Taz99
Aerospace
- May 18, 2011
- 21
Hi All,
I usually work on Aerospace projects but have ended up sizing a new Stand Off Clamp design and wanted to run a few things past the group.
I have been advised by the customer of an pipeline operating pressure that they wish to be able to claim, they have advised that we should apply a 1.5 factor to this pressure and test the clamp at this pressure (and this seems to match what the other existing clamps claim to be tested to). However, at least in Aerospace, sometimes there are additional knock down factors we would apply in the analysis but not when doing the final test, one being an additional 1.15 factor on the bolt loads. For this case my two main allowables are bolt strength and material strength is anyone aware of additional safety factors or knockdowns that need to be applied? I have a copy of ASME B31.3-2004 but I am not convinced if the requirements are applicable to a stand off clamp design.
Next question, I have identified a 190 ksi 1/2 inch diameter bolt with 27000 lb axial ultimate strength to use. The customer would like to use a A194 Grade 2H heavy hex nut, the A194 spec Table 3 gives the proof load of 24830 lb but nowhere states the ultimate strength of the nut which should be higher than the proof strength. My customer tells me that they don't know the ultimate strength. There are calculations to determine the thread strength but a published value removes the chance of calculation error. Is anyone able to point me to published values, my Google searches have not turned up anything so far?
Thanks
I usually work on Aerospace projects but have ended up sizing a new Stand Off Clamp design and wanted to run a few things past the group.
I have been advised by the customer of an pipeline operating pressure that they wish to be able to claim, they have advised that we should apply a 1.5 factor to this pressure and test the clamp at this pressure (and this seems to match what the other existing clamps claim to be tested to). However, at least in Aerospace, sometimes there are additional knock down factors we would apply in the analysis but not when doing the final test, one being an additional 1.15 factor on the bolt loads. For this case my two main allowables are bolt strength and material strength is anyone aware of additional safety factors or knockdowns that need to be applied? I have a copy of ASME B31.3-2004 but I am not convinced if the requirements are applicable to a stand off clamp design.
Next question, I have identified a 190 ksi 1/2 inch diameter bolt with 27000 lb axial ultimate strength to use. The customer would like to use a A194 Grade 2H heavy hex nut, the A194 spec Table 3 gives the proof load of 24830 lb but nowhere states the ultimate strength of the nut which should be higher than the proof strength. My customer tells me that they don't know the ultimate strength. There are calculations to determine the thread strength but a published value removes the chance of calculation error. Is anyone able to point me to published values, my Google searches have not turned up anything so far?
Thanks