Engineering question.........incoming!
Now, my tiny little non-engineering mind thinks, "Gee, there's a lot of important stuff hanging offa this here bolt!" :eek:
Why not grade 8 bolts here and in some other places that "seem" structurally important. Can't just be cost savings. Chevy would never do that on a Corvette would it? ;)
Okay engineers, give me the full treatment. :crazy:
:D
Why not grade 8 bolts here and in some other places that "seem" structurally important. Can't just be cost savings. Chevy would never do that on a Corvette would it?
The task of GM engineers was to figure out the least expensive component that could be used in an application safely, and corporate liability for owner safety was not taken lightly. Paying more for a Grade 8 fastener because it was "safer" would be overkill, and GM would never run up the manufacturing cost without good cause.
Because of the relatively close lateral clearances, the loads on the bolt are taken primarily in shear, i.e. the edges of the hole are trying to cut the bolt perpendicular to its length. There are no significant bending stresses to consider.
I don't know the maximum loads that this bolt could see, but it is, what, a 9/16" or 1/2" diameter bolt? That means the cross-sectional area is about 0.2 square inches. Assuming an ultimate shear strength of 50 ksi for a Grade 5 bolt (heck, I don't know, you engineers speak up :D ), that calculates out to about 10,000 pounds maximum load before failure.
Considering they probably used a safety factor of about 5, that means they were actually designing for loads around 2,000 pounds at the fastener. Actual side loads at the wheel would be less because of the moment lever of the trailing arm, but I doubt you could get enough friction between the road surface and the tire to come close to overstressing that bolt.
Fatigue stress was generally of greater concern, but in this application, the number of cycles was probably nowhere even close to those of, say, a connecting rod bolt.
Duke








