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Method for producing a cam

Assignee: Supervis
•
Filing: 1990-12-17
•
Granted: 1992-01-21
•
Expires: 2010-12-17
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Abstract

Abstract Molded articles, particularly cams for camshafts of internal combustion engines, are subjected to high wear conditions. In order to make them resistant to wear, they are produced from a sintered alloy, which has been fabricated by powder metallurgical means. The alloy has a hardened matrix with interstitial copper and consists of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight of copper, 0.1 to 1.5% by weight of carbon and, optionally, of admixtures of chromium, manganese, silicon and nickel totalling, at most, 5% by weight, the remainder being iron.

Inventors

  • 👤 Karl Leithner

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 09:24
CPC Classifications
B; B22; B22F; B22F5/00; B22F5/08; C; C22; C22C; C22C33/00; C22C33/02; C22C33/0257

Claims Analysis

Total Claims: 15
Claim 1
Independent Claim 109 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising pressing sintering powder of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight copper, 0.1 to 1.5% by weight carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5% by weight, the remainder being iron, into a molded cam with a green density of more than 7 g/cc, sintering the molded cam at a temperature below 1150° C. during a sintering period of 10 to 60 minutes and subsequently hardening and tempering the sintered cam.
Claim 2
Independent Claim 109 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising pressing sintering powder of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight copper, 0.1 to 1.5% by weight carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5% by weight, the remainder being iron, into a molded cam with a green density of more than 7 g/cc, sintering the molded cam at a temperature below 1150° C. during a sintering period of 10 to 60 minutes and subsequently hardening and tempering the sintered cam.
Claim 3
Dependent Claim 17 words
The method of claim 1, in which the sintering powder is comprised of a prealloyed iron-molybdenum powder.
Claim 4
Dependent Claim 20 words
The method of claim 2, in which the sintering powder is prepared by mixing copper with the prealloyed iron-molybdenum powder.
Claim 5
Dependent Claim 18 words
The method of claim 1, in which the carbon is introduced by mixing graphite with the sintering powder.
Claim 6
Dependent Claim 18 words
The method of claim 3, in which the carbon is introduced by mixing graphite with the sintering powder.
Claim 7
Dependent Claim 27 words
The method of claim 1, in which the carbon is introduced at least partly by means of a carburizing atmosphere during the sintering and/or during the hardening.
Claim 8
Dependent Claim 27 words
The method of claim 3, in which the carbon is introduced at least partly by means of a carburizing atmosphere during the sintering and/or during the hardening.
Claim 9
Independent Claim 156 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising preparing an alloy having a hardened matrix with interstitial copper, wherein the alloy consists of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight of copper, 0.1 to 1.5% by weight of carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5%, by consolidating sintering powder selected from partially alloyed or mixed alloyed iron-molybdenum powder, optionally containing carbon, homogenizing the consolidated sintering powder by sintering to produce an article with open pores, hardening, tempering and introducing copper into the open pores of the article by impregnation, with the proviso that the carbon is introduced into the sintering powder or the carbon is introduced by means of a carburizing atmosphere during sintering and/or hardening or the carbon is introduced by a combination thereof.
Claim 10
Independent Claim 156 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising preparing an alloy having a hardened matrix with interstitial copper, wherein the alloy consists of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight of copper, 0.1 to 1.5% by weight of carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5%, by consolidating sintering powder selected from partially alloyed or mixed alloyed iron-molybdenum powder, optionally containing carbon, homogenizing the consolidated sintering powder by sintering to produce an article with open pores, hardening, tempering and introducing copper into the open pores of the article by impregnation, with the proviso that the carbon is introduced into the sintering powder or the carbon is introduced by means of a carburizing atmosphere during sintering and/or hardening or the carbon is introduced by a combination thereof.
Claim 11
Dependent Claim 17 words
The method of claim 8, in which carbon is introduced by mixing graphite with the sintering powder.
Claim 12
Dependent Claim 14 words
The method of claim 8 in which the mixed alloyed iron-molybdenum powder contains carbon.
Claim 13
Dependent Claim 27 words
The method of claim 8, in which the carbon is introduced partly or completely by means of a carburizing atmosphere during sintering, hardening or a combination thereof.
Claim 14
Independent Claim 191 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising preparing an alloy having a hardened matrix with interstitial copper, wherein the alloy consists of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight of copper, 0.1 to 1.5% by weight of carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5%, by pressing sintering powder of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight copper, optionally 0.1 to 1.5% weight carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5% by weight, the remainder being iron, into a molded cam with a green density of more than 7 g/cc, sintering the molded cam at a temperature below 1150° C. during a sintering period of 10 to 60 minutes and subsequently hardening and tempering the sintered cam, with the proviso that the carbon is introduced into the sintering powder or carbon is introduced partly or completely by means of a carburizing atmosphere during sintering, hardening or a combination thereof.
Claim 15
Independent Claim 191 words
A method for the manufacture of molded articles, including a cam for a camshaft of internal combustion engines which is assembled according to the modular principle, comprising preparing an alloy having a hardened matrix with interstitial copper, wherein the alloy consists of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight of copper, 0.1 to 1.5% by weight of carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5%, by pressing sintering powder of 0.5 to 16% by weight of molybdenum, 1 to 20% by weight copper, optionally 0.1 to 1.5% weight carbon and, optionally, admixtures of chromium, manganese, silicon and nickel totalling at most 5% by weight, the remainder being iron, into a molded cam with a green density of more than 7 g/cc, sintering the molded cam at a temperature below 1150° C. during a sintering period of 10 to 60 minutes and subsequently hardening and tempering the sintered cam, with the proviso that the carbon is introduced into the sintering powder or carbon is introduced partly or completely by means of a carburizing atmosphere during sintering, hardening or a combination thereof.

References Cited (Backward Citations)

US4664706A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1995-01-20 1995-07-22 1996-01-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1999-01-20 1999-07-22 2000-01-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2003-01-20 2003-07-22 2004-01-21 $7700.00 Window Closed / Lapsed

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