Heat treatment of friction stir welded 7X50 aluminum
AssigneeThe United States of America as represented by the National Aeronautics and Space Administration
InventorsGeorge E. Petter, John D. Figert, Daniel J. Rybicki, Timothy H. Burns
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Abstract
A method for treating alloy before and after friction stir welding, the method comprising the following steps. First solution heat treating a multiplicity of aluminum-zinc alloy engineered components for a first time period at a first temperature. First air cooling the components in ambient air at room temperature until the components are cooled to room temperature. Friction stir welding the components to form an assembly. Second solution heat treating the assembly for a second time period at a second temperature. Additional steps and embodiments are considered.
Claims28
A method for treating alloy before and after friction stir welding, the method comprising the steps of:
- first solution heat treating a multiplicity of 7X50 alloy engineered components for a first time period at a first temperature;
- first air cooling the components in ambient air at room temperature until the components are cooled to room temperature;
- friction stir welding the components to form an assembly;
- and
- second solution heat treating the assembly for a second time period at a second temperature.
A method for treating aluminum alloy before and after friction stir welding, the method comprising the steps of:
- first solution heat treating a multiplicity of 7X50 aluminum alloy engineered components for a first time period from about 60 minutes to about 90 minutes at a first temperature from about 880 degrees F. to about 900 degrees F.;
- first air cooling the multiplicity of 7X50 aluminum alloy engineered components in ambient air at room temperature until the multiplicity of 7X50 aluminum alloy engineered components are cooled to room temperature;
- friction stir welding the multiplicity of 7X50 aluminum alloy engineered components to form an assembly;
- second solution heat treating the assembly for a second time period from about 5 minutes to about 20 minutes at a second temperature from about 880 degrees F. to about 900 degrees F.;
- quenching the assembly in a water bath at a third temperature from about 50 degrees F. to about 125 degrees F. wherein the quenching step is initialized no later than about 10 seconds after completion of the second solution heat treating step;
- stabilizing the assembly in ambient air at room temperature for a third time period of at least about 4 hours;
- first aging the assembly for a fourth time period from about 3 hours to about 6 hours at a fourth temperature from about 240 degrees F. to about 260 degrees F.;
- and
- second aging the assembly for a fifth time period from about 24 hours to about 30 hours at a fifth temperature from about 315 degrees F. to about 335 degrees F.
A method for treating aluminum alloy before and after friction stir welding, the method comprising the steps of:
- first solution heat treating a multiplicity of 7X50 aluminum alloy engineered components having a thickness from about 0.25 inches to about 0.50 inches for a first time period of about 60 minutes at a first temperature of about 890 degrees F.;
- first air cooling the multiplicity of 7X50 aluminum alloy engineered components in ambient air at room temperature until the multiplicity of 7X50 aluminum alloy engineered components are cooled to room temperature;
- friction stir welding the multiplicity of 7X50 aluminum alloy engineered components to form an assembly;
- second solution heat treating the assembly for a second time period of about 10 minutes at a second temperature of about 890 degrees F.;
- quenching the assembly in water bath at a third temperature from about 85 degrees F. to about 100 degrees F. wherein the quenching step is initialized no later than about 10 seconds after completion of the second solution heat treating step;
- stabilizing the assembly in ambient air at room temperature for a third time period of at least about 96 hours;
- first aging the assembly for a fourth time period of about 5 hours at a fourth temperature of about 250 degrees F.;
- and
- second aging the assembly for a fifth time period of about 27 hours at a fifth temperature of about 325 degrees F.
Dependencies are inferred from the claim text.