← Back to Patent Explorer
US3665585A Expired / Lapsed US ⏱️ 0.0 years remaining

Composite heavy-duty mechanism element and method of making the same

Assignee: Federal Mogul LLC
•
Filing: 1970-12-04
•
Granted: 1972-05-30
•
Expires: 1990-12-04
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract A composite mechanism element, such as a bevel pinion (FIGS. 1 to 6 inclusive), or the inner race of a tapered roller bearing (FIGS. 7 to 10 inclusive and 16) has its working or load-bearing portion or portions composed of sintered powdered highperformance alloy while its supporting portion not subjected to concentrated or heavy loads, is made of a base metal, such as sintered powdered iron. The toothed outer load-bearing portion of the composite bevel pinion (FIG. 6) and the hollow frusto-conical inner supporting portion (FIGS. 10 to 15) are separately briquetted from high performance alloy powder and low performance metal powder respectively and separately sintered after which the low performance inner supporting portion is pressed into the high performance toothed outer portion so as to be inseparably secured thereto. In the inner race (FIG. 15) of the composite tapered roller bearing (FIG. 16) the low-performance and high-performance portions of the inner race are separately compacted in dies in a briquetting press to form briquettes which are separately sintered and thereafter are pressed together in an assembling operation which causes the high performance and low performance portions of each race to be inseparably secured to one another. The composite outer race is formed by arranging base metal powder and high performance alloy powder in abutting zones in an annular cavity of a briquetting press die and compressing them to form a composite briquette which is then sintered and afterward deformed in a forging die into its final annular shape. The resulting composite sintered powdered mechanism elements are of much lower material cost than corresponding mechanism elements formed of high performance alloy throughout yet perform satisfactorily and have sufficient strength and durability for most purposes. The tapered roller bearing races (FIG. 9) or the bevel pinion (FIG. 15) may be used as they are if of satisfactory density for their intended uses, or they may be further densified by being subjected to an additional hot forging operation with the article sintered thereafter if deemed necessary.

Inventors

  • 👤 William M Dunn
  • 👤 Myron C Sarnes

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-24 13:52
CPC Classifications
F; F16; F16H; F16H55/00; F16H55/02; F16H55/06; B; B21; B21K; B21K1/00; B21K1/04; B22; B22F; B22F5/00; B22F5/08; B22F5/10; B22F7/00; B22F7/06; F16C; F16C33/00; F16C33/30; F16C33/58; F16C33/62

Claims Analysis

Total Claims: 7
Claim 1
Independent Claim 86 words
A method of making a composite heavy-duty mechanism element, comprising confining an annular mass of low-performance metal particles in an annular enclosure, confining an annular mass of high-performance powdered alloy particles in an annular enclosure having a side wall surface configured to impart to said high performance mass a surface adapted to mate with a surface of said low-performance mass, compacting each mass separately in its respective annular enclosure, sintering each such compacted mass, and pressing said masses into particle-interlocking mating engagement subsequent to said sintering.
Claim 2
Independent Claim 86 words
A method of making a composite heavy-duty mechanism element, comprising confining an annular mass of low-performance metal particles in an annular enclosure, confining an annular mass of high-performance powdered alloy particles in an annular enclosure having a side wall surface configured to impart to said high performance mass a surface adapted to mate with a surface of said low-performance mass, compacting each mass separately in its respective annular enclosure, sintering each such compacted mass, and pressing said masses into particle-interlocking mating engagement subsequent to said sintering.
Claim 3
Dependent Claim 25 words
A method, according to claim 1, wherein the high-performance alloy particle mass is disposed externally of the low-performance metal particle mass during said pressing step.
Claim 4
Dependent Claim 15 words
A method, according to claim 1, including forming teeth in the high-performance alloy particle mass.
Claim 5
Dependent Claim 18 words
A method, according to claim 1, including forming an annular roller path on the high-performance alloy particle mass.
Claim 6
Dependent Claim 22 words
A method, according to claim 3, including inclining said teeth relatively to the axis of said mass during formation of said teeth.
Claim 7
Dependent Claim 35 words
A method, according to claim 4, including recessing said roller path into said high-performance alloy particle mass during formation of said roller path into said high-performance alloy particle mass during formation of said roller path.

References Cited (Backward Citations)

US3146099A Cited
US3611546A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1975-05-30 1975-11-29 1976-05-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1979-05-30 1979-11-29 1980-05-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1983-05-30 1983-11-29 1984-05-30 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag