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7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm

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7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm

Large Image : 7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm

Product Details:

Place of Origin:	CHINA
Brand Name:	KALU
Certification:	ISO9001
Model Number:	KALU-CZ-Aluminum-Plate-817

Payment & Shipping Terms:

Minimum Order Quantity:	5 tons per Specification
Price:	usd 25000-40000 per ton
Packaging Details:	Stretch film + non-woven fabric + wooden pallet
Delivery Time:	5-8 work days
Payment Terms:	30% TT advance payment, balance paid before shipment
Supply Ability:	2000 tons per month

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Detailed Product Description

Grade:	7050	Temper:	T7451 L/LT/ST, T7651 LT
Thickness:	6-200mm	Standard:	AMS 4050
Tensile Strength:	≥469MPa	Yield Strength:	≥407MPa
Feature1:	Extremely High Strength	Feature2:	Resistance To Spalling Corrosion
Feature3:	Resistance To Stress Corrosion	Feature4:	Good Mechanical Properties And Anodic Reaction
Application1:	Aircraft Lip Grille	Application2:	Wing, Fuselage
Application3:	Suspension System	Application4:	Engine Parts
Highlight:	AMS 4050 Aluminum Plate , 7050 Aluminum Plate T7451 , 7050 Aluminum Plate T7651

7050 Aluminum Plate Grade: 7050 Temper: T7451 L/LT/ST, T7651 LT Thickness: 6-200mm Standard: AMS 4050

Product Detail

ZHANGJIAGANG KALU is manufacturer and supplier of 7050 Aluminum Plate. 7050 aluminum plate is a high-strength heat-treatable alloy with very high strength and resistance to spalling corrosion and stress corrosion fracture. Commonly used in aircraft structural parts for medium and thick plate extruded parts, free forging parts and die forging parts. Manufacture of such parts on the alloy requirements are: resistance to spalling corrosion and stress corrosion cracking ability, fracture toughness and fatigue resistance are strong.

7050 series aluminum alloy main alloying element is zinc, to the alloy containing 3% -75% zinc add magnesium, can form a significant strengthening effect of MgZn2, so that the heat treatment effect of the alloy is far better than the aluminum-zinc binary alloy. By increasing the zinc and magnesium content of the alloy, the tensile hardness will be further improved and the resistance to stress corrosion and spalling corrosion will rise. After heat treatment, very high strength properties are achieved. The material is generally alloyed with a small amount of copper and chromium. The 7050-T7451 aluminum alloy is the best of this family and is regarded as the finest of the aluminum alloys, with high strength, far superior to that of soft steel. This alloy has good mechanical properties and anodic reaction. Mainly used in aerospace, mold processing, machinery and equipment. Work holding fixtures, especially for aircraft structures and other high-stress structures that require high strength and corrosion resistance.

Specification

Grade	7050
Temper	T7451 L/LT/ST, T7651 LT
Thickness	6-200mm
Standard	AMS 4050
Tensile Strength	≥469MPa
Yield Strength	≥407MPa

7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm 0

Feature

Feature1	Extremely high strength
Feature2	Resistance to spalling corrosion
Feature3	Resistance to stress corrosion
Feature4	Good mechanical properties and anodic reaction

7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm 4

Application

Application1	Aircraft lip grille
Application2	Wing, fuselage
Application3	Suspension system
Application4	Engine parts

7050 Aluminum Plate T7451 L/Lt/St T7651 Lt Standard AMS 4050 Thickness 6-200mm 6

Packaging

ZHANGJIAGANG KALU Products are packed and labeled according to the regulations and customer's requests. Great care is taken to avoid any damage which might be caused during storage or transportation. In addition, clear labels are tagged on the outside of the packages for easy identification of the product I. D. and quality information.