brin
Aerospace
- Mar 12, 2000
- 122
We have a drawing for an aircraft part that uses a 7075 hand forging. The drawing requires it to be rough machined, solution heat treated, quenched, held in the refrigerated state before final machining, and aged to the T6 condtion. This is different from most drawings which require final machining in the T6 condition.
Can anyone shed some insight into why a part would be final machined in the as quenched condition rather than -T6 condition? I understand that the T6 condition is easier to machine.
Can anyone shed some insight into why a part would be final machined in the as quenched condition rather than -T6 condition? I understand that the T6 condition is easier to machine.