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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
Lugar de origen Shandong, China
Nombre de la marca CHALCO
Certificación ISO 9001:2015, ASTM B209, AMS 4045, SAE AMS-QQ-A-250/12
Número de modelo AL7075-T6-3.0
Cantidad de orden mínima 1 tonelada
Precio USD 3850-4450 / Ton
Detalles de empaquetado Recubrimiento de aceite anticorrosión, película protectora de PE en ambos lados, plataforma de mader
Tiempo de entrega 15-25 días hábiles después de la confirmación del pedido
Condiciones de pago T/T, L/C a la vista
Capacidad de la fuente 3000 toneladas por mes
Datos del producto
Aleación 7075 Temperamento T6 (Solución tratada térmicamente envejecida artificialmente)
Espesor 3,0 mm Ancho Las medidas de seguridad se aplican a los vehículos de las categorías M1 y M2.
Longitud 2438 mm / 3000 mm / 4000 mm Contenido de zinc 5,1-6,1%
Contenido del magnesio 2,1-2,9% Resistencia a la tracción ≥540 MPa
Fuerza de producción ≥470MPa Dureza ≥150 HB
Resaltar

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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Descripción de producto
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.

Etiquetas:

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5754 Aluminum Sheet Plates

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