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US3762881A Expired / Lapsed US ⏱️ 0.0 years remaining

Composite high strength machine element and method of making the same

Assignee: Federal Mogul LLC
•
Filing: 1971-06-14
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Granted: 1973-10-02
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Expires: 1991-06-14
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Abstract

Abstract This composite high-strength bushing consists of a heavy-loadbearing sleeve of sintered powdered high-performance alloy and a lesser-load-bearing support sleeve of sintered base metal such as sintered powdered iron. The outer sleeve has an internal taper while the inner sleeve has a matching external taper, both sleeves being separately formed from their respective powdered metals by suitable dies in conventional briquetting presses and thereafter sintered and forged by forcing them together in a hotforging press at a high temperature. The outer and inner sleeves are thereby firmly and inseparably joined by high heat and pressure and interlocked by the migration of minute portions of one of the metals past minute portions of the other metal across the tapered interface therebetween, thereby forming an intermediate zone of the intermingled metals encircling the interface. A modification employs tapers of slightly different convergence between the outer and inner sleeves but also results in a similarly-inseparable interlocking connection by a similar migration of the metals into an intermediate zone encircling the interface.

Inventors

  • 👤 W Dunn

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-03 23:16
CPC Classifications
F; F16; F16C; F16C33/00; F16C33/02; F16C33/04; F16C33/06; F16C33/14; F16C33/12; F16C33/121; F16C33/122; F16C33/30; F16C33/58; F16C33/62; F16C33/64; F16C17/00; F16C17/02; F16C19/00; F16C19/22; F16C19/24; F16C19/26; F16C2204/00; F16C2204/60; F16C2220/00; F16C2220/20; F16C2220/40; F16C2220/46; F16C2223/00; F16C2223/10; F16C2223/12; F16C2226/00; F16C2226/10; F16C2226/16; F16C2226/50; F16C2226/70; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49826; Y10T29/49861; Y10T428/00; Y10T428/12; Y10T428/12014; Y10T428/12028; Y10T428/12451; Y10T428/12493; Y10T428/12771; Y10T428/12778; Y10T428/12986

Claims Analysis

Total Claims: 2
Claim 1
Independent Claim 18 words
A composite high-strength bushing, according to claim 1, wherein said high-strength material is a nickel-content manganese-molybdenum iron alloy.
Claim 2
Dependent Claim 18 words
A composite high-strength bushing, according to claim 1, wherein said high-strength material is a nickel-free manganese-molybdenum iron alloy.

References Cited (Backward Citations)

No citation records indexed.

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-10-01 1977-04-02 1977-10-02 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-10-01 1981-04-02 1981-10-02 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-10-01 1985-04-02 1985-10-02 $7700.00 Window Closed / Lapsed

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