Abstract: A process for manufacturing polymer/metal disks in a single piece batch size comprises applying a bonding agent to a metallic hub, pressing a polymeric ring over the metallic hub to form a ring/hub assembly, and heating the ring/hub assembly to cause bonding to occur between the polymeric ring and the metallic hub. The bonding agent may either be sprayed or applied directly to the metallic hub. Other methods of application may also be employed, such as dipping of the metallic hub in the bonding agent. The bonding agent is generally an organosilane, although other compounds capable of bonding a polymer to a metallic substrate can be used. The pressing of the polymeric ring over the metallic hub comprises enlarging the polymeric ring and mounting it over the metallic hub. The enlargement of the polymeric ring is typically effectuated either with heat or by stretching.

Abstract: A process for surface hardening a ferrous article such as an aircraft engine rocker lever shaft includes the steps of creating a nitrocarburized oxide layer atop the ferrous core, and subsequently creating a nitrogen enriched case between the oxide layer and the ferrous core. The article is exposed at a first elevated temperature to a mixture of an inert carrier gas, ammonia, carbon dioxide and sulfur dioxide, and thereafter exposed to the carrier gas and ammonia at a second elevated temperature higher than the first temperature. The article formed by the process has a ferrous core covered by a case of nitrogen enriched, institially hardened steel over the core, and a complex nitrocarburized oxide layer atop the case. The complex nitrocarburized oxide layer includes a lower portion comparable to a conventional epsilon nitride or white layer, and an upper porous oxide zone. The upper porous oxide zone is preferably infused with an extreme pressure oil or a liquid polytetrafluoride material.

Abstract: A turbocompound engine having a stratified charge or diesel cycle rotary internal combustion engine, with a first output shaft and a turbine engine with a second output shaft. The first and second output shafts are coupled together so that the shafts rotate in synchronism with each other and provide a rotary output from the turbocompound engine. A valve variably directs air inducted into the engine between the turbine engine and internal combustion engine in dependence upon engine operating conditions.