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6061 T6 Aircraft Aluminum Sheet High Corrosion Resistance 10.8mm Thickness

Place of Origin china
Brand Name HUANYU
Model Number HYAP6061T6
Minimum Order Quantity 1 metric ton
Price US$3499-US$3899/ metric ton
Packaging Details plywood case
Delivery Time 7 days
Payment Terms T/T
Supply Ability 478 metric tons per month
Product Details
Thickness 10.8mm Ultimate Tensile Strength 310 MPa
Tensile Yield Strength 276 MPa Elongation At Break 17%
Hardness, Brinell 95 Density 2.7g/c.c.
Melting Point 582 - 652 °C Electrical Resistivity 3.99e-006 Ohm-cm
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airplane aluminum sheets

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7075 t6 aluminum plate

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Product Description

 

6061 Aircraft Aluminum Sheet Plate

is made of one of the most versatile of all of the aluminum alloys. Aircraft Aluminum Sheet Plateis the alloy of choice for all-purpose applications.

This alloy has medium strength, formability, weldability, machinability and corrosion resistance. Aircraft Aluminum Sheet Plateis used for tooling plate, architectural applications, transportation equipment, bridge railing components, and is useful in welded structural application.

 

 

6061 Aluminum Chemical Composition Limits
Weight% Al Si Fe Cu Mn Mg Cr Zn Ti Other Each Others Total
6061 Bal 0.40 - 0.80 0.70 max 0.15-0.40 0.15 0.8-1.2 0.04-0.35 0.25 max 0.15 max 0.05 max 0.15 max

 

 

Physical Properties Metric English Comments
6061 T6  Aircraft Aluminum Sheet  High Corrosion Resistance 10.8mm Thickness 0
Density 2.7 g/cc 0.0975 lb/in³ AA; Typical

Mechanical Properties
6061 T6  Aircraft Aluminum Sheet  High Corrosion Resistance 10.8mm Thickness 0
Hardness, Brinell 95 95 AA; Typical; 500 g load; 10 mm ball
Hardness, Knoop 120 120 Converted from Brinell Hardness Value
Hardness, Rockwell A 40 40 Converted from Brinell Hardness Value
Hardness, Rockwell B 60 60 Converted from Brinell Hardness Value
Hardness, Vickers 107 107 Converted from Brinell Hardness Value
Ultimate Tensile Strength 310 MPa 45000 psi AA; Typical
Tensile Yield Strength 276 MPa 40000 psi AA; Typical
Elongation at Break 12 % 12 % AA; Typical; 1/16 in. (1.6 mm) Thickness
Elongation at Break 17 % 17 % AA; Typical; 1/2 in. (12.7 mm) Diameter
Modulus of Elasticity 68.9 GPa 10000 ksi AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
Notched Tensile Strength 324 MPa 47000 psi 2.5 cm width x 0.16 cm thick side-notched specimen, Kt = 17.
Ultimate Bearing Strength 607 MPa 88000 psi Edge distance/pin diameter = 2.0
Bearing Yield Strength 386 MPa 56000 psi Edge distance/pin diameter = 2.0
Poisson's Ratio 0.33 0.33 Estimated from trends in similar Al alloys.
Fatigue Strength 96.5 MPa 14000 psi AA; 500,000,000 cycles completely reversed stress; RR Moore machine/specimen
Fracture Toughness 29 MPa-m½ 26.4 ksi-in½ KIC; TL orientation.
Machinability 50 % 50 % 0-100 Scale of Aluminum Alloys
Shear Modulus 26 GPa 3770 ksi Estimated from similar Al alloys.
Shear Strength 207 MPa 30000 psi AA; Typical

 

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