na = F·S/(0.6·Rm·A0); nl = F·S/(1.5·Rm·d0·tmin)
Both allowable stresses come from the same tensile strength and safety factor: τallow ≈ 0.6·Rm/S for shear, σl,allow ≈ 1.5·Rm/S for bearing.
Both allowable stresses come from the same tensile strength and safety factor: τallow ≈ 0.6·Rm/S for shear, σl,allow ≈ 1.5·Rm/S for bearing.
Select a target and calculate.
Both allowable stresses come from the same tensile strength and safety factor: τallow ≈ 0.6·Rm/S for shear, σl,allow ≈ 1.5·Rm/S for bearing.
20,000 N, a 10 mm rivet diameter, 8 mm governing plate thickness, Rm = 400 MPa and S = 1.5 give na = 2 (shear) and nl = 1 (bearing); 2 rivets govern.
Single-shear joint with even load sharing across all rivets; the rivet count actually chosen is the larger of the two values, rounded up to a whole number.
This calculator finds the required rivet count of a single-shear joint against both shear and bearing failure; the larger of the two values always governs the design.
From the classical allowable stresses τa,allow ≈ 0.6·Rm/S for shear and σl,allow ≈ 1.5·Rm/S for bearing (Rm tensile strength, S safety factor), two independent minimum rivet counts follow: na = F/(τa,allow·A0) from shear failure and nl = F/(σl,allow·d0·tmin) from bearing failure. Both are rounded up to a whole number; the rivet count actually chosen is the larger of the two.
This is like sizing a component that can fail in two different ways: the required design is calculated separately for each failure mode, then whichever imposes the stricter requirement is chosen — similar to a beam checked against both bending strength and deflection and sized by the stricter criterion.
na = F·S/(0.6·Rm·A0); nl = F·S/(1.5·Rm·d0·tmin)
na = F·S/(0.6·Rm·A0)nl = F·S/(1.5·Rm·d0·tmin)governs: n = max(na, nl)| Symbol / input | Meaning |
|---|---|
| Rivet count against shear na | Calculated, rounded-up rivet count from shear failure. |
| Rivet count against bearing nl | Calculated, rounded-up rivet count from bearing failure. |
| Transverse load F | Force to be transmitted, acting perpendicular to the rivet axis. |
| Rivet hole diameter d0 | Diameter of the formed rivet. |
| Governing plate thickness tmin | Smallest sum of plate thicknesses acting in the same direction. |
| Tensile strength Rm | Tensile strength of the rivet material (for shear) or component material (for bearing); for steel rivets after forming, about 400 MPa. |
| Safety factor S | Chosen safety factor against tensile strength. |
Load F, rivet diameter d0, governing plate thickness tmin, tensile strength Rm and safety factor S jointly determine both rivet counts, since τa,allow and σl,allow both derive from the same Rm and S.
Enter force, diameter, plate thickness, tensile strength and safety factor. The calculator shows both required rivet counts na and nl; always choose the larger for the design, rounded up to a whole number.
20,000 N, a 10 mm rivet diameter, 8 mm governing plate thickness, Rm = 400 MPa (formed steel rivets) and S = 1.5 give na = 2 (shear) and nl = 1 (bearing); 2 rivets should be chosen since shear failure governs here.
na exceeding nl shows that shear failure drives the design in this example — increasing plate thickness alone would not reduce rivet count, while a larger rivet diameter or more rivets directly address the shear issue.
Force is given in N, diameter and plate thickness in mm, tensile strength in MPa, and safety factor and rivet counts are dimensionless.
Whether shear or bearing first causes a riveted joint to fail depends on the specific geometry: a large rivet diameter with a thin plate favors bearing failure, a small diameter with a thick plate favors shear failure. Since both failure modes can occur independently and no general rule predicts which becomes critical first, a safe design always requires both checks, choosing the larger of the two resulting rivet counts.
The calculation is used for initial sizing of riveted joints, to quickly estimate how many rivets of a given size a load requires before the final arrangement is checked in detail.
The model applies to a single-shear joint with even load sharing. For double-shear joints, na should be halved accordingly. Edge distances, hole spacing and plate net-section stress are not checked here and need separate verification, as does possible eccentric loading of larger rivet groups.
Common mistake: A common mistake is checking only one failure mode and overlooking the other — depending on geometry, either shear or bearing can govern. It is also easy to skip rounding up the computed result, even though only a whole rivet count makes practical sense.
Always the larger of the two, rounded up to a whole number, since both failure modes can occur independently.
They are classical ratios, established in mechanical engineering practice, between allowable shear or bearing stress and the material's tensile strength Rm.
For the shear check, additionally divide by the number of shear planes; the bearing check stays unchanged.
Edge distances, hole spacing, plate net-section stress and eccentric loading; see the assumptions and limits section.
It depends on load type, material and application; static machine-design loads commonly use values around 1.5 to 2, with higher values for safety-relevant or dynamic applications.