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Aluminium 7050 Plates

Aluminium 7050 Plates

Aluminium Alloy 7050 Plates is a high-strength alloy with excellent fatigue properties and corrosion resistance. It comprises zinc, magnesium, copper, chromium, iron and manganese with a relatively low aluminium content. This alloy can be used for heavy load-bearing structures, aircraft components, and automotive parts due to its remarkable strength-to-weight ratio. Additionally, due to its excellent formability characteristics, it has multiple usages in the transportation industry.

 

Aluminium Alloy 7050 Plates possess a high strength-to-weight ratio, making it an ideal choice for aerospace, military and other highly stressed applications. This alloy exhibits excellent fracture toughness, stress corrosion cracking resistance, and good fatigue strength. It can be used in tempers ranging from T7451 (AMS 4201) to T7651 (AMS 4202). Commonly found uses of 7050 aluminium plates include wing skins, fuselage frames and structural components on missiles and aircraft where high strength is required.

Aluminium Alloy 7050 Plates is a high-strength alloy with excellent fatigue properties and corrosion resistance. It comprises zinc, magnesium, copper, chromium, iron and manganese with a relatively low aluminium content. This alloy can be used for heavy load-bearing structures, aircraft components, and automotive parts due to its remarkable strength-to-weight ratio. Additionally, due to its excellent formability characteristics, it has multiple usages in the transportation industry.

 

Aluminium Alloy 7050 Plates possess a high strength-to-weight ratio, making it an ideal choice for aerospace, military and other highly stressed applications. This alloy exhibits excellent fracture toughness, stress corrosion cracking resistance, and good fatigue strength. It can be used in tempers ranging from T7451 (AMS 4201) to T7651 (AMS 4202). Commonly found uses of 7050 aluminium plates include wing skins, fuselage frames and structural components on missiles and aircraft where high strength is required.

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