Abstract A composite heavy-duty machine element such as a face gear (FIG. 7), a spur or helical gear (FIG. 14), or ball bearing races (FIG. 18), has its working or load bearing portion composed of sintered powdered high-performance alloy while its supporting portion not subjected to concentrated or intense heavy loads is made of a base metal such assintered powdered iron. In FIGS. 1 through 18 the powders of the two portions are inserted separately and successively in the die cavity of a briquetting press and simultaneously compacted to form a composite briquette which is then sintered to bond the separate portions together even though they are of different materials with different physical characteristics. The resulting composite sintered powdered metal machine element is of lower material cost than such an element formed of high-performance alloy in its entirety, and may then be used as it is if of satisfactory density for its intended use, or it may be further densified by means of an additional compressing operation with the article cold, warm or by a hot forging operation, or with subsequent sintering if deemed necessary depending upon its intended use. If the machine element is to be a face gear, the face gear as briquetted and sintered is subjected to a further deforming operation to so incline its teeth.
Inventors
👤 William M. Dunn
👤 Myron C. Sarnes
Bibliographic Details
Application Number—
JurisdictionUS
Data Sourcegoogle_patents
Last Synchronized2026-10-25 13:50
CPC Classifications
B; B22; B22F; B22F7/00; B22F7/06; B22F2998/00
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
122 words
A method of making a composite heavyduty machine element comprising confining a first annular mass of low-performance powdered metal particles in a first annular compartment, confining a second annular mass of high-performance powdered manganese-molybdenum alloy particles in a second annular compartment adjacent said first annular compartment, one of said annular compartments surrounding the other annular compartment, bringing said annular masses into surface-to-surface abutting engagement with one aother along a common substantially annular junction between said compartments, compacting said annular masses simultaneously, and sintering said annular masses simultaneously while in said abutting engagement with one another whereby to secure said masses to one another in surface-to-surface coaxial relationship with their respective particles at the junction between said masses disposed in geometrically interlocking engagement.
Claim 2
Independent Claim
122 words
A method of making a composite heavyduty machine element comprising confining a first annular mass of low-performance powdered metal particles in a first annular compartment, confining a second annular mass of high-performance powdered manganese-molybdenum alloy particles in a second annular compartment adjacent said first annular compartment, one of said annular compartments surrounding the other annular compartment, bringing said annular masses into surface-to-surface abutting engagement with one aother along a common substantially annular junction between said compartments, compacting said annular masses simultaneously, and sintering said annular masses simultaneously while in said abutting engagement with one another whereby to secure said masses to one another in surface-to-surface coaxial relationship with their respective particles at the junction between said masses disposed in geometrically interlocking engagement.
Claim 3
Dependent Claim
26 words
A method, according to claim 1, including the additional step of densifying said masses into substantially solid condition by hot-forging said masses subsequent to said sintering.