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Aluminum Alloys: A Guide to Bending and Tempers

Aluminum Stretch Forming Process

Aluminum alloys offer a myriad of possibilities in various industries, from aerospace to automotive and beyond. Understanding their behavior in bending operations and the role of tempers is crucial for achieving optimal results.
Aluminum alloys are prized for their versatility, lightweight nature, and corrosion resistance, making them ideal for a wide range of applications. From structural components to intricate designs, aluminum alloys offer unparalleled flexibility and durability.

PBA aluminum bending machine

Tempering Expectations: The Crucial Role of Tempers in Bending

Tempers play a pivotal role in determining the bendability of aluminum, with different alloys requiring specific tempers for optimal results:

Non-Heat-Treatable Alloys (3xxx and 5xxx series): The O-temper is preferred for bending, offering high formability without compromising strength.
Heat-Treatable Alloys (6xxx, 7xxx, and 2xxx series): Ideally bent in the T4 condition due to reduced yield strength, although natural aging may necessitate transitioning to the more challenging T6 temper for certain applications.

Understanding Aluminium Tempers and Their Impact on Bending

Aluminum temper refers to the material’s hardness and strength achieved through heat treatment and mechanical working. Different tempers significantly influence bending outcomes:

O (Annealed) Temper: Highly formable but lacks the strength for complex bends, making it suitable for simple bending operations.
H (Strain-Hardened) Tempers (e.g., H14 and H24): Strike a balance between formability and strength, allowing for moderate bends without cracking.
T (Thermal Treatment) Tempers (e.g., T6 and T651): Offer high strength and moderate formability, but require caution, especially for tight radii bends, to avoid cracking due to reduced ductility.

Choosing the Right Aluminum Alloy and Temper for Profile Bending

Stretch Forming Process of Aluminum Alloy Automobile Roof Rack【Stretch Forming Machine

Selecting the appropriate alloy and temper is critical for both manufacturability and performance. Factors to consider include bending complexity, required strength, and environmental conditions:

  • Simple Bends: Alloys from the 1xxx and 3xxx series in O or H14 temper suffice, prioritizing formability.
  • Balanced Formability and Strength: The 6xxx series in H14 or H24 temper is commonly chosen.
  • High Strength and Corrosion Resistance: The 5xxx series with appropriate tempers meets demands for strength and corrosion resistance in challenging applications.
  • Aluminum alloys 6061 and 6082 are prized for their heat-treatable properties, boasting excellent elongation when annealed. However, as they transition to T4 and T6 tempers, their bendability diminishes. To optimize bending, starting in the T4 state and later transitioning to T6 through heat treatment is recommended.

By understanding the nuances of tempers and their impact on bending, manufacturers can make informed decisions to achieve optimal results in profile bending processes.

Aluminum Mechanical Properties

per The Aluminum Association, Inc.

Alloy & Temper Thickness Tensile Strengths – ksi
ULTIMATE YIELD Elongation % min in 2in or 4D
Min Max Min Max
1100-H14 .009-.012 16.0 21.0 14.0 1
.013-.019 16.0 21.0 14.0 2
.020-.031 16.0 21.0 14.0 3
.032-.050 16.0 21.0 14.0 4
.051-.113 16.0 21.0 14.0 5
.114-.499 16.0 21.0 14.0 6
.500-1.00 16.0 21.0 14.0 10
3003-H14 .009-.012 20.0 26.0 17.0 1
.013-.019 20.0 26.0 17.0 2
.020-.031 20.0 26.0 17.0 3
.032-.050 20.0 26.0 17.0 4
.051-.113 20.0 26.0 17.0 5
.114-.161 20.0 26.0 17.0 6
.162-.249 20.0 26.0 17.0 7
.250-.499 20.0 26.0 17.0 8
.500-1.00 20.0 26.0 17.0 10
3105-H14 .013-.019 22.0 29.0 18.0 1
.020-.031 22.0 29.0 18.0 1
.032-.050 22.0 29.0 18.0 2
.051-.080 22.0 29.0 18.0 2
5052-H32 .017-.019 31.0 38.0 23.0 4
.020-.050 31.0 38.0 23.0 5
.051-.113 31.0 38.0 23.0 7
.114-.249 31.0 38.0 23.0 9
.250-.499 31.0 38.0 23.0 11
.500-2.00 31.0 38.0 23.0 12
5052-H34 .009-.019 34.0 41.0 26.0 3
.020-.050 34.0 41.0 26.0 4
.051-.113 34.0 41.0 26.0 6
.114-.249 34.0 41.0 26.0 7
.250-1.00 34.0 41.0 26.0 10
5052-H36 .006-.007 37.0 44.0 29.0 2
.008-.031 37.0 44.0 29.0 3
.032-.162 37.0 44.0 29.0 4
5052-H38 .006-.007 39.0 32.0 2
.008-.031 39.0 32.0 3
.032-.128 39.0 32.0 4
5083-H116 .063-.499 44.0 31.0 10
.500-1.25 44.0 31.0 12
1.251-1.500 44.0 31.0 12
1.501-3.00 41.0 29.0 12
5086-H32 .020-.050 40.0 47.0 28.0 6
.051-.249 40.0 47.0 28.0 8
.250-2.00 40.0 47.0 28.0 12
5086-H116 .063-.249 40.0 28.0 8
.250-.499 40.0 28.0 10
.500-1.25 40.0 28.0 10
1.251-2.00 40.0 28.0 10
5454-O .020-.031 31.0 41.0 12.0 12
.032-.050 31.0 41.0 12.0 14
.051-.113 31.0 41.0 12.0 16
.114-3.00 31.0 41.0 12.0 18
5454-H32 .020-.050 36.0 44.0 26.0 5
.051-.249 36.0 44.0 26.0 8
.250-2.00 36.0 44.0 26.0 12
5454-H34 .020-.050 39.0 47.0 29.0 4
.051-.161 39.0 47.0 29.0 6
.162-.249 39.0 47.0 29.0 7
.250-1.00 39.0 47.0 29.0 10
6061-T6 .006-.007 42.0 35.0 4
.008-.009 42.0 35.0 6
.010-.020 42.0 35.0 8
.021-.249 42.0 35.0 10
6061-T651 .250-.499 42.0 35.0 10
.500-1.00 42.0 35.0 9
1.001-2.00 42.0 35.0 8
2.001-4.00 42.0 35.0 6
4.001-6.00 42.0 35.0 6

Aluminum Chemical Composition

per The Aluminum Association, Inc.

GradeSiFeCuMnMgCrNiZiTi
1100.095 Si + Fe.05-.20.050.10
30030.600.70.05-.201.0-1.50.10
50520.250.400.100.102.2-2.8.15-.350.10
50830.400.400.10.40-1.04.0-4.9.05-.250.250.15
50860.400.500.10.20-.73.5-4.5.05-.250.250.15
54540.250.400.10.50-1.02.4-3.0.05-.200.250.20
6061.40-.800.70.15-.400.15.80-1.2.04-.350.250.15