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Method for fabricating shell molds for the production of superalloy castings

Assignee: RTX Corp
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Filing: 1974-12-16
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Granted: 1976-01-20
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Expires: 1994-12-16
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Abstract

Abstract A method for producing shell molds for the investment casting and subsequent directional solidification of nickel and cobalt based superalloys is described. The shell mold is composed of high purity alumina and characterized by the presence of silica in trace form only. The shell mold of the present invention is nonreactive with molten nickel and cobalt base superalloys even during exposures of up to 12 hours. Additionally the alumina shell mold of the present invention has a unique combination of mechanical strength and stability at elevated temperatures.

Inventors

  • 👤 Michael H. Fassler
  • 👤 James S. Perron

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 13:12
CPC Classifications
B; B22; B22C; B22C9/00; B22C9/02; B22C9/04; B22C1/00; B22C1/16; B22C1/165

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 280 words
A method for the fabrication of shell molds suited for use in the production of directionally solidified components made from nickel and cobalt base alloys, comprising the steps of A. providing a pattern which duplicates the size and shape of the desired final product, said pattern being made of wax or similar material; B. providing a slurry containing from 15 to 25 parts of an aqueous solution containing about 50% aluminum polyoxychloride, from 6 to 10 parts water, from 8 to 14 parts of a binding agent such as latex, from 25 to 35 parts of -325 mesh alumina, from 7 to 12 parts of -100 mesh alumina, from 10 to 20 parts of -38/+100 mesh alumina, and from 0.5 to 1.5 parts of a pH control agent such as a 2% aqueous solution of HCl; C. dipping the pattern into the slurry so as to coat the pattern with the slurry; D. drying the coated pattern; E. dipping the coated pattern into the slurry and then applying dry -38/+100 mesh alumina; F. drying the coated pattern; G. dipping the coated pattern into ethyl alcohol, then into the slurry, and then applying dry -28/+48 mesh alumina; H. drying the coated pattern; I. repeating steps G and H a plurality of times; J. removing the wax by heating the coated pattern to a temperature in excess of the melting temperature of the pattern material; K. firing the mold at an elevated temperature to remove all pattern residue and consolidate the shell mold; whereby the resultant shell mold is composed of substantially pure alumina and is resistant to attack by molten nickel and cobalt alloys during exposures of up to 12 hours.
Claim 2
Independent Claim 280 words
A method for the fabrication of shell molds suited for use in the production of directionally solidified components made from nickel and cobalt base alloys, comprising the steps of A. providing a pattern which duplicates the size and shape of the desired final product, said pattern being made of wax or similar material; B. providing a slurry containing from 15 to 25 parts of an aqueous solution containing about 50% aluminum polyoxychloride, from 6 to 10 parts water, from 8 to 14 parts of a binding agent such as latex, from 25 to 35 parts of -325 mesh alumina, from 7 to 12 parts of -100 mesh alumina, from 10 to 20 parts of -38/+100 mesh alumina, and from 0.5 to 1.5 parts of a pH control agent such as a 2% aqueous solution of HCl; C. dipping the pattern into the slurry so as to coat the pattern with the slurry; D. drying the coated pattern; E. dipping the coated pattern into the slurry and then applying dry -38/+100 mesh alumina; F. drying the coated pattern; G. dipping the coated pattern into ethyl alcohol, then into the slurry, and then applying dry -28/+48 mesh alumina; H. drying the coated pattern; I. repeating steps G and H a plurality of times; J. removing the wax by heating the coated pattern to a temperature in excess of the melting temperature of the pattern material; K. firing the mold at an elevated temperature to remove all pattern residue and consolidate the shell mold; whereby the resultant shell mold is composed of substantially pure alumina and is resistant to attack by molten nickel and cobalt alloys during exposures of up to 12 hours.
Claim 3
Dependent Claim 23 words
A method as in claim 1 wherein the slurry contains from 0.5 to 1.5 parts calcium nitrate in addition to the elements recited.
Claim 4
Dependent Claim 25 words
A method as in claim 1 wherein the slurry contains from 0.05 to 0.25 parts of a wetting agent in addition to the elements recited.
Claim 5
Dependent Claim 23 words
A method as in claim 1 wherein the ratio of fine alumina to coarse alumina in the slurry is from 6:1 to 1:1.
Claim 6
Dependent Claim 15 words
A method as in claim 1 wherein the firing temperature is from 2100° to 2700°F.
Claim 7
Dependent Claim 112 words
A slurry material suitable for the production of alumina shell molds, for casting superalloys, consisting of: A. from 15 to 25 parts of an aqueous solution containing about 50 percent aluminum polyoxychloride; B. from 6 to 10 parts water; C. from 8 to 14 parts of a binding agent such as latex; D. from 25 to 35 parts of alumina having -325 mesh particle size; E. from 7 to 12 parts of alumina having a -100 mesh particle size; F. from 10 to 20 parts of alumina having a -38/+100 mesh particle size; G. from 0.5 to 1.5 parts of pH control agent such as a 2 percent aqueous solution of HCl.
Claim 8
Dependent Claim 112 words
A slurry material suitable for the production of alumina shell molds, for casting superalloys, consisting of: A. from 15 to 25 parts of an aqueous solution containing about 50 percent aluminum polyoxychloride; B. from 6 to 10 parts water; C. from 8 to 14 parts of a binding agent such as latex; D. from 25 to 35 parts of alumina having -325 mesh particle size; E. from 7 to 12 parts of alumina having a -100 mesh particle size; F. from 10 to 20 parts of alumina having a -38/+100 mesh particle size; G. from 0.5 to 1.5 parts of pH control agent such as a 2 percent aqueous solution of HCl.

References Cited (Backward Citations)

GB924510A Cited
US3748157A Cited
US3743003A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-01-19 1979-07-21 1980-01-20 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-01-19 1983-07-21 1984-01-20 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-01-19 1987-07-21 1988-01-20 $7700.00 Window Closed / Lapsed

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