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2xxx Series Fatigue Resistance 2014 Aluminum Alloy Plate For Aircraft Skin

2xxx Series Fatigue Resistance 2014 Aluminum Alloy Plate For Aircraft Skin

Fatigue Resistance 2014 Aluminum Plate

2xxx Series 2014 Aluminum Plate

Aircraft Skin 2014 Aluminum Plate

Place of Origin:

CHINA

Brand Name:

JERO

Certification:

NADCAP AMS AS9100D IRIS

Model Number:

JA72

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Product Details
Type:
A2014 Luminum Plate
Alloy:
AA2014
Temper:
T4 T6 T62
Thickness:
4-12mm
Application:
Aircraft Skin
Trade Terms:
FOB,CIF,CNF,EXW
Highlight:

Fatigue Resistance 2014 Aluminum Plate

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2xxx Series 2014 Aluminum Plate

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Aircraft Skin 2014 Aluminum Plate

Payment & Shipping Terms
Minimum Order Quantity
8 TONS
Price
2800-3200USD/TON
Packaging Details
STANDARD EXPORT PACKAGES
Delivery Time
25-30 WORKING DAYS
Payment Terms
L/C,T/T,Western Union
Supply Ability
2,500 TONS PER MONTH
Product Description
2xxx Series Fatigue Resistance 2014 Aluminum Alloy Plate For Aircraft Skin
2xxx Series 2014 Aluminum Alloy Sheet For Aerospace Industry

2014 alloy is primarily used in aerospace/military applications where high strength is critical. For commercial uses, modified 2XXX/7XXX alloys are often preferred due to better corrosion resistance.

Properties of 2014 Aluminum Alloy
Composition
Primarily composed of copper (3.9-5.0%), magnesium (0.2-0.8%), and manganese (0.4-1.2%). Strengthened by precipitation hardening (θ' and S phases).
Mechanical Properties
Tensile strength: ≥425 MPa (T6 temper)
Yield strength: ≥370 MPa
Elongation: 3-10% (varies with temper)
Corrosion Resistance
Poor due to high copper content; requires alclad (pure aluminum cladding) or coatings for skin applications.
Workability
Good hot workability but challenging for cold working (annealing may be needed).
Advantages for Aircraft Skin
  • High Strength-to-Weight Ratio: Comparable to steel, reducing structural weight and improving fuel efficiency.
  • Fatigue Resistance: Suitable for cyclic aerodynamic loads during flight.
  • Formability: Compatible with riveting, welding (with specialized techniques), and shaping (e.g., curved skin panels).
  • Cost-Effectiveness: More economical than advanced alloys like 2024 or 7075, ideal for non-critical structures.
Common Tempers
Temper Process Characteristics
T4 Solution heat treated + naturally aged High strength + good ductility
T6 Solution heat treated + artificially aged Maximum strength/hardness
O Annealed Soft state for forming
Alloy Comparison
Property 2014 2024 (More Common) 7075
Strength High Medium-High Very High
Corrosion Poor (Alclad) Moderate (Alclad) Poor (Coated)
Cost Moderate Moderate High
Typical Use Secondary Primary Skin High-Stress
Typical Thicknesses
Aerospace: 1.5-50 mm
Machinery: 5-30 mm
Transportation: 2-20 mm
Tooling: 10-100 mm
Limitations
Poor weldability (requires special techniques)
Low corrosion resistance (needs coating)
Fast work hardening (may require annealing)
2xxx Series Fatigue Resistance 2014 Aluminum Alloy Plate For Aircraft Skin 0
Our Company Advantages
Technological & Production Strengths
  • R&D Capabilities: Own a national-level corporate technology center and contributes to industry standards.
  • Production Scale: We had an annual capacity exceeding 1 million tons of aluminium large-scale rolling mills.
  • Production Ability: We can produce the great Aluminum material for automobile, railway transportation, marine, aerospace etc fields, and obtained the relevant certification.
Advanced Manufacturing Equipment
Code Name Brand
a aluminum ignot melting furnace GAUTSCHI (Switzerland)
b 2800mm width single stand cold rolling mill SMS Group (Germany)
c 4 continuous hot rolling mills SMS Group (Germany)
d heavy crop and dividing shear SMS Group (Germany)
e coil material annealing furnace SMS Group (Germany)
f all automatic three-dimensional elevated warehouse Dematic (USA)
2xxx Series Fatigue Resistance 2014 Aluminum Alloy Plate For Aircraft Skin 1

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