Analytical and experimental studies were performed to investigate the
effect of gear rim thickness on crack propagation life. The FRANC (FRa
cture ANalysis Code) computer program was used to simulate crack propa
gation. The FRANC program used principles of linear elastic fracture m
echanics, finite element modeling, and a unique re-meshing scheme to d
etermine crack tip stress distributions, estimate stress intensity fac
tors, and model crack propagation. Various fatigue crack growth models
were used to estimate crack propagation life based on the calculated
stress intensity factors. Experimental tests were performed in a gear
fatigue rig to validate predicted crack propagation results. Test gear
s were installed with special crack propagation gages in the tooth fil
let region to measure bending fatigue crack growth. Good correlation b
etween predicted and measured crack growth was achieved when the fatig
ue crack closure concept was introduced into the analysis. As the gear
rim thickness decreased, the compressive cyclic stress in the gear to
oth fillet region increased. This retarded crack growth and increased
the number of crack propagation cycles to failure.