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Hợp kim nhôm trong ngành hàng không - Tính chất và ứng dụng

# Hợp Kim Nhôm Trong Ngành Hàng Không - Tính Chất Và Ứng Dụng
Aluminum alloys là vật liệu chủ đạo trong ngành aerospace nhờ tỷ lệ strength-to-weight tuyệt vời.
## Các Series Hợp Kim Nhôm
### 2xxx Series (Al-Cu):
**Đại diện**: 2024, 2014, 2219
**Đặc điểm**:
- **High strength** (up to 470 MPa)
- **Good** machinability
- **Poor** corrosion resistance
- **Heat treatable**
**Ứng dụng**:
- Aircraft structures
- Fuselage frames
- Wing spars
- Landing gear
### 6xxx Series (Al-Mg-Si):
**Đại diện**: 6061, 6082, 6063
**Đặc điểm**:
- **Medium strength** (up to 310 MPa)
- **Excellent** corrosion resistance
- **Good** weldability
- **Extrudable**
**Ứng dụng**:
- Aircraft panels
- Interior structures
- Non-critical components
### 7xxx Series (Al-Zn):
**Đại diện**: 7075, 7050, 7150
**Đặc điểm**:
- **Highest strength** (up to 570 MPa)
- **Excellent** fatigue resistance
- **Good** machinability
- **Premium** applications
**Ứng dụng**:
- Wing structures
- Fuselage frames
- Landing gear
- High-stress components
## Chi Tiết 7075-T6
### Composition:
```
Aluminum: 87.1-91.4%
Zinc: 5.1-6.1%
Magnesium: 2.1-2.9%
Copper: 1.2-2.0%
Chromium: 0.18-0.28%
```
### Mechanical Properties:
```
Tensile Strength: 572 MPa
Yield Strength: 503 MPa
Elongation: 11%
Hardness: 150 HB
Density: 2.81 g/cm³
```
### Heat Treatment:
```
Solution: 465-482°C, 1-2 hours
Quench: Water, <15 seconds
Age: 121°C, 24 hours (T6)
```
## Manufacturing Processes
### Machining:
**Cutting Parameters**:
```
Speed: 200-400 m/min
Feed: 0.1-0.3 mm/rev
Depth: 1-5 mm
Coolant: Flood recommended
```
**Tool Selection**:
- **Carbide** inserts
- **Sharp** cutting edges
- **Positive** rake angles
- **Polished** surfaces
### Welding:
**TIG Welding**:
```
Current: 80-150A AC
Electrode: 2% Thoriated
Filler: ER4043 or ER5356
Gas: Argon, 15-20 L/min
```
**Challenges**:
- **Hot cracking** susceptibility
- **Porosity** issues
- **Strength** reduction in HAZ
### Forming:
**Bend Radius**:
```
2024-T3: 2.5t minimum
6061-T6: 1.5t minimum
7075-T6: 4.0t minimum
```
## Corrosion Protection
### Anodizing:
**Type II** (Sulfuric Acid):
- **Thickness**: 5-25 μm
- **Colors**: Natural, Black, etc.
- **Corrosion** resistance improved
**Type III** (Hard Anodizing):
- **Thickness**: 25-100 μm
- **Hardness**: 300-500 HV
- **Wear** resistance excellent
### Chemical Conversion:
**Alodine/Chromate**:
- **Thin** coating (0.5-3 μm)
- **Paint** adhesion improved
- **Electrical** conductivity maintained
### Primers:
- **Zinc Chromate** (traditional)
- **Zinc Phosphate** (modern)
- **Epoxy** based systems
## Quality Standards
### Aerospace Standards:
- **AMS**: Aerospace Material Specifications
- **ASTM**: American Society for Testing
- **EN**: European Norms
- **JIS**: Japanese Industrial Standards
### Testing Requirements:
```
Tensile Testing: ASTM E8
Hardness: ASTM E18 (Rockwell)
Corrosion: ASTM B117 (Salt spray)
Fatigue: ASTM D7791
```
## Cost Considerations
### Material Costs (per kg):
```
6061-T6: $3-4
2024-T3: $5-7
7075-T6: $8-12
```
### Processing Costs:
- **Machining**: High (work hardening)
- **Welding**: Medium (skill required)
- **Forming**: Medium (springback)
- **Finishing**: Low-Medium
## Future Trends
### Advanced Alloys:
- **Al-Li** alloys (lighter)
- **Al-Sc** alloys (stronger)
- **MMCs** (Metal Matrix Composites)
### Manufacturing:
- **Additive** manufacturing
- **Friction** stir welding
- **Superplastic** forming
## Environmental Impact
### Recycling:
- **95%** energy savings vs primary
- **Infinite** recyclability
- **Closed loop** systems
### Sustainability:
- **Lightweight** = fuel savings
- **Corrosion** resistance = longevity
- **Recyclable** = circular economy
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