US2006042081A1PendingUtilityA1

High-precision sintered cam lobe material

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Assignee: TAKAMURA HIROYUKIPriority: Sep 30, 2002Filed: Sep 19, 2003Published: Mar 2, 2006
Est. expirySep 30, 2022(expired)· nominal 20-yr term from priority
C22C 33/0257F01L 2301/00C22C 38/16Y10T74/2101F16H 53/025C22C 38/08F01L 2303/00F01L 1/04Y10T29/49293B22F 2998/00B22F 2998/10B22F 2003/248C22C 38/10
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Claims

Abstract

The present invention is to provide a high-precision sintered cam lobe part which has high dimensional accuracy even when producing a cam lobe having a complicated shape and needs no grinding processing after fabricated while it has high wear resistance and pitting resistance. In order to attain the above object, the high-precision sintered cam lobe part of the present invention is a sintered cam lobe part obtained by subjecting a sintering powder to compression-molding and sintering one time only or two or more times repetitively to make the powder into a predetermined form and by carrying out thermal refining of the resulting body as required, wherein the cam lobe part is made of an iron-based sintered alloy comprising one or both of 0.3 to 5.0% by weight of Ni and 0.2 to 4.0% by weight of Cu, 0.5 to 1.2% by weight of C and unavoidable impurities, which is balanced with Fe, and has a density of 7.3 g/cm 3 or more, the hardness of the outer periphery of the cam lobe of 45 HRC or more and the rate of dimensional change from the molded body obtained in the final compressing process to the sintered body obtained in the final sintering process within ±0.5%.

Claims

exact text as granted — not AI-modified
1 . A high-precision sintered cam lobe part obtained by subjecting a sintering powder to compression-molding and sintering one time only or two or more times repetitively to make the powder into a predetermined form and by carrying out thermal refining of the resulting body as required, wherein the cam lobe part is made of an iron-based sintered alloy comprising one or both of 0.3 to 5.0% by weight of Ni and 0.2 to 4.0% by weight of Cu, 0.5 to 1.2% by weight of C and unavoidable impurities, which is balanced with Fe, and has a density of 7.3 g/cm 3  or more, the hardness of the outer periphery of the cam lobe of 45 HRC or more and the rate of dimensional change from the molded body obtained in the final compressing process to the sintered body obtained in the final sintering process within ±0.5%.  
     
     
         2 . A high-precision sintered cam lobe part according to  claim 1 , containing both of said Ni and said Cu.  
     
     
         3 . A high-precision sintered cam lobe part according to  claim 2 , which further contains 0.1 to 2.5% by weight of Mo.  
     
     
         4 . A method of producing a high-precision sintered cam lobe part, comprising steps of: subjecting a sintered body to quench-temper treatment in which the sintered body is formed into a predetermined shape by repeating compression and sintering once or two or more times using a sintering powder prepared so as to have the following final composition; and producing a sintered cam lobe part which is made of an iron-based sintered alloy having a final composition comprising one or both of 0.3 to 5.0% by weight of Ni and 0.2 to 4.0% by weight of Cu, 0.5 to 1.2% by weight of C and unavoidable impurities, which is balanced with Fe, and in which the density is 7.3 g/cm 3  or more, the hardness of the outer periphery of the cam lobe is 45 HRC or more, and the rate of dimensional change from the molded body obtained in the final compressing process to the sintered body obtained in the final sintering process is within ±0.5%.  
     
     
         5 . A method of producing a high-precision sintered cam lobe part according to  claim 4 , wherein the compressing and sintering process is carried out two or more times.  
     
     
         6 . A method of producing a high-precision sintered cam lobe part according to  claim 4 , wherein the outer periphery of the cam piece is processed by shotblasting after the quench-temper treatment.  
     
     
         7 . A method of producing a high-precision sintered cam lobe part according to  claim 4 , wherein the final composition contains both of said Ni and said Cu.  
     
     
         8 . A method of producing a high-precision sintered cam lobe part according to  claim 7 , wherein the final composition further contains 0.1 to 2.5% by weight of Mo.

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