Superalloy article repair method and alloy powder mixture
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B23P-006/04
B23K-001/04
B22F-007/02
출원번호
US-0383078
(1982-05-28)
발명자
/ 주소
Smith, Jr., Murray S.
Hilboldt, Mark S.
Bhat, Thirmaleshwara A.
출원인 / 주소
General Electric Company
대리인 / 주소
Sachs, Lee H.Lawrence, Derek P.
인용정보
피인용 횟수 :
45인용 특허 :
5
초록▼
A powder alloy mixture for use in a method of repairing high temperature superalloy articles includes a first, higher temperature alloy powder in the range of about 35-65 weight percent of the mixture. The first alloy powder is based on at least one element selected from Ni and Co and is characteriz
A powder alloy mixture for use in a method of repairing high temperature superalloy articles includes a first, higher temperature alloy powder in the range of about 35-65 weight percent of the mixture. The first alloy powder is based on at least one element selected from Ni and Co and is characterized as having good strength and environmental resistance along with the substantial absence of melting point depressant elements selected from Si and B in amounts greater than about 1% Si and 0.5% B. The second alloy powder is of a lower melting temperature alloy of Ni--Cr--Si--B--Co and is characterized by the substantial absence of C.
대표청구항▼
1. A mixture of a first alloy powder and a second alloy powder; the first alloy powder characterized as having good strength and environmental resistance and the substantial absence of melting point depressant elements selected from the group consisting of Si and B in amounts greater than, by wei
1. A mixture of a first alloy powder and a second alloy powder; the first alloy powder characterized as having good strength and environmental resistance and the substantial absence of melting point depressant elements selected from the group consisting of Si and B in amounts greater than, by weight, 1% Si and 0.05% B; the first alloy powder consisting essentially of, by weight, 0.01-0.65% C, 19-27% Cr, 0.2-16% W, up to 10% Mo, up to 20% Fe, up to 4% Ta, up to 1% Ti, up to 1% Zr, up to 0.5% La, up to 2% Mn, with the balance incidental impurities and at least one element selected from the group consisting of Ni and Co; the second alloy powder being of a Ni-Cr-Si-B-Co base alloy with a melting temperature lower than that of the first alloy powder and consisting essentially of, by weight, about 8-18% Cr, 2-6% Si, 1-5% B, 10-30% Co, up to about 5% Fe, with the balance Ni and incidental impurities, and further characterized by the substantial absence of C in amounts greater than an impurity level; the mixture consisting essentially of, by weight, 35-65% of the first alloy powder and 35-65% of the second alloy powder. 2. The mixture of claim 1 in which the first alloy powder has a melting temperature greater than about 2150° F. and consists essentially of, by weight, 0.05-0.55% C, 20-27% Cr, 0.2-8% W, up to 10% Mo, up to 20% Fe, with the balance Ni, Co and incidental impurities. 3. The mixture of claim 2 in which the first alloy powder includes Ni in the range of about 9-12 weight percent, the first alloy powder being about 45-50 weight percent of the mixture. 4. The mixture of claim 2 in which the first alloy powder includes Co in the range of about 0.5-3 weight percent, the first alloy powder being about 40-45 weight percent of the mixture. 5. The mixture of claim 1 in which the second alloy powder consists essentially of, by weight, 12-14% Cr, 3-5% Si, 2-3% B, 15-25% Co, up to about 5% Fe, with the balance Ni and incidental impurities, the second alloy being about 50-60 weight percent of the mixture. 6. The mixture of claim 5 in which the second alloy includes Co in the range of about 18-22 weight percent. 7. The mixture of claim 1 in which: the first alloy powder has a melting temperature greater than about 2150° F. and consists essentially of, by weight, 0.05-0.15% C, 20-23% Cr, 0.2-1% W, 8-10% Mo, 17-20% Fe, 0.5-3% Co, with the balance Ni and incidental impurities; and the second alloy powder consists essentially of, by weight, 12-14% Cr, 3-5% Si, 2.5-3% B, 18-22% Co, with the balance Ni and incidental impurities, the second alloy powder being about 55 weight percent of the mixture. 8. The mixture of claim 1 in which: the first alloy powder has a melting temperature greater than about 2150° F. and consists essentially of, by weight, 0.45-0.55% C, 24-27% Cr, 7-8% W, up to about 2% Fe, 9-12% Ni, with the balance Co and incidental impurities; and the second alloy powder consists essentially of, by weight, 12-14% Cr, 3-5% Si, 2.5-3% B, 18-22% Co, with the balance Ni and incidental impurities, the second alloy power being about 55 weight percent of the mixture. 9. A method for repairing a superalloy article comprising the steps of: providing the powder mixture of claim 1 of the first alloy powder and the second alloy powder; cleaning the article at least in an article portion to be repaired; applying the powder mixture to the article portion; and then, heating the powder mixture and at least the article portion in a vacuum at a temperature at which the second alloy powder will melt but at which the first alloy powder will not melt completely; the heating being conducted for at least 1/2 hour to allow interdiffusion to occur between the alloy powders. 10. The method of claim 9 for repairing a superalloy article including a brazed joint having a predetermined remelt temperature, wherein the heating is conducted at a temperature less than the brazed joint remelt temperature. 11. The method of claim 10 in which: the powder mixture is in the mixture of claim 2; and the heating is conducted at a temperature in the range of 2100°-2200° F. 12. The method of claim 10 in which: the powder mixture is the mixture of claim 7; and the heating is conducted at about 2150° F. for about 11/2 to 21/2 hours. 13. The method of claim 10 in which: the powder mixture is the mixture of claim 8; and the heating is conducted at about 2150° F. for about 11/2 to 21/2 hours.
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이 특허에 인용된 특허 (5)
Baladjanian Gregor (Malibu CA) Rothman Robert L. (San Pedro CA), High temperature braze repair of superalloys.
Duvall David S. (Cobalt CT) Owczarski William A. (Cheshire CT) Paulonis Daniel F. (Moodus CT) Schaefer Robert P. (East Hartford CT), Method of repairing surface defects using metallic filler material.
Lee Jack W. (Brookfield CT) Miller Jule A. (Derby CT), High temperature metal alloy mixtures for filling holes and repairing damages in superalloy bodies.
Smith ; Jr. Murray S. (Cincinnati OH) Perkins Roger J. (Evendale OH) Fryxell Robert E. (Cincinnati OH) Young William R. (Cincinnati OH), Homogenous alloy powder.
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Zheng, Qingjun; Liu, Yixiong; Faust, James A; Rowe, Mark J; De Wet, Danie J; Subbaiyan, Sudharsan; Meyer, Michael J, Methods of making metal matrix composite and alloy articles.
Cohen, Joel Heywood; Budinger, David Edwin; Caldwell, James Michael; Gordon, Michael Glenn; Emilianowicz, Edward John, Nickel-base braze material and braze repair method.
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