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7075 T6 Aerospace Grade Aluminum Sheet 3.0mm Zinc Magnesium Copper Alloy High Strength for Aircraft Wing Components

  • 7075 T6 Aerospace Grade Aluminum Sheet 3.0mm Zinc Magnesium Copper Alloy High Strength for Aircraft Wing Components
Plaats van herkomst Shandong, China
Merknaam CHALCO
Certificering ISO 9001:2015, ASTM B209, AMS 4045, SAE AMS-QQ-A-250/12
Modelnummer AL7075-T6-3.0
Min. bestelaantal 1 ton
Prijs USD 3850-4450 / Ton
Verpakking Details Corrosiewerende oliecoating, PE-beschermfolie aan beide zijden, versterkte houten pallet met stalen
Levertijd 15-25 werkdagen na orderbevestiging
Betalingscondities T/T, L/C op zicht
Levering vermogen 3000 ton per maand
Productdetails
Legering 7075 Woedeaanval T6 (Oplossing, hittebehandeld, kunstmatig verouderd)
Dikte 3,0 mm Breedte 1219 mm / 1500 mm
Lengte 2438 mm / 3000 mm / 4000 mm Zinkinhoud 5,1-6,1%
Magnesiuminhoud 2,1-2,9% Treksterkte ≥540 MPa
Opbrengststerkte ≥470 MPa Hardheid ≥150 HB
Markeren

Aerospace Grade Zinc Alloy

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Ultra High Strength 7075 Sheet

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3.0mm Aircraft Structural Wing Plate
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Productomschrijving
7075 T6 Aerospace Grade Aluminum Sheet 3.0mm Zinc Magnesium Copper Alloy High Strength for Aircraft Wing Components
Ultra-High Strength at One-Third the Weight of Steel

Our 7075 T6 Aerospace Grade Aluminum Sheet is the highest strength aluminum alloy commercially available, with tensile strength exceeding 540 MPa — approaching that of structural steel at only one-third the weight. Engineered with a zinc-magnesium-copper alloy system and fully heat treated to T6 temper, this 3.0mm sheet is the definitive choice for aircraft structural components, wing spars, fuselage frames, and high-stress aerospace applications where failure is not an option.

Key Features
  • Ultra-High Strength: ≥540 MPa tensile strength and ≥470 MPa yield strength, comparable to mild structural steel (S235) but at only 34% of the weight
  • Zinc-Magnesium-Copper Alloy: 5.1-6.1% Zn, 2.1-2.9% Mg, and 1.2-2.0% Cu provides precipitation hardening capability for maximum mechanical properties
  • Full T6 Heat Treatment: Solution treated at 480°C, water quenched, and artificially aged at 120°C for 24 hours for peak strength and hardness
  • Excellent Fatigue Properties: Superior fatigue crack growth resistance critical for cyclic loading in aerospace structures
  • Outstanding Strength Retention: Maintains significant strength at moderately elevated temperatures up to 120°C continuous service
Applications
  • Aircraft wing spars and ribs
  • Fuselage frames
  • Missile components
  • High-performance bicycle frames
  • Rock climbing equipment
  • Competition firearms receivers
  • Molds for plastic injection
  • Precision structural components where weight reduction is critical
Quality Assurance
Comprehensive Testing & Certification

Every sheet undergoes electrical conductivity testing (32-36% IACS for T6 verification), ultrasonic C-scan inspection for internal integrity per AMS-STD-2154 Class A, chemical analysis by OES, tensile testing per ASTM E8, and hardness testing. AMS 4045 aerospace specification compliance with full melt-to-product traceability. NADCAP-accredited testing laboratory certification available.

Markeringen:

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