The present disclosure relates to engine camshafts, and more specifically to a lightweight camshaft assembly.
This section provides background information related to the present disclosure which is not necessarily prior art.
An engine camshaft assembly may include a plurality of projections, e.g., lobes and main bearing supports or journals, located on the exterior surface of a hollow tube. During operation of the engine, the camshaft assembly is rotated and the lobes act to open the intake and/or exhaust valves of the engine. The journals provide the bearing surface for the support of the camshaft assembly of the engine. The mass of the camshaft affects the efficiency of an engine and, in the case of motor vehicles, fuel economy. Therefore, engine designers typically attempt to reduce the mass of the camshaft assembly by various means.
This section provides a general summary of the disclosure, and is not a comprehensive disclosure of its full scope or all of its features.
A camshaft assembly may include a shaft and a cam assembly coupled thereto. The cam assembly may comprise a hollow structure with an interior surface and an exterior surface, with a plurality of projections on the exterior surface. The interior surface may define a recess axially aligned with at least one of the plurality of projections. At least one of the plurality of projections may include an undercut portion.
An engine assembly may comprise an engine structure and a camshaft assembly. The camshaft assembly may include a shaft and a cam assembly coupled thereto. The cam assembly may comprise a hollow structure with an interior surface and an exterior surface, with a plurality of projections on the exterior surface. The interior surface may define a recess axially aligned with at least one of the plurality of projections. At least one of the plurality of projections may include an undercut portion.
A method of assembling a camshaft assembly may include providing a shaft and forming a cam assembly. The cam assembly may comprise a hollow structure with an interior surface and an exterior surface, with a plurality of projections on the exterior surface. The interior surface may define a recess axially aligned with at least one of the plurality of projections. At least one of the plurality of projections may include an undercut portion. The cam assembly may be coupled with the shaft.
Further areas of applicability will become apparent from the description provided herein. The description and specific examples in this summary are intended for purposes of illustration only and are not intended to limit the scope of the present disclosure.
The drawings described herein are for illustrative purposes only and are not intended to limit the scope of the present disclosure in any way.
Corresponding reference numerals indicate corresponding parts throughout the several views of the drawings.
Examples of the present disclosure will now be described more fully with reference to the accompanying drawings. The following description is merely exemplary in nature and is not intended to limit the present disclosure, application, or uses.
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As described above, one or more projections 16 may project from the exterior surface 17 of cam assembly 14. In order to achieve a reduction in mass of the cam assembly 14, all or a subset of the projections 16 may include an undercut portion 16U. The undercut portion 16U may be constructed such that the axial length 16L along the contact surface 16C of the projection 16 is greater than the axial length 16L′ along the exterior surface 17 of cam assembly 14. Further, the height of the undercut portion 16H may be increased to maximize the reduction of mass while maintaining the strength, structural integrity and performance of the projection 16 and cam assembly 14.
The interior surface 19 may also be profiled in order to reduce the mass of cam assembly 14. As seen in
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An exemplary method of manufacturing a camshaft assembly, such as camshaft assembly 10 described above, is described as follows. A shaft 12 may be provided. The shaft 12 may comprise a hollow tube structure, as described above. By way of non-limiting example, the shaft 12 may be a thin walled tube structure that is designed to reduce the mass of shaft 12, while also maintaining the strength, structural integrity and performance of the camshaft assembly 10.
A cam assembly 14 may be formed. In a first non-limiting example, the cam assembly 14 may be formed by an investment casting process. The investment casting process may include the step of forming an investment within a shell of a ceramic or similar material. The shell may be filled with a molten material, e.g., steel, that will be used to form the cam assembly 14. Upon cooling of the material, the shell may be removed, e.g., by hammering, vibration, chemical removal or other process. Alternatively, the shell may begin to crack and fall away from the cam assembly 14 upon cooling. In comparison to other casting processes, the accuracy of an investment reduces the amount of machining to complete the cam assembly 14. In a second non-limiting example, the cam assembly 14 may be formed by a powder metallurgy (“PM”) process. With a PM process, however, the coupling of the cam assembly 14 with the shaft 12 (described below) may be accomplished by sinter bonding.
The formed cam assembly 14 may be hardened, for example, by induction hardening, flame hardening, laser hardening or any other hardening process. The cam assembly 14 as a whole may be hardened or individual components of the cam assembly 14, such as projections 16, may be hardened. The hardened cam assembly 14 may then be coupled with shaft 12, which is described more fully below.
The cam assembly 14 and shaft 12 may be coupled by being frictionally engaged with each other, for example, by a ballizing process. In a ballizing process, the cam assembly 14 may be positioned on a hollow, tubular shaft 12. The tubular shaft 12 may then be expanded to hold the cam assembly 14 in position. This may be accomplished by clamping the ends of the shaft 12 to prevent longitudinal growth and forcing a ball (or plurality of balls of increasing diameter) through the tubular shaft 12. The ball or balls are larger than the original shaft 12 inner diameter, thus expanding the shaft 12 to engage cam assembly 14. Other forms of coupling the cam assembly 14 with shaft 12 may also be used, such as sinter bonding, welding, shrink fitting, an expanding mandrel process or any other method.
It is understood that the parts of the camshaft assembly 10 may be coupled to one another in a variety of ways and the present disclosure is not limited to a frictional engagement. For example, in various embodiments the shaft 12 may be formed integrally with the cam assembly 14 to form a monolithic camshaft assembly 10. In these embodiments, the step of coupling the shaft 12 with cam assembly 14 may be eliminated as the shaft 12 and cam assembly 14 may be formed as a single, monolithic piece.
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