CSrac
Aerospace
- Nov 5, 2003
- 18
As an N/C programmer, part of my job is to 5 axis program core details (non-metalic) for aircraft bond assemblies. We use several special cutters and some leave a rough finish which we currently remove with finish passes and sanding. What effect would a fuzzy core finish have on bond strength? We are now designing some pull and NDI test to compare, but I wondered if anyone else has an Idea what finish is necessary. Our spec is very general and only states " Machined fiber fuzz shall not be longer than .10 inches."