Historicalarchived
F-35 Composite Edge of Part Machining
National Center for Defense Manufacturing & Machining
Material: Composite Wing Skin Material Conventional Machining Method: Tool life lasting 9 liner feet at one-third the total material thickness Required a total of 24 tools per wing skin Excessive delamination of the composite material System Solution: Increased cutting distance more than 6x (from 9 to 57 linear feet) at full material thickness Reduced number of tools per wing skin from 24 to 2 Reduced programming time and increased productivity while reducing scrap Cost Savings = $80K per aircraft with an estimated savings/cost avoidance of $222.6M over the projected build of 2,783 F-35 aircraft
Provenance
- Original
- https://dodtechmatch.com/dod/techad/view.aspx?id=10047
- Archived copy
- Wayback Machine snapshot
This record was recovered from a public web archive of dodtechmatch.com and is preserved for historical reference. It may be outdated. Not affiliated with the U.S. Department of Defense. Contact details from the original listing have been withheld.