Customized aerospace aluminum alloy die – castings

Processing materials: Aviation – grade aluminum alloys are used (such as A380, A356, ZL104, etc.).
Characteristics: High corrosion resistance, adaptable to complex aviation environments such as high humidity and salt spray.
Processes: High – pressure die – casting (with pressure up to over 1000 bar) or vacuum die – casting processes are adopted.
Accuracy: The tolerance grade can reach CT6 – CT8 (GB/T 6414), and the surface roughness is Ra≤3.2μm.
Customization: Full – process customization services from drawing design, mold development to mass production are supported.
Standards: Comply with AMS 2771 (heat treatment of aluminum alloys), ASTM B179 (die – casting standards) and AS9100 aviation quality management system.

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Description

1. Processable Materials (Aerospace-Grade Alloys)

Material Type
Typical Grades
Core Properties
Aluminum Alloy
7075-T6, 6061-T6
Tensile Strength ≥572MPa, Density 2.8g/cm³, Heat Resistance ≤200℃
Titanium Alloy
Ti-6Al-4V (TC4)
Tensile Strength ≥900MPa, Density 4.43g/cm³, Heat Resistance ≤500℃
Magnesium Alloy
AZ91D
Tensile Strength ≥240MPa, Density 1.8g/cm³, Optimal for Lightweight Design
High-Temperature Alloy
Inconel 718
Tensile Strength ≥1220MPa, Heat Resistance ≤700℃, Excellent Fatigue Resistance

2. Dimensional Processing Capabilities

  • Size Range: Maximum 1000×800×500mm (L×W×H)
  • Minimum Wall Thickness: 0.5mm (complex structures) / 1.0mm (regular parts)
  • Dimensional Tolerance: GB/T 6414 CT4 Grade (±0.15mm/100mm)
  • Surface Roughness: Ra≤1.6μm (mold surface) / Ra≤0.8μm (polished surface)
  • Weight Range: 0.1kg–50kg (per part)

3. Surface Treatment Processes (Aerospace Standards)

Process
Performance Indicators
Application Scenarios
Anodizing
Oxide film thickness 10–25μm, Salt spray test ≥500h
Corrosion protection & insulation for aluminum parts
Electroless Nickel Plating
Coating hardness HV 500–600, Thickness 5–15μm
Wear resistance enhancement for titanium parts
Passivation Treatment
Blue spot test corrosion-free, Film thickness 2–5μm
Oxidation resistance for high-temperature alloys
Conductive Anodizing
Surface resistance ≤0.1Ω, Film thickness 0.3–0.5μm
Electromagnetic shielding components

4. Core Characteristics (Data-Driven Advantages)

  • High Precision: CMM inspection accuracy ±0.005mm, First-piece full inspection rate 100%
  • Low Defect Rate: X-ray flaw detection defect rate ≤0.1%, Air tightness test 0.6MPa leak-free
  • Long Service Life: Mold life ≥50,000 cycles (titanium parts), Fatigue test cycles ≥10⁶ times
  • Lightweight Design: Specific strength (strength/density) 300%+ higher than traditional steel

5. Application Areas (Aerospace Adaptation)

  • Engine Systems: Compressor blades, fuel pump housings (high pressure resistance 20MPa, heat resistance 650℃)
  • Structural Components: Wing ribs, fuselage frames (weight reduction 15%–30%, compliant with AS9100D)
  • Landing Gear Systems: Joint connectors, brackets (tensile strength ≥800MPa, passed aerospace stress tests)
  • Avionics Equipment: Enclosures & mounting frames (electromagnetic shielding effectiveness ≥60dB, surface conductivity ≥10⁶S/m)
Contact now for exclusive quotes including material solutions + inspection reports + aerospace certifications!