Aircraft Aluminum Plate

2219 alloy Products Description : Products name:2219-t62 High strength aluminum alloys sheet /2219-t6 aluminum shee/2219 aluminum alloy sheet/2219 aluminum sheet/2219-t851 aluminum plate Temper :T6,t62,t851,T351 Technical:Extrusion &Stretching Featurte of 2219-t62 High strength aluminum alloys sheet High strength and ductility Extremely low level of porosity for excellent fatigue performance Minimal residual stre practically no distortion after

2014 Aluminum Plate has high strength and good cutting performance, but poor corrosion resistance. Widely used in aircraft structures (skin, skeleton, rib beam, bulkhead, etc.) rivets, missile components, truck wheel hubs, propeller components and other structural components. Temper with T3, T4 and T6. Chemical Composition WT(%) Silicon Iron Copper Magnesium Manganese Chromium Zinc Titanium Others Aluminum 0.5~1.2 0.7 3

Product Description 6000 series aluminum is formed by the addition of small amount of copper in pure aluminum, with excellent forming characteristics,high corrosion resistance, good welding and electrical conductivity. Name Alloy 6061 T6 aircraft grade aluminum sheet / plate prices per kg Material 1050,1060,1100,3003,3A21,5052.5005.5083.5A05,6061 Thickness 0.15-200mm Width 20-2500mm Packing Export standard packing or

Products detail Alloy: 7175 AA7175 A7175 Temper:T351,T451,T7651,T7451,T74 Aluminium alloy is a main material in aerospace industry due to its excellent specific strength, corrosion resistance, low temperature performance and welding performance. Tianjin Zhongwang aims at a leading supplier of the global aerospace industry. Key Feature High strength Light weight Good shape Corrosion resistance Good performance under low

1. Alloy : 2A90 LD9 A2018 2018 . Standard:YS/T 439-2001 Aluminum alloy 2A11 LY11 AlCu4MgSi A2017 Application 1. Aerospace Engine Piston Aluminum alloy 2A11 LY11 AlCu4MgSi A2017 Feature : 1. High strength 2. Heat-resistant forged aluminum, 3. Good thermal strength 2A90 A2018 A92018 Aluminum Alloy Plate LD9 2018 Properties Range Si Fe Cu Mn Mg Ni Zn Ti Each total Aluminum Standard 0.5~1.0 0.5~1.0 3.5~4.5 0.20 0.40~0.8 1.8~2.3 Max.0.30

​ Alloy: 2A70 LD7 A2618, Temper : T4,T6,T351 Standard 1. Chemical Composition Limit:GB/T 3191-2010 2. Mechanical Property :GB/T 3191-2010 Features:Strong stability Application of 2A70 LD7 A2618 Aerospace aluminum plate 1. Aircraft skin, 2. Aircraft engine piston, 3. Aircraft wind wheel, Wheel etc 2A70 LD7 A2618 Aluminum Chemical Composition Limit Cu Mg Mn Fe Si Zn Ti Ni other Al 1.9~2.5 1.4~1.8 0.20 0.9~1.5 0.35 0.3 0.02

Alloy:7175 temper:T351,T451,T7651,T7451,T74 Advantages 1. Excellent toughness 2. Excellent anti-fatigue 3. High Strength 4. High extensibility 5. Excellent comprehensive performance 7175 aluminum composition Cu Mg Mn Fe Si Zn Ti Cr Zr Other Al 2.0~2.6 1.9~2.6 0.1 0.15 0.12 5.7~6.7 0.06 0.04 0.08~0.15 0.15 Remainder 7175 Aluminum stretching plate specification Alloy Series Alloy Tempe Thickness (MM) Width (MM) Length (MM

Alloy: 7075-t7351 A7075 B95 76528 A97075 Temper : T7651 ,T7351,t651 t7651 O Features of 7075 T7351 aluminum High strength alloy igh hard alloy aluminum with heat treatable Good mechanical properties Good usability Easy to process and Solderability Corrosion resistance,The antioxidant properties are meet and high standards Moderate toughness Moderate corrosion resistance. 7075-t7351 A7075 B95 76528 A97075 aluminum Mill