irfan08
Aerospace
- Jan 28, 2008
- 69
We manufacture pressure vessels, DFMA reports following critical parts,
1. Neck
2. Top & Bottom Head
3. Shell
4. Stud
I would like to have a good understanding on how to implement tolerance stackup using data from spreadsheet. For starter we are only concerned in 1-D (Height Only) analysis for POC.
I have seen the excel file from KENAT, its just I am new to statistical tolerancing or even tolerancing, I need a basic work around which is simple and easy.
Any help will be appreciated.
Thanks
1. Neck
2. Top & Bottom Head
3. Shell
4. Stud
I would like to have a good understanding on how to implement tolerance stackup using data from spreadsheet. For starter we are only concerned in 1-D (Height Only) analysis for POC.
I have seen the excel file from KENAT, its just I am new to statistical tolerancing or even tolerancing, I need a basic work around which is simple and easy.
Any help will be appreciated.
Thanks