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Master Bond adhesives
Aluminum 4032-T6
Categories: Metal; Nonferrous Metal; Aluminum Alloy; 4000 Series Aluminum Alloy

Material Notes: Information provided by Alcoa and the references. General 4032 characteristics and uses: Good machinability and drilling characteristics when using single point or multi-spindle screw machines. Excellent surface finish using polycrystalline or carbide tooling. Superior wear resistance, eliminated the need for hard coat anodizing. High strength, low thermal expansion.

Uses: Master brake cylinders, transmission valves, copier parts, bushings for rack and pinion steering systems, sound recording devices, bearings and hydraulic applications, forged pistons.

Data points with the AA note have been provided by the Aluminum Association, Inc. and are NOT FOR DESIGN.

Composition Notes:
Composition information provided by the Aluminum Association and is not for design.

Key Words: UNS A94032; Aluminium 4032-T6; AA4032-T6; Al4032-T6
Vendors:
Available Properties
  • Density, AA; Typical
  • Hardness, Brinell, AA; Typical; 500 g load; 10 mm ball
  • Hardness, Knoop, Converted from Brinell Hardness Value
  • Hardness, Rockwell A, Converted from Brinell Hardness Value
  • Hardness, Rockwell B, Converted from Brinell Hardness Value
  • Hardness, Vickers, Converted from Brinell Hardness Value
  • Tensile Strength, Ultimate, AA; Typical
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Ultimate
  • Tensile Strength, Yield, AA; Typical
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Tensile Strength, Yield
  • Tensile Strength, Yield
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  • Tensile Strength, Yield
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break
  • Elongation at Break, AA; Typical
  • Rupture Strength
  • Rupture Strength
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  • Rupture Strength
  • Modulus of Elasticity, AA; Typical; Average of tension and compression. Compression modulus is about 2% greater than tensile modulus.
  • Poissons Ratio, Estimated from trends in similar Al alloys.
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
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  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
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  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength
  • Fatigue Strength, completely reversed stress; RR Moore machine/specimen
  • Machinability, 0-100 Scale of Aluminum Alloys
  • Shear Modulus
  • Shear Strength, AA; Typical
  • Electrical Resistivity, AA; Typical
  • CTE, linear
  • CTE, linear, AA; Typical; average over range
  • CTE, linear
  • CTE, linear
  • Specific Heat Capacity, Estimated from trends in similar Al alloys.
  • Thermal Conductivity, AA; Typical at 77°F
  • Melting Point, AA; Typical range based on typical composition for wrought products >= 1/4 in. thickness. Eutectic melting is not eliminated by homogenization.
  • Solidus, AA; Typical
  • Liquidus, AA; Typical
  • Annealing Temperature, 2 to 3 hr at temperature then furnace cooled to 500°F at 50°F per hour max
  • Solution Temperature, Hold 4 min at temperature then quench in cold water; for heavy or complicated forgings, quench in water at 150 to 212°F
  • Aging Temperature, 8 to 12 hr at temperature
  • Aluminum, Al, As remainder
  • Chromium, Cr
  • Copper, Cu
  • Iron, Fe
  • Magnesium, Mg
  • Nickel, Ni
  • Other, each
  • Other, total
  • Silicon, Si
  • Zinc, Zn
  
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