rollingcloud
Aerospace
- Aug 9, 2022
- 172
The new supplier stated that the thread of the nut is chipping out during the first removal cycle after baking (image attached) and the nut is getting stuck after 3-4 cycles of room temperature torque test.
.190-32 UNJF Nut material: A286, hardness 24- 37 HRC, 130 ksi tensile strength. Dry film lubricated.
Actual measured hardness: 40 - 43 HRC. I believe the crimping process would increase the hardness?
Test bolt material: Incol 718, hardness 36 HRC min, min of 180 ksi tensile strength. Actual hardness: 45-46 HRC
Nut-bolt assembly is heated to 850° F for 6 hours for testing.
I checked the reported thread dimensions, no deviation from the standard.
Did they over-crimp the nut? How do manufacturers typically perform the crimping? I feel it might be tricky to get it right. I attempted to screw the nut (we have some good parts left in house) onto the bolt by hand, but when it reached the deformed thread area, it was far too tight without a tool.
.190-32 UNJF Nut material: A286, hardness 24- 37 HRC, 130 ksi tensile strength. Dry film lubricated.
Actual measured hardness: 40 - 43 HRC. I believe the crimping process would increase the hardness?
Test bolt material: Incol 718, hardness 36 HRC min, min of 180 ksi tensile strength. Actual hardness: 45-46 HRC
Nut-bolt assembly is heated to 850° F for 6 hours for testing.
I checked the reported thread dimensions, no deviation from the standard.
Did they over-crimp the nut? How do manufacturers typically perform the crimping? I feel it might be tricky to get it right. I attempted to screw the nut (we have some good parts left in house) onto the bolt by hand, but when it reached the deformed thread area, it was far too tight without a tool.