506818
Aerospace
- Jun 5, 2014
- 35
I'm designing a system housed in an enclosure (Peli case style) that will hold 1 psi (0.0069 N/mm^2) pressure with a top panel held in by a number of screws.
The top panel has a surface area of 83607mm^2, therefore, a total force of = 0.0069*83607 = 577N. At present, I have 10 screws holding the part in place (57.7N per screw).
The case is made from polypropylene with M4x0.7 stainless steel screws used to hold the top panel in place. There are mounting holes on the case that I am planning on drilling larger and tapping (5 mm of thread used by screw) to fit the M4 screws. However, I need to ensure that the screws hold the top panel in place without stripping the plastic thread on the case. I'm not worried by the screw, more about the case.
I've found this calculation for internal threads shear force area (imperial-based):Associated calculator:
The values I have come up (metric):
n = 25.4/0.7 = 36.29
Le = 5 mm
Dsmin = 3.838 mm
Enmax = 3.523 mm
As = 0.07102 in^2 = 45.819 mm^2 (not sure if calculator is correct on the website as I get 30.71 mm^2)
Above thread dimensions calculated using:
Then with F = shear strength * shear area
(shear for polypropylene = 0.5* tensile strength = 0.5*31 = 15.5 N/mm^2, data from here:
Therefore, the max force each screw can theoretically handle is:
F = 15.5*45.819 = 710 N
This seems to indicate that I should be fine, but it's all theoretical and would like some idea if I'm on the right path. Am I?
The top panel has a surface area of 83607mm^2, therefore, a total force of = 0.0069*83607 = 577N. At present, I have 10 screws holding the part in place (57.7N per screw).
The case is made from polypropylene with M4x0.7 stainless steel screws used to hold the top panel in place. There are mounting holes on the case that I am planning on drilling larger and tapping (5 mm of thread used by screw) to fit the M4 screws. However, I need to ensure that the screws hold the top panel in place without stripping the plastic thread on the case. I'm not worried by the screw, more about the case.
I've found this calculation for internal threads shear force area (imperial-based):Associated calculator:
The values I have come up (metric):
n = 25.4/0.7 = 36.29
Le = 5 mm
Dsmin = 3.838 mm
Enmax = 3.523 mm
As = 0.07102 in^2 = 45.819 mm^2 (not sure if calculator is correct on the website as I get 30.71 mm^2)
Above thread dimensions calculated using:
Then with F = shear strength * shear area
(shear for polypropylene = 0.5* tensile strength = 0.5*31 = 15.5 N/mm^2, data from here:
Therefore, the max force each screw can theoretically handle is:
F = 15.5*45.819 = 710 N
This seems to indicate that I should be fine, but it's all theoretical and would like some idea if I'm on the right path. Am I?