Tie Rod Stress Analysis - Critical locations

AI Thread Summary
Modifying the length of a tie rod body may not significantly impact its structural integrity if the cut and weld are executed properly. The critical stress points are typically at the clevis and end rod, but if the rod is shortened and welded with a homogeneous material, it can maintain its ability to transmit forces effectively. A shorter tie rod is also less susceptible to buckling. Proper welding should mitigate concerns about fatigue, provided there are no cracks. Additional details about the tie rod's geometry and loading patterns could further clarify the analysis.
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I'm faced with a problem where I need to cut the length of the rod body on a tie rod, however, I need to prove that this modification will not affect the entire structure seeing as how the critical points of stress on a tie rod exist at the clevis and end rod. How would I go about proving that these are in fact the critical locations??
 
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Hello,

I am not a tie rod specialist, so I do not know the specific load pattern for such piece of equipment (you are talking about a tie rod in a car steering system right?), but it appears to me that a tie rod, although they might come in a lot a shape, can be viewed as a cylindrical beam used to transmit a compressive or tensile force ( along its axis). So, if you intend to cut that cylinder and fully weld it back together with a homogeneous material, you have the same area to transmit the forces, therefor the same static stress. It should withstand the same load for the same lifetime. Hence, you don't have to prove that the clevis and the rod end are critical.

Being shorter, it will be less prone to buckling. If the welding is done properly (no cracks), there should not be a problem with fatigue.

hope I understand your problem correctly and I could help. If not, can you give us a little bit more information on the tie rod geometry and the loading pattern.
 
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