Help me understand how bolts take less load than members

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In summary, bolts typically take less load than structural members due to their role as fasteners that connect components rather than bear loads themselves. The load distribution in a structure often results in the members, such as beams or columns, bearing the majority of the forces, while bolts primarily serve to maintain the integrity of connections. Factors like shear and tensile forces acting on the bolts, along with their material properties and design specifications, further limit their load-bearing capacity compared to the larger structural elements they connect.
  • #1
davidwinth
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TL;DR Summary
A bolt holds two members in compression, and is said to take less of the external load even when the numbers say different.
Hello,

I am studying through a machine design book and ran across this confusing statement which summarizes the results of an example problem. The problem has a bolt and nut that together hold two members in compression. The stiffness ratio is given as $$K_m = 6K_b$$. The bolt is preloaded with $$P_i = 1100 lbs$$ and the members have an external load (that tries to pull them apart) of $$F_e = 1200 lbs$$. The example then finds the resultant compression in the members and the tension in the bolts. The tension in the bolt is 1271.42 lbs and the compression in the members is 71.42 lbs. Then the book gives this statement: "In this problem, it can be seen that the proportion of the load shared by the bolt is very small because the stiffness of the bolt is low when compared to the members."

How is 1271.42 less than 71.42? Thanks.
 
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  • #2
I suspect you are missing something, and have also left it out of your question.

I assume the bolt is elastic, and provides a clamping force that is multiplied by static friction between the members.

A diagram would help.
Please provide a reference to the book title, author, edition, and page number.
 
  • #3
The book is called, "The Machine Design Problem Solver" page 215, and there is no consideration of friction mentioned at all. Of course both the bolt and the members are considered as elastic (hence the reference to their stiffnesses). I have not left out anything that I can see. The entire example is only two equations which give the results I showed above. As for a picture, it looks much like the one below except the two members are of equal thickness and there are external forces pulling the members apart. I typed an exact quote of the summarizing the findings. Thank you.

1710361189992.png
 
  • #4
I believe it is all to do with understanding the implied direction of the applied forces. Here is the problem...

Problem 4-5
Consider a bolted connection shown in Figure 1, in which the stiffness coefficients are given as Km ≈ 6 Kb. If the connection is preloaded with Pi = 1100 lbs. and the members are externally loaded with Fe = 1200 lbs., find the resultant compression of the machine parts and the tension of the bolt.
bolt1.jpg

bolt2.jpg

In this problem, it can be seen that the proportion of the load shared by the bolt is very small because the stiffness of the bolt is low when compared to the members. The result is that the machine parts are still in compression even after applying an external load greater than the preload. Therefore, there is no separation of the parts.
 
  • #5
davidwinth said:
"In this problem, it can be seen that the proportion of the load shared by the bolt is very small because the stiffness of the bolt is low when compared to the members."
The load shared by the bolt is:
$$\frac{K_b f_e}{K_b+K_m} = 171.43\text{ lb}$$
The load shared by the members:
$$\frac{K_m f_e}{K_b+K_m} = 1028.57\text{ lb}$$
Thus:
$$171.43\text{ lb} < 1028.57\text{ lb}$$
 
  • #6
I was also confused by this. Here is a related thread.
Post #6 from that thread contains the insight that made it click for me.

I think I finally got an intuition about why that happens.
When the external separation force is applied, the tension force on the bolt must increase but simultaneously, the force the clamped parts were doing on the bolt diminishes. The net effect on the bolt depends on the stiffness ratio of the joint.
In the case of the clamped parts being WAY stiffer than the bolt, it is possible to increase the external force until it surpasses the preload so it causes gapping without almost affecting the bolt. At the instant where gapping occurs, all the external force travels exclusively through the bolt but before that, the bolt did not see a significant increment in tension.

1701614468775.png
 

FAQ: Help me understand how bolts take less load than members

1. Why do bolts take less load than structural members?

Bolts are typically designed to connect structural members, but they are not as strong as the members themselves. The load-bearing capacity of a bolt is limited by its material properties, cross-sectional area, and the way it is installed. In contrast, structural members like beams or columns are designed to handle larger loads due to their geometry and material strength, which allows them to distribute loads more effectively.

2. What factors influence the load capacity of a bolt?

The load capacity of a bolt is influenced by several factors, including its diameter, grade (material strength), thread type, and the method of installation (such as tensioning and the use of washers). Additionally, the type of load (shear, tensile, or combined) and the conditions of the joint (such as friction and bearing) also play significant roles in determining how much load a bolt can safely handle.

3. How does the connection design affect the load distribution between bolts and members?

The design of the connection significantly affects how loads are distributed between bolts and structural members. If the connection is designed properly, the load will be shared between the bolts and the members, but if the connection is not adequately designed, the bolts may experience higher loads than they can handle. Factors such as the number of bolts used, their arrangement, and the type of load (static or dynamic) can all impact how effectively the load is distributed.

4. Can bolts fail under load, and what are the common failure modes?

Yes, bolts can fail under load, and common failure modes include shear failure, tensile failure, and fatigue failure. Shear failure occurs when the bolt is unable to withstand the shear forces acting on it, while tensile failure happens when the bolt is stretched beyond its tensile strength. Fatigue failure can occur over time due to repeated loading and unloading cycles, leading to cracks and eventual failure of the bolt.

5. How can engineers ensure that bolts are adequately sized for their applications?

Engineers can ensure that bolts are adequately sized by conducting thorough calculations based on the expected loads, selecting the appropriate bolt grade, and considering factors such as safety margins and environmental conditions. Additionally, using proper installation techniques and following industry standards and guidelines will help ensure that bolts can handle the loads they will encounter in service.

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