• 7050 T7451 Aerospace Aluminum Alloy Plate Bar with Ultra High Strength and SCC Resistance for Aircraft Components
  • 7050 T7451 Aerospace Aluminum Alloy Plate Bar with Ultra High Strength and SCC Resistance for Aircraft Components
7050 T7451 Aerospace Aluminum Alloy Plate Bar with Ultra High Strength and SCC Resistance for Aircraft Components

7050 T7451 Aerospace Aluminum Alloy Plate Bar with Ultra High Strength and SCC Resistance for Aircraft Components

Product Details:

Place of Origin: Guangdong, China
Brand Name: WNRLN
Certification: ISO 9001:2015, AMS 4050
Model Number: 7050-T7451-PB

Payment & Shipping Terms:

Minimum Order Quantity: 500 kg
Price: USD 3.2-5.8 / kg
Packaging Details: Export-grade PVC wrapping with wooden pallet, moisture-proof packaging, seaworthy shipping protection
Delivery Time: 5 working days for stock, 15-25 days for production
Payment Terms: T/T, L/C, Western Union
Supply Ability: 200 Metric Tons per Month
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Detail Information

Alloy: 7050 Temper: T7451
Thickness Range: 12mm - 200mm Tensile Strength: ≥524 MPa
Yield Strength: ≥455 MPa Fracture Toughness: Excellent
Shape: Plate Bar
Highlight:

7050 T7451 Aerospace Plate Bar

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Ultra High Strength Aluminum Bar

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Stress Corrosion Resistant Alloy Bar

Product Description

7050 T7451 Aerospace Aluminum Alloy Plate Bar Ultra High Strength SCC Resistant Aircraft Wing Rib Components
7050 T7451 Aerospace Aluminum Alloy Plate Bar

7050-T7451 aluminum alloy plate bar is designed for the most demanding aerospace structural applications. With optimized zinc-magnesium-copper composition and T7451 over-aged temper, it delivers exceptional strength combined with superior stress corrosion cracking resistance for critical aircraft components.

Key Features
  • Tensile strength: ≥524 MPa
  • Superior stress corrosion cracking resistance (SCC)
  • Excellent fracture toughness
  • Good exfoliation corrosion resistance
  • Precision machined flatness tolerance
Technical Specifications
Alloy 7050 (Al-Zn-Mg-Cu-Zr)
Temper T7451
Thickness Range 12mm - 200mm
Width Up to 2500mm
Yield Strength ≥455 MPa
Elongation ≥8%
Applications
  • Aircraft wing ribs
  • Fuselage frames
  • Bulkheads
  • Upper wing skins
  • Military aircraft structural parts

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