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7A04 Aluminum Bars

7A04 Aluminum Bars Specifications

Standards: ASTM B221, B211, B565, B316 3003, DIN AlMnCu

Aluminum bar form: Aluminum round, hexagonal, flat, semi-circular, oval, rectangular black, and glossy finish

Aluminum round bar diameter: 0.1-600mm, etc.

Aluminum hexagonal bar: 0.1-600mm, etc.

Aluminum angle bar size: 0.5mm*40mm*40mm-20mm*400mm*400mm

Aluminum flat steel thickness: 0.1-600mm, etc.

Aluminum flat bar size: 1-2500mm, etc.

Aluminum round bar length: 1-12m, random, fixed, and cut length or according to customer requirements

Product Introduction

Aviation super duralumin alloy, high strength, good wear resistance

7A04 belongs to the Al-Zn-Mg-Cu series of ultra-high-strength aluminum alloys, also known as super-duralumin, which is quite mature in super-duralumin. Use a longer and wider alloy. High strength, good heat treatment strengthening effect, moderate plasticity under annealing and new quenching; Different from duralumin, the corrosion resistance in the artificial aging state is better than that in the natural aging state, and the natural aging process is slow, and it takes 3 months to reach the peak of aging hardening, so 7A04 is used in the quenching artificial aging state. Its disadvantages are that the tissue stability is not high, the fatigue strength of the low frequency is low, and there is a tendency to stress corrosion and rupture. Alloy spot welding is good, gas welding is poor, and the machinability is good after heat treatment, but the machinability after annealing is not good.

Typical uses

7A04 is mainly used for the manufacture of aircraft structures and other high stress structural parts that require high strength and corrosion resistance, such as aircraft, lower wing wall panels, trusses, etc. Good plasticity after solid solution treatment, good heat treatment strengthening effect, good strength below 150 degrees, and particularly good low temperature strength, poor welding performance, stress corrosion cracking tendency. It is also widely used in mold processing, machinery and equipment, tooling fixtures, aerospace industry, blow molding (bottle) mold, ultrasonic plastic welding mold, golf head, shoe mold, paper mold, foam molding mold, wax removal mold, mechanical equipment, used to make high-end aluminum alloy bicycle frame. In 2014, it will be used for the first time as the body material of the smartphone OPPO N3.

Chemical composition

Alloy grade

Si

Fe

Cu

Mn

Mg

Cr

Zn

Ti

Zr

other

AL

New grade

Old grade

0.50

0.50

1.4-2.0

0.2-0.6

1.8-2.8

0.1-0.25

5.0-7.0

0.10

0.08-0.15

each

total

7A04

LC4

0.05

0.15

Allowance

Mechanical properties

Aluminum alloy grade andtensile strength Rm/MpaYield strength
Rp0.2/Mpa
Elongation/%hardness/ HBWα
7A04-T64904107150

Physical properties

Aluminum alloy grade and
state
Coefficient of thermal expansion
(20-100℃)
μm/m·k
Melting point range
(℃)
electrical conductivity
20℃(68℉)
(%IACS)
Resistivity20℃(68℉)
Ωmm2/m
density
(20℃)(g/cm3)
7A04-T623.6485-650330.05152.9

Quality characteristics

Density: 2.90g/cm³.

Shear strength: alloy (bare) and aluminum-clad alloy, O state: 152MPa (22ksi); Alloy (bare) T6, T651 status: 331MPa (48ksi); Aluminum alloy T6, T651 Status: 317MPa (46ksi)

Hardness: O state: 60HB; T6, T651 Status: 150HB; The data is taken from the 10 mm diameter ball and the test results of 30 s under a load of 500 kg.

Poisson’s ratio: 0.33.

Modulus of elasticity: Tensile: 71.0 GPa (10.3×106psi), Shear: 26.9GPa (3.9×106psi), Compression 72.4GPa (10.5×106psi)

Fatigue strength: T6, T651, T73 Status: Smooth non-notched specimen in R· R· In the Moore type test, 5×108 cycles were made at 159MPa (23ksi).

7A04 Aluminum Bar Packages

The following is our company’s standard aluminum coil export packaging. If the customer has any packaging requirements, our company can meet them.

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