Abstract: A component for a machine is disclosed. The component may include an interior frame, a protruding member extending from the interior frame, and a carbon fiber wrapped over the interior frame and around the protruding member. A method of manufacturing a component for a machine is also disclosed. The method may include supplying an interior frame with a protruding member extending from the interior frame. The method may further include wrapping a carbon fiber around the interior frame and the protruding member, and curing the carbon fiber to the interior frame.

Abstract: Problems associated with soot production and coking build up in nozzle spray passages are addressed by plating a bore wall of an injector body tip piece with a primarily nickel coating using an electroless plating technique. The coating has an average thickness that is at least one order of magnitude smaller than an average diameter of the bore.

Abstract: A process for building up a leading edge of a machine component such as a leading edge of a turbine blade for a turbocharger includes forming a molten pool along the edge of the machine component, feeding a filler material in a solid state into the molten pool and melting the filler material via heat transfer between the molten pool and the filler material. A solid layer may be formed along the leading edge by cooling the molten pool. The process is applicable to remanufacturing damaged machine components having a plurality of blades with relatively thin leading edges.

Abstract: A process for building up a leading edge of a machine component such as a leading edge of a turbine blade for a turbocharger includes forming a molten pool along the edge of the machine component, feeding a filler material in a solid state into the molten pool and melting the filler material via heat transfer between the molten pool and the filler material. A solid layer may be formed along the leading edge by cooling the molten pool. The process is applicable to remanufacturing damaged machine components having a plurality of blades with relatively thin leading edges.

Abstract: While ceramic materials possess properties that make them suitable for use in fuel system components, they tend to be susceptible to failure when exposed to tensile stresses. The retention system described herein helps to reduce the tensile stresses experienced by a retained member by providing a retained member with an engagement structure, a multi-piece retention ring that engages the engagement structure, a resilient member coupled to the retention ring, and a retainer coupled around at least a portion of the retention ring and resilient member and spaced apart from the retention ring and/or resilient member by a gap. The retained member, retention ring, resilient member, and retainer are configured so that the retention ring is moveable in an axial direction relative to the retained member and so that the movement of the retention ring acts to expand the resilient member against the bias provided by the resilient member.