eE jeremy;201267 wrote: Al should only be used on cosmetic applications in my opinion, fairing bolts, gauge cluster mounting, fuel cap screws, etc, nothing involving wheels, drivetrain, brakes, or suspension...
+1000000000000!!!
Ti is about 1/2 the density (~0.16 lb/in^3) of steel and its strength/weight is higher that steel (density ~ 0.283 lb/in^3)
Al is about 1/3 the density (~0.102 lb/in^3) of steel and its strength/weight is higher than steel
(strength/weight is the ratio of the strength per unit weight of a material)
A high strength steel (i.e. Ph13-8, which is actually a stainless) fastener has a shear strength of about 125,000 psi
A standard Ti fastener has a shear strength of about 95,000 psi
Most higher strength Aluminums I deal with have shear allowables of around 40,000 psi....not even close to steel!
We don't use aluminum fasteners in aircraft, unless they are rivets and we are getting away from rivets.