Все продукты
Контактное лицо : Cathy
Номер телефона : +86 13812283719
WhatsApp : +8613812283719

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
Место происхождения Шаньдун, Китай
Фирменное наименование CHALCO
Сертификация ISO 9001:2015, ASTM B209, AMS 4045, SAE AMS-QQ-A-250/12
Номер модели АЛ7075-Т6-3.0
Количество мин заказа 1 тонна
Цена USD 3850-4450 / Ton
Упаковывая детали Антикоррозионное масляное покрытие, защитная полиэтиленовая пленка с обеих сторон, усиленный деревян
Время доставки 15-25 рабочих дней после подтверждения заказа
Условия оплаты Т/Т, Л/К по предъявлении
Поставка способности 3000 тонн в месяц
Подробная информация о продукте
Сплав 7075 Характер T6 (термообработанный раствор, искусственно состаренный)
Толщина 3,0 мм Ширина 1219 мм / 1500 мм
Длина 2438 мм/3000 мм/4000 мм Содержание цинка 5,1-6,1%
Содержание магния 2,1-2,9% Предел прочности ≥540 МПа
Предел текучести ≥470 МПа Твердость ≥150 ГБ
Выделить

Aerospace Grade Zinc Alloy

,

Ultra High Strength 7075 Sheet

,

3.0mm Aircraft Structural Wing Plate
Оставьте сообщение
Характер продукции
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.

Бирки:

machinery 1060 Aluminum Sheet Plates

5754 Aluminum Sheet Plates

H26 7075 t6 aluminum plate