Torquing Stainless screws into Aluminum

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SUMMARY

This discussion focuses on the proper torque application for stainless steel 4-40 socket head machine screws being torqued into 6061-T6 aluminum threaded holes. Participants emphasize the importance of calculating the pull-out strength of the aluminum threads to avoid over-torquing, which could lead to thread failure. A standard preload of 60% of the lower value between the bolt and thread strength is recommended. Additionally, the shear area must be considered in torque calculations, specifically using the formula 0.5 * π * shear diameter * engagement.

PREREQUISITES
  • Understanding of torque specifications for different materials
  • Knowledge of thread engagement and pull-out strength calculations
  • Familiarity with the properties of 6061-T6 aluminum
  • Experience with using thread-locking compounds like blue thread-locker
NEXT STEPS
  • Research the torque tables specific to stainless steel and aluminum combinations
  • Learn how to calculate pull-out strength for threaded connections
  • Study the effects of lubricants on torque values and thread engagement
  • Explore the mechanics of shear area calculations in fastening applications
USEFUL FOR

Manufacturing engineers, mechanical designers, and anyone involved in fastening applications using stainless steel screws in aluminum materials will benefit from this discussion.

KeninCA
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I'm torquing a stainless steel 4-40 socket head machine screw into a 6061-T6 aluminum threaded hole.

I've located some torque tables that give differing values for different screw materials, but I'm wondering how this applies since I'm going into a threaded hole of a softer material.

We've chosen to use torque values as a manufacturing standard, and I don't want to over-torque what the aluminum threads can handle.

We are using a small amount of blue thread-locker, which may act as a lubricant during torquing.

Does anyone out there have experience in this application?
 
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You need to calcuate the pull-out strength of the aluminum threads. Depending on your thread engagement, it could be the bolt will fail first, or it could be the threads will pull out.

At my work our standard is preload to 60% of whichever is lower. Here's an older thread on thread pullout strengths: https://www.physicsforums.com/showthread.php?t=389146

Keep in mind that the shear area should be considered (0.5 * pi * shear diameter * engagement). I missed that factor of two, note my signature :redface:
 

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