markarnold
Mechanical
- Feb 20, 2004
- 9
We manufacture a series of pneumatically driven rack and pinion actuators. When the series was originally designed, the engineer chose 1144 stressproof as the material for both the rack and pinion gear. He also specified flame hardening .030" to .060" deep to 50-55 Rockwell C scale of the tooth flanks. This design has been trouble free for almost 10 years until recently. On our highest volume size we are breaking the teeth of pinion at the root of the teeth. I suspect a heat treat method. We've used the same supplier for several years with no problems. Their claim is there has been no change in material or heat treat. We did find after cutting a pinion gear in half that the hardness extends throughout the tooth and just below the root. Below the root it transitions very quickly to 30-35 Rockwell C. The gears haven't fatigued as we are seeing failures upon initial startup testing at our facility. The supplier's heat treater claims that the 1144 material does not case harden very well and that the heat treat goes much deeper. I am considering change the gear to an 8620 alloy that is case hardened via gas carburization, but I am both concerned about the lower tensile strength and the fact that they had not failed before. I would like some suggestions as to where I should proceed next.