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US4285459A Expired / Lapsed US ⏱️ 0.0 years remaining

High temperature braze repair of superalloys

Assignee: Chromalloy Gas Turbine Corp
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Filing: 1979-07-31
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Granted: 1981-08-25
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Expires: 1999-07-31
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Abstract

Abstract Cracks in superalloys are braze repaired after notching or cutting away material adjacent the cracks, filling the recess with a braze component containing a melting point depressant and subjecting the repair area to a first elevated temperature to form a melt. The melting point of the repair region is raised by diffusing the depressant into the braze material and repair region at second and third elevated temperatures lower than the first elevated temperature to form a repaired superalloy exhibiting highly desirable properties.

Inventors

  • 👤 Gregor Baladjanian
  • 👤 Robert L. Rothman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 07:38
CPC Classifications
B; B23; B23P; B23P6/00; B23P6/002; B23P6/007; B22; B22F; B22F1/00; B22F1/09; B23K; B23K1/00; B23K1/008; B23K1/19; B23K1/20; B23K35/00; B23K35/22; B23K35/24; B23K35/30; B23K35/3033; B23K35/304; B23P6/04; B23P6/045; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49718; Y10T29/49721; Y10T29/49723; Y10T29/49725; Y10T29/49726; Y10T29/49728; Y10T29/49746

Claims Analysis

Total Claims: 21
Claim 1
Independent Claim 333 words
The method for repairing a crack in an article consisting of superalloy material selected from the group that includes Ni and Co as a base material, the crack extending into the article from the surface thereof, the method comprising the steps: (a) mechanically removing said material adjacent that part of the crack that extends from said surface down into the article, thereby to form in the article a recess whose walls are oxide free, (b) filling into the recess a braze mix that consists essentially of first and second portions in powdered state, the first portion consisting essentially of said superalloy material or a material analogous thereto, and the second portion consisting essentially of a braze component containing a melting point depressant, the weight ratio of said first and second portions being less than 1.5/1, (c) subjecting said mix in the recess and the article material adjacent the recess to first elevated temperature under vacuum conditions and for a first time interval for causing said mix to form a melt, said first elevated temperature being less than the melting temperature of said material adjacent the recess; and (d) thereafter subjecting the melt and the article material adjacent the recess to second elevated temperature near said first elevated temperature under vacuum conditions and for an extended time sufficient to diffuse the depressant out of a melt into the recess wall and into the first portion of the mix, and thereby to increase the melting temperature of said melt to slightly below that of the article superalloy material, (e) said extended time including a primary interval during which the second elevated temperature remains at an initial level lower than said first elevated temperature, and at a lower level within the range 2050°-2150°, and a secondary and subsequent interval during which the second elevated temperature remains at another level which is higher than said initial level, each of said primary and secondary intervals being less than five hours but substantially greater than said first time interval.
Claim 2
Independent Claim 333 words
The method for repairing a crack in an article consisting of superalloy material selected from the group that includes Ni and Co as a base material, the crack extending into the article from the surface thereof, the method comprising the steps: (a) mechanically removing said material adjacent that part of the crack that extends from said surface down into the article, thereby to form in the article a recess whose walls are oxide free, (b) filling into the recess a braze mix that consists essentially of first and second portions in powdered state, the first portion consisting essentially of said superalloy material or a material analogous thereto, and the second portion consisting essentially of a braze component containing a melting point depressant, the weight ratio of said first and second portions being less than 1.5/1, (c) subjecting said mix in the recess and the article material adjacent the recess to first elevated temperature under vacuum conditions and for a first time interval for causing said mix to form a melt, said first elevated temperature being less than the melting temperature of said material adjacent the recess; and (d) thereafter subjecting the melt and the article material adjacent the recess to second elevated temperature near said first elevated temperature under vacuum conditions and for an extended time sufficient to diffuse the depressant out of a melt into the recess wall and into the first portion of the mix, and thereby to increase the melting temperature of said melt to slightly below that of the article superalloy material, (e) said extended time including a primary interval during which the second elevated temperature remains at an initial level lower than said first elevated temperature, and at a lower level within the range 2050°-2150°, and a secondary and subsequent interval during which the second elevated temperature remains at another level which is higher than said initial level, each of said primary and secondary intervals being less than five hours but substantially greater than said first time interval.
Claim 3
Dependent Claim 30 words
The method of claim 1 wherein said mechanical removal of the material adjacent the crack includes cutting away the superalloy material of said article adjacent opposite sides of the crack.
Claim 4
Dependent Claim 23 words
The method of claim 1 carried out to repair a crack extent associated with weld repair of a primary crack in the article.
Claim 5
Dependent Claim 43 words
The method of claim 1 wherein the crack extends completely through the article between opposite sides thereof and said mechanical removal step is carried out to completely remove article material between said opposite sides so that said recess communicates between said opposite sides.
Claim 6
Dependent Claim 18 words
The method of claim 1 wherein said first elevated temperature is between about 2125° F. and 2175° F.
Claim 7
Dependent Claim 18 words
The method of claim 5 wherein said second elevated temperature is between about 2050° F. and 2150° F.
Claim 8
Dependent Claim 31 words
The method of claim 6 wherein said initial level of said second elevated temperature is about 2050° F., and said other level of said second elevated temperature is about 2150° F.
Claim 9
Dependent Claim 21 words
The method of claim 7 wherein said primary interval is about 3 hours, and said secondary interval is about 4 hours.
Claim 10
Dependent Claim 26 words
The method of claim 8 wherein said subjecting of the mix to said first elevated temperature is continued for a time interval of about 30 minutes.
Claim 11
Dependent Claim 12 words
The method of claim 1 wherein said superalloy consists of Rene 80.
Claim 12
Dependent Claim 19 words
The method of claim 10 wherein said first and second portions of the mix are about equal in weight.
Claim 13
Dependent Claim 15 words
The method of claim 11 wherein said second portion of the mix consists of BRB.
Claim 14
Dependent Claim 11 words
The method of claim 1 wherein said superalloy consists of X-40.
Claim 15
Dependent Claim 26 words
The method of claim 1 wherein the article initially has a surface coat, including the initial step of removing said coat, at least adjacent the crack.
Claim 16
Dependent Claim 12 words
The method of claim 14 wherein the article comprises a turbine vane.
Claim 17
Dependent Claim 25 words
The method of claim 15 wherein said mix consists of about 40% by weight of X-40 and about 60% by weight of said second portion.
Claim 18
Dependent Claim 15 words
The method of claim 16 wherein said second portion of the mix consists of AMS4783.
Claim 19
Dependent Claim 12 words
The method of claim 1 wherein the article comprises a turbine vane.
Claim 20
Dependent Claim 11 words
The method of claim 1 wherein said depressant consists of boron.
Claim 21
Dependent Claim 16 words
The method of claim 1 wherein the powdered braze mix will pass a 150 mesh screen.

References Cited (Backward Citations)

US3632319A Cited
US3759692A Cited
US4004047A Cited
US4008844A Cited
US4028787A Cited
US4098450A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-08-24 1985-02-23 1985-08-25 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-08-24 1989-02-23 1989-08-25 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-08-24 1993-02-23 1993-08-25 $7700.00 Window Closed / Lapsed

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