Determine the load on a single bushing from the actual reaction force, support configuration, and impact factor. Select a reference material to automatically verify if the design pressure (p) and PV parameters are within standard engineering guidelines.
Note: Vehicle GVM (e.g., 80 tonnes) is not the load on one bushing. Enter the actual reaction force at the pivot (derived from structural analysis), then let the tool distribute it according to the bearing arrangement.
1 · Inputs & Material Selection
Measured/computed reaction, not vehicle GVM.
Select an alloy to compare computed results against typical allowable limits (assumes lubricated conditions).
Integer. Assumes equal load sharing.
Integer. Assumes equal load sharing.
Integer. e.g., 2 for a trunnion with two bearing eyes.
Typical 1.5–2.5 for haul-truck shock.
mm — for bearing pressure computation.
mm — effective load-bearing length.
degrees — for surface velocity / PV limits.
cycles per minute.
% of R on side A (remaining percentage on side B).
2 · Results & Verification
Notice: Please ensure Bore diameter (D) and Bushing length (L) are greater than 0 to compute bearing pressure and PV.
Total supports (nA + nB)
—
supports
Load per support
—
kN
Design load per bushing (incl. impact K)
—
kN
Bearing pressure (p)
—
MPa
Mean surface velocity (v)
—
m/s
PV value
—
MPa·m/s
Model:
Load per support = R / (nA + nB) [or R·sA/nA and R·(1−sA)/nB if asymmetric]
Load per bushing = (Load per support) / (bushings per support)
Design load per bushing = Load per bushing × K
p = Peak Design load / (D × L) [projected area] → MPa
vmean = (2/π)·(D/2)·(2π·f·α) , with f in Hz, α in rad → m/s
PV = p × vmean → MPa·m/s
For Engineering Reference Only: This tool provides a preliminary distribution of the supplied reaction force and indicative pressure/PV calculations. The material reference limits assume standard lubricated conditions and moderate environmental factors. Final bushing material selection, dimensioning, and fitness for service shall be verified by a qualified engineer against the complete duty cycle — including static/dynamic limits, oscillation angles, shaft surface hardness, lubrication regimens, clearance, and fatigue loads.