US2003039572A1PendingUtilityA1
Method of producing powder metal parts using induction sintering
Priority: Jun 22, 2001Filed: Jun 22, 2001Published: Feb 27, 2003
Est. expiryJun 22, 2021(expired)· nominal 20-yr term from priority
C22C 33/02B22F 3/105B22F 2003/023B22F 2003/1053
40
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Claims
Abstract
A method of forming a part from a metallurgical powder includes compressing a metallurgical powder including no more than 0.3 weight percent of lubricant within a die to provide a green compact. The green compact is subsequently sintered by induction heating up to a sintering temperature of the green compact and maintaining the compact at the temperature for a time sufficient to provide a sintered compact. The sintered part may be subsequently hot formed and/or forged to densify and adjust the dimensions of the sintered compact.
Claims
exact text as granted — not AI-modifiedWhat is claimed is:
1 . A method of forming a part from a metallurgical powder, the method comprising:
compressing a metallurgical powder comprising 0 up to 0.3 weight percent of internal lubricant within a die to provide a green compact; and sintering the green compact by induction heating the green compact to provide a sintered compact.
2 . The method of claim 1 , wherein the metallurgical powder further comprises a particulate metallic material that may be heated by induction.
3 . The method of claim 2 , wherein the particulate metallic material is least one of a pure iron powder and an iron-containing powder.
4 . The method of claim 2 , wherein the metallurgical powder is one of a single powder and a powder blend.
5 . The method of claim 1 , wherein the metallurgical powder comprises 0 up to 3 weight percent graphite, 0 up to 12 weight percent nickel, 0 up to 3 weight percent molybdenum, 0 up to 10 weight percent copper, 0 up to 2 weight percent manganese, 0 up to 20 weight percent chromium, and iron.
6 . The method of claim 1 , wherein the metallurgical powder comprises 0 up to 1 weight percent graphite, 0 up to 6 weight percent nickel, 0 up to 2 weight percent molybdenum, 0 up to 3 weight percent copper, 0 up to 1 weight percent manganese, 0 up to 3 weight percent chromium, and iron.
7 . The method of claim 1 , wherein sintering the green compact comprises induction heating the green compact to a sintering temperature within the range of 1900° F. to 2500° F.
8 . The method of claim 1 , wherein the metallurgical powder is free of internal lubricant.
9 . The method of claim 1 , wherein the metallurgical powder comprises at least one internal lubricant selected from ethylene bis-stearamide, zinc stearate, and stearic acid.
10 . The method of claim 1 , wherein compressing at least a portion of the metallurgical powder comprises compressing at least a portion of the metallurgical powder in at least one of a self-lubricating die and a die including a die wall coated with a material to reduce friction and die wear.
11 . The method of claim 1 , wherein compressing the metallurgical powder comprises compressing the metallurgical powder at a pressure in the range of 10 up to 70 tsi.
12 . The method of claim 5 , wherein the green compact has a green strength of at least 1000 psi.
13 . The method of claim 5 , wherein the green compact has a density of at least 4.0 g/cc.
14 . The method of claim 1 , wherein induction heating the green compact comprises inducing a current within the green compact to increase the temperature of the green compact to a sintering temperature of the green compact.
15 . The method of claim 1 , wherein induction heating the green compact comprises placing the green compact within an induction work coil while passing alternating current through the coil to thereby induce a secondary current within the green compact through electromagnetic induction.
16 . The method of claim 14 , wherein the green compact is maintained at the sintering temperature for a time in the range of 2 up to 600 seconds.
17 . The method of claim 14 , wherein the green compact comprises 0 up to 3 weight percent graphite, 0 up to 12 weight percent nickel, 0 up to 3 weight percent molybdenum, 0 up to 10 weight percent copper, 0 up to 2 weight percent manganese, 0 up to 20 weight percent chromium, and balance iron and incidental impurities, and further wherein the green compact is maintained at the sintering temperature for at least 20 up to 180 seconds.
18 . The method of claim 14 , wherein the sintering temperature, measured in Fahrenheit degrees, is 60 up to 95 percent of the melting point of the primary component of the metallurgical powder.
19 . The method of claim 1 , further comprising:
processing the sintered compact by at least one of hot forming and forging the sintered compact.
20 . The method of claim 19 , wherein hot forming and forging the sintered compact comprises placing the sintered compact in a heated die and applying pressure to the sintered compact.
21 . The method of claim 20 , wherein the heated die is at a temperature in the range of 200 up to 800° F. (93° C. up to 427° C.).
22 . The method of claim 20 , wherein 20 up to 90 tsi pressure is applied to the sintered compact.
23 . The method of claim 20 , wherein about 40 tsi pressure is applied to the sintered compact.
24 . The method of claim 20 , further comprising prior to hot forming the sintered compact, cooling the sintered compact to a temperature less than the sintering temperature.
25 . The method of claim 24 , wherein cooling the sintered compact comprises cooling the sintered compact to a temperature in the range of 1400 up to 2100° F. (1371° C.).
26 . A method of forming a part from a metallurgical powder, the method comprising:
compressing a metallurgical powder comprising predominantly iron and further comprising 0 up to 3 weight percent graphite, 0 up to 12 weight percent nickel, 0 up to 3 weight percent molybdenum, 0 up to 10 weight percent copper, 0 up to 2 weight percent manganese, 0 up to 20 weight percent chromium, and up to 0.3 weight percent internal lubricant, within a die at a pressure in the range of 10 up to 70 tsi to provide a green compact; sintering the green compact by induction heating the green compact to a sintering temperature of the green compact, and maintaining the sintering temperature for a time in the range of 2 up to 600 seconds to provide a sintered compact; cooling the sintered compact to a temperature lower than the sintering temperature; and processing the sintered compact by at least one of hot forming and forging the sintered compact by placing the sintered compact in a heated die and applying a pressure in the range of 20 up to 90 tsi to the sintered compact.
27 . The method of claim 26 , wherein the green compact has a density of at least 4.0 g/cc.
28 . The method of any of claims 1 and 26 , wherein the part is selected from a gear, a sprocket, a spur pinion, a helical pinion, a cam lobe, a bushing, a bearing, and a bearing race.
29 . A part formed by a method comprising:
compressing a metallurgical powder comprising 0 up to 0.3 weight percent of internal lubricant within a die to provide a green compact; and sintering the green compact by induction heating the green compact to provide a sintered compact.
30 . The part of claim 29 , wherein the method further comprises:
processing the sintered compact by at least one of hot forming and forging the sintered compact.
31 . A part formed by a method comprising:
compressing a metallurgical powder comprising predominantly iron and further comprising 0 up to 3 weight percent graphite, 0 up to 12 weight percent nickel, 0 up to 3 weight percent molybdenum, 0 up to 10 weight percent copper, 0 up to 2 weight percent manganese, 0 up to 20 weight percent chromium, and up to 0.3 weight percent lubricant, within a die at a pressure in the range of 10 up to 70 tsi to provide a green compact; sintering the green compact by induction heating the green compact to a sintering temperature of the green compact and maintaining the sintering temperature for a time in the range of 2 up to 600 seconds to provide a sintered compact; cooling the sintered compact to a temperature lower than the sintering temperature; and processing the sintered compact by at least one of hot forming and forging the sintered compact in a heated die by applying a pressure in the range of 20 up to 90 tsi to the sintered compact.
32 . The part of any of claims 29 and 31 , wherein the part is selected from a gear, a sprocket, a spur pinion, a helical pinion, a cam lobe, a bushing, a bearing, and a bearing race.Join the waitlist — get patent alerts
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