Strut Rods:
I was rebuilding my rear suspension this summer. Upon removing and inspecting the rear strutrods I found a problem. The shank that holds the rubber bushings in place had a nominal diameter of 18mm, however on one of the rods from my car I measured 10 mm diameter
. This was a no-no in my book
. So the day I found this I started designing new strutrods. Basically made a quick CAD model, structural analysis, cost analysis, and a bill of materials. I ended up using the following
Hexrod:
Rockwell Hardness - C39,
Tensile Yield Strength - 163ksi
Bolts:
Thread - 18mmX2.5mm
Class - 12.9
Rockwell Hardness - C39
Tensile Yield Strength - 174ksi
The Bolts and the hex rod where cut at a 45 degree angle to take advantage of the maximum in plane shear stress. Once I cut these I welded them together using mig spray arc transfer. I really wanted to do a tig root pass, but I did not have the correct electrode and filler.
I incorporated three nut locking features. Just as a comparison military aircraft applications only require 2 locking features.
1) Threads themselves
2) Nylock nuts
3) Cotterpins
I was rebuilding my rear suspension this summer. Upon removing and inspecting the rear strutrods I found a problem. The shank that holds the rubber bushings in place had a nominal diameter of 18mm, however on one of the rods from my car I measured 10 mm diameter
. This was a no-no in my book
. So the day I found this I started designing new strutrods. Basically made a quick CAD model, structural analysis, cost analysis, and a bill of materials. I ended up using the followingHexrod:
Rockwell Hardness - C39,
Tensile Yield Strength - 163ksi
Bolts:
Thread - 18mmX2.5mm
Class - 12.9
Rockwell Hardness - C39
Tensile Yield Strength - 174ksi
The Bolts and the hex rod where cut at a 45 degree angle to take advantage of the maximum in plane shear stress. Once I cut these I welded them together using mig spray arc transfer. I really wanted to do a tig root pass, but I did not have the correct electrode and filler.
I incorporated three nut locking features. Just as a comparison military aircraft applications only require 2 locking features.
1) Threads themselves
2) Nylock nuts
3) Cotterpins
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