Magnesium ZK60A

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Aging Procedure

Following solution heat treatment (930 F for 2 hours, hot water quench), heat to 300 F for 24 hours.

Applications

Commonly employed in a variety of aircraft applications such as landing gear, brake housings, instrumentation bodies, ribs and spars.

Formability

Best results are obtained by preheating the material to 500 F. Bend radii of twice the material thickness is possible with proper procedures.

Heat Treatability

Solution heat treat at 930 F for 2 hours and quench in warm/ hot water.

Hot Workability

Work at 500 F.

Machinability

Very high machinability rating. As with any magnesium alloy, great care should be taken because this material is flammable. To avoid this potential hazard, positive cuts should be taken, as large chips are less likely to ignite. Flooding with lubricant is also required and good procedure should include constant monitoring of the operation by a machinist equipped with a magnesium fire arresting kit, such as black powder.

Principle Design Features

ZK60A is a heat treatable magnesium alloy used primarily in extruded shapes and forgings. The alloy is generally considered for applications requiring shock and impact resistance and for parts that will be highly stressed.

Weldability

Arc welding is not recommended, however, resistance welding has proven good results.

Known Forms

Billet

Billet

Flat Bar

Flat Bar

Ingot

Ingot

Plate

Plate

Rod

Rod

Round Bar

Round Bar

Sheet

Sheet

Square Bar

Square Bar

Additional Data

Specifications

B107,B91

Chemical Elements

MagnesiumBalance
Remainder Total0.3 max
Zinc4.8 - 6.2
Zirconium0.45 nom

Physical Properties

Density: 0.066lb/in³Density

Electrical Resistivity: 5.7µΩ·cmElectrical Resistivity

Specific Heat: 0.245BTU/lb·°FSpecific Heat

Mechanical Properties

Thermal Conductivity: 5.8333BTU/hr·ft·°FThermal Conductivity

Thermal Expansion: 14.5µin/in·°FThermal Expansion

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