mg): 4.0-4.9% (solid solution strengthening) Manganese (Mn): 0.4-1.0% (grain refinement) Chromium (Cr): 0.05-0.25% […]
6061 T6 Aluminum Plate
1. Material Composition & Manufacturing Process 6061 aluminum alloy (ASTM B209, AMS QQ-A-250/11) is a heat-treatable Al-Mg-Si alloy optimized for high strength-to-weight ratio applications. The T6 temper provides optimal mechanical properties through solution heat treatment and artificial aging: Alloy Chemistry: Magnesium (Mg): 0.8-1.2% (solution strengthening) Silicon (Si): 0.4-0.8% (precipitation hardening) Copper (Cu): 0.15-0.40% (enhanced machining) […]
5052 Aluminum Plate
1. Material Composition & Manufacturing Process 5052 aluminum alloy (ASTM B209, AMS 4002) features a magnesium-chromium alloying system optimized for corrosion resistance and formability: Alloy Chemistry: Magnesium (Mg): 2.2-2.8% (solution strengthening) Chromium (Cr): 0.15-0.35% (corrosion resistance) Iron (Fe): ≤0.40% max Silicon (Si): ≤0.25% max Copper (Cu): ≤0.10% max Base Material: Aluminum (Al): ≥96.7% (balance) Trace […]
