RicN
Aerospace
- Mar 20, 2007
- 3
Hi,
I am new here as I just found out about the site. I just got a job at Boeing in the Payloads group as a designer working on cabinets, closets.. I got a design assignment making a plenum. It basically a rectangular box made up of honeycomb panels, and my lead said to use the tab and slot joints. I did a quick search on Boeing documents about the subject, and found some about Mortise and Tenon joint, and Rabbett joint. However I haven't found any document that says how loose/tight should the tab/slot be, spacing between the adjacent tab/slot. Before I went to my lead and ask for more specific infos, I wonder if anybody here know anything about it and can offer me some kn
I am new here as I just found out about the site. I just got a job at Boeing in the Payloads group as a designer working on cabinets, closets.. I got a design assignment making a plenum. It basically a rectangular box made up of honeycomb panels, and my lead said to use the tab and slot joints. I did a quick search on Boeing documents about the subject, and found some about Mortise and Tenon joint, and Rabbett joint. However I haven't found any document that says how loose/tight should the tab/slot be, spacing between the adjacent tab/slot. Before I went to my lead and ask for more specific infos, I wonder if anybody here know anything about it and can offer me some kn