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Thread: Bolt Pre load calcs

  1. #1
    Associate Engineer moneytree's Avatar
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    Bolt Pre load calcs

    I have a Stainless Steel bolt being torqued into an Aluminium plate. I can calculate the pre load induced in the bolt when using a torque and the bolt and nut are the same material. BUT I do not have the calculation required for the pre load induced when the 'nut' is a weaker material than the bolt.
    Can anybody help ?

    Thanks.

  2. #2
    tom.howells
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    The strength of bolts loaded in tension can be
    easily determined by the ultimate tensile
    strength. To determine the amount of force
    required to break a bolt, multiply its ultimate
    tensile strength by its tensile stress area, As
    Determining the strength of the threads is more complicated. Since the male threads pull past the
    female threads, or vice-versa, the threads fail in shear and not in tension. Therefore, the stripping
    strength of an assembly depends on the shear strength of the nut and bolt materials.
    To determine the force required to strip the threads, multiply the shear strength by the cross
    sectional area being sheared. The difficulty lies in determining the
    cross sectional area in which the shear will occur. Here are three
    possible scenarios for this type of failure.
    1. The nut material is stronger than the bolt material. In this
    example, the nut threads will shear out the bolt threads. The
    failure will occur at the root of the bolt threads.
    2. The bolt material is stronger than the nut material. In this
    scenario, the bolt threads will shear out the nut threads. The
    failure will occur at the root of the nut threads.
    3. The nut and bolt are the same strength. In this scenario, both
    threads will strip simultaneously. This failure will occur at the
    pitch line.
    The tensile strength of most fasteners is usually specified, whereas
    shear strength is not. In order to avoid shearing the threads, ensure
    that the length of engagement between the internal and external thread is long enough to provide
    adequate cross-sectional thread area.
    Failure scenarios #1 and #3 can typically be avoided by ensuring proper thread engagement. With
    proper engagement, those scenarios would result in a tensile failure of the bolt rather than thread
    stripping.

    Removed Link...
    Last edited by Kelly_Bramble; 07-05-2012 at 07:27 AM.

  3. #3
    Technical Fellow Kelly_Bramble's Avatar
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    Quote Originally Posted by moneytree View Post
    I have a Stainless Steel bolt being torqued into an Aluminium plate. I can calculate the pre load induced in the bolt when using a torque and the bolt and nut are the same material. BUT I do not have the calculation required for the pre load induced when the 'nut' is a weaker material than the bolt.
    Can anybody help ?

    Thanks.
    Use the weaker material in your calculations to determine the pre-load and torque...
    Last edited by Kelly_Bramble; 07-05-2012 at 07:30 AM.

  4. #4
    Technical Fellow Kelly_Bramble's Avatar
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    Here are a few Engineers Edge resources that should be helpfull..

    Bolt Pre-load equation and calculator
    http://www.engineersedge.com/calcula...alculation.htm

    Fastener torque engineering and design resources..
    http://www.engineersedge.com/fastener_thread_menu.shtml

  5. #5
    Associate Engineer moneytree's Avatar
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    Thanks for the answers but this is not quite what I am after. Perhaps I should clarify :-
    Example 1
    M10 StSteel bolt A2 class 70 and Nut A2 class 70 Is torqued to 33 Nm preload in bolt induced is 17 KN.

    Example 2 (My problem)
    M10 StSteel bolt A2 class 70 and Tapped Aluminium Plate. Bolt torqued to 33 Nm preload in bolt ???????

    Although the torque is the same aluminium is softer therefore the preload will be less, but by how much.

    I have attached my standard calcs for similar materials.

    calc1.jpg
    calc2.jpg

  6. #6
    Technical Fellow Kelly_Bramble's Avatar
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    Quote Originally Posted by moneytree View Post
    Thanks for the answers but this is not quite what I am after. Perhaps I should clarify :-
    Example 1
    M10 StSteel bolt A2 class 70 and Nut A2 class 70 Is torqued to 33 Nm preload in bolt induced is 17 KN.

    Example 2 (My problem)
    M10 StSteel bolt A2 class 70 and Tapped Aluminium Plate. Bolt torqued to 33 Nm preload in bolt ???????

    Although the torque is the same aluminium is softer therefore the preload will be less, but by how much.

    I have the attached my standard calcs for similar materials.

    calc1.jpg
    calc2.jpg
    ? Seriously, the pre-load is going to be identical in both components... Are you really looking for the thread shear stress or applied stress/strain on each of the material?

    Is this homework?

  7. #7
    Associate Engineer moneytree's Avatar
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    Thanks kelly.

    Its taken a couple of go's but I now understand.

    p.s. Its not homework.

    p.p.s I havn't had home work since 1981.

    Thanks again.

  8. #8
    Technical Fellow Kelly_Bramble's Avatar
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    moneytree,

    Don't be a stranger around Engineers Edge, bunch of thin-grey hairs hang around here!....

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