Aluminum Alloy and Temper Designation Systems

     

Introduction

The numbers in an aluminum alloy contain definite information. The four digit number defines the alloy series and deontes the particular alloy. The letter and numbers in the suffix describe the temper, heat treatment and the method of manufacture. This is illustrated in the examples below.


Examples

Non-Heat-Treatable

5

Main alloying element (manganese)

H

Strain hardened

0

No modifications of original alloy

1

Basic operation

8

Specific Alloy

1

Degree of strain hardening

6

2

Variation of two digit temper

 

 

 

 

Heat-Treatable

2

Main alloying element (copper)

H

Heat treated

0

No modifications of original alloy

1

Specific sequence of treatments

2

Specific Alloy

1

Additional Processing for Properties

4

2


Designation Systems

Alloy Designation System
A system of four digit numbers identifies wrought aluminum and its alloys. As was noted previously, the first digit indicates the alloy group and the second digit indicates alloy modifications or impurity limits. The last two digits identify the alloy or indicate aluminum purity.

Temper Designation System
As previously noted, the temper designation follows the alloy designation, the two being separated by a dash. The temper designation describes how the particular alloy was treated and will establish the mechanical properties of the material.

Designations

Basic Temper Designations
F-as fabricated. Applies to the products of shaping processes in which no special control over thermal conditions or strain-hardening is employed. For wrought products, there are no mechanical property limits.

O-annealed (wrought products only). Applies to wrought products which are fully annealed to obtain the lowest strength conditions.

H-strain-hardened (wrought products only). Applies to products which have their strength increased by strain-hardening, with or without supplementary thermal treatments to produce some reduction in strength. The H is always followed by two or more digits.

T-applies to products which are thermally treated, with or without supplementary strain-hardening, to produce stable tempers. The T is always followed by one or more digits.


The H and T tempers are further subdivided:

Subdivision of H Temper: Strain-Hardened

The first digit following the H indicates the specific combination of basic operations, as follows:

H1-strain-hardened only. Applies to the products which are strain-hardened to obtain the desired strength without supplementary thermal treatment. The number following this designation indicates the degree of strain-hardening.

H2-strain-hardened and partially annealed. Applies to the products which are strain-hardened more than the desired final amount and then reduced in strength to the desired level by partial annealing. For alloys that age-soften at room temperature, the H2 tempers have the same minimum ultimate tensile strength as the corresponding H3 tempers. For other alloys, the H2 tempers have the same minimum ultimate tensile strength as the corresponding H1 tempers and slightly higher elongation. The number following this designation indicates the degree of strain-hardening remaining after the product has been partially annealed.

H3-strain-hardened and stabalized. Applies to products which are strain-hardened and whose mechanical properties are stabilized by a low temperature thermal treatment which results in slightly lowered tensile strength and improved ductility. This designation is applicable only to those alloys which, unless stabilized, gradually age-soften at room temperature. The number following this designation indicates the degree of strain-hardening before the stabilization treatment.

The third digit, when used, indicates a variation of a two digit temper. It is used when the degree of control of temper or the mechanical properties are different from but close to those for the two-digit H temper designation to which it is added, or when some other characteristic is significantly affected.

The following three-digit H temper designations have been assigned for wrought products in all alloys:

H111 - Applies to products which are strainhardened less than the amount required for a controlled H11 temper.

H112 - Applies to products which acquire some temper from shaping processes not having special control over the amount of strain-hardening or thermal treatment, but for which there are mechanical property limits.

The following three-digit H temper designations have been assigned for wrought products in alloys containing over a nominal 4% magnesium.

H311 - Applies to products which are strain-hardened less than the amount required for a controlled H31 temper.

H321 - Applies to products which are strain-hardened less than the amount required for a controlled H32 temper.

H323 & H343 - Applies to products which are specially fabricated to have acceptable resistance to stress corrosion cracking.

Subdivisions of T Temper: Thermally Treated

Numerals 1 through 10 following the T indicate specific sequences of basic treatments, as follows:

T1-Applies to products for which the rate of cooling from an elevated temperature shaping process, such as casting or extrusion, is such that their strength is increased by room temperature aging.

T2-Applies to cast products which are annealed to improve ductility and dimensional stability.

T3-Applies to products which are cold worked to improve strength, or in which the effect of cold work in flattening or straightening may not be recognized in mechanical property limits.

T4-Applies to products which are not cold worked after solution heat-treatment, or in which the effect of cold work in flattening or straightening may not be recognized in mechanical property limits.

T5-Applies to products which are cooled from an elevated temperature shaping process, such as casting o r extrusion, and then artificially aged to improve mechanical properties or dimensional stability or both.

T6-Applies to products which are not cold worked after solution heat-treatment, or in which the effect of cold work in flattening or strengthening may not be recognized in mechanical property limits.

T7-Applies to products which are stabilized to carry them beyond the point of maximum strength to provide control of some special characteristics.

T8-Applies to products which are cold worked to improve strength, or in which the effect of cold work in flattening or straightening is recognized in mechanical property limits.

T9-Applies to products which are cold worked to improve strength.

T10-Applies to products which are artificially aged after cooling from an elevated temperature shaping process, such as casting or extrusion, and then cold worked to further improve strength.

Additional Digits for T Tempers

The following additional digits have been assigned for stress-relieved tempers or wrought products:

TX51-Applies to the following products when stretched the indicated amounts after solution heat-treatment.

Plate - 1½ to 3% permanent set. Rod, bar, shapes, extruded tube - 1 to 3% permanent set. Applies directly to plate and rolled or cold finished rod and bar. These products receive no further straightening after stretching. Applies to extruded rod, bar, shapes and tube when designated as follows:

TX510-Products that receive no further straightening after stretching.

TX511-Products that may receive minor straightening after stretching to comply with standard tolerances.

TX52-Applies to products which are stress-relieved by compressing after solution heat-treatment, to produce a permanent set of 1 to 5%.

The following temper designations have been assigned for variations of T4 and T6 tempers of wrought products:

T-42-solution heat-treated from the O or F temper by the user, or by the producer to demonstrate response to heat-treatment, and naturally aged to a substantially stable condition.

T-62-solution heated treated from the O or F temper by the user, or by the producer to demonstrate response to heat-treatment, and artificially aged. Apply when available data indicate that any characteristic such as corrosion resistance, fatigue, or a mechanical property is significantly different from that for the T4 to T6 temper, respectively.

The solution heat-treatment practice used is the same as that for the T4 temper of the same alloy and product, and the artificial aging practice used is usually the same as that for the T6 temper of the same alloy and product. Material which is formed or cold worked by the user prior to solution heat-treatment may not attain the mechanical properties applicable to these tempers.

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