KirbyWan
Aerospace
- Apr 18, 2008
- 583
Howdy all,
I would like to have the details for and aircraft part laser cut from aluminum sheet stock (.025" thick and .010" thick), but I have a process specification issue. STP 51-310 requires that I do a test with the same alloy, gage, thickness and heat treat to determine the extent of the heat affected zone, and have that HAZ removed in subsequent processing.
What is the size of the HAZ for laser cut thin aluminum? Specifically I'm cutting 7075-T6 .010" thick and .025" thick chem milled (in places) to .012/.014.
Since all of these parts are adhesivly bonded the edge of the sheet does not carry significant load so the HAZ (If it's as small as I think it is) should not make any difference anyway.
Has anyone dealt with this issue before and have suggestions? The spec was last updated in 1996 so what may have been a new process at the time is now old news with no current issues.
Thanks for your help.
-Kirby
Kirby Wilkerson
Remember, first define the problem, then solve it.
I would like to have the details for and aircraft part laser cut from aluminum sheet stock (.025" thick and .010" thick), but I have a process specification issue. STP 51-310 requires that I do a test with the same alloy, gage, thickness and heat treat to determine the extent of the heat affected zone, and have that HAZ removed in subsequent processing.
What is the size of the HAZ for laser cut thin aluminum? Specifically I'm cutting 7075-T6 .010" thick and .025" thick chem milled (in places) to .012/.014.
Since all of these parts are adhesivly bonded the edge of the sheet does not carry significant load so the HAZ (If it's as small as I think it is) should not make any difference anyway.
Has anyone dealt with this issue before and have suggestions? The spec was last updated in 1996 so what may have been a new process at the time is now old news with no current issues.
Thanks for your help.
-Kirby
Kirby Wilkerson
Remember, first define the problem, then solve it.