
NAS6605, MS21042-5, Torque - Aircraft engineering | Eng-Tips
2019年3月22日 · NAS6605-14 shear bolts and MS21042-5 self locking nuts are ideal for structure... but be advised, this is 'classic shear' structure. NAS6603-6620 Bolts are intended for primarily cyclic-shear load at 95-SKSI + static torque-tensile loads for structure clamp up with some transient cyclic tension-tension above the static preload.
NAS6605-12 Bolts Bending Stress - Aircraft engineering - Eng-Tips
2009年6月18日 · Hello, I wanted to check what would be bending stress allowable for NAS6605-12 bolts which has only 160 Ksi as Ftu and 95Ksi as Fsu. Please advise if anyone has idea of dealing with same.
oversize bolt for 5/16-24 bolt repair - Aircraft engineering
2009年5月25日 · NAS6603--6620 [NAS6605 = 5/16 Nom] steel NAS6703--6720 [NAS6705 = 5/16 Nom] A286 NAS6803--6820 [NAS6805 = 5/16 Nom] Titanium [may only use with stress engr approval due to 1/2 stiffness of steel & CRES] CAUTION: review fastener specs for appropriate coding [coatings, undrilled or drilled head/shank, OS marking, etc] Regards, Wil Taylor
Torque Settings - Aircraft engineering | Eng-Tips
2001年5月22日 · One thing you need to be aware of regarding the torque setting for any bolt is the application it is being used on: if a seal or gasket is being used, whether the bolt is being torqued with a nut or into an insert (and what the parent material is when an insert is used), etc.
Aircraft engineering | Page 22 | Eng-Tips
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