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US4705203A Expired / Lapsed US ⏱️ 0.0 years remaining

Repair of surface defects in superalloy articles

Assignee: Pioneer Data Corp
•
Filing: 1986-08-04
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Granted: 1987-11-10
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Expires: 2006-08-04
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Abstract

Abstract Methods of repairing defects in superalloy articles are described. Defective areas are cleaned and prepared to expose clean substrate surfaces. A layer of superalloy powder material containing a melt depressant (boron) is applied. A layer of superalloy material essentially free from boron is then applied. The dual coated article is heated to a temperature at which the boron containing layer melts, but the boron-free layer does not. The boron diffuses into the substrate raising the melting point of the molten material until solidification results. The unmelted surface layer is subsequently removed leaving behind a repaired article free from surface defects.

Inventors

  • 👤 Charles C. McComas
  • 👤 Dennis C. Stewart

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-09 09:44
CPC Classifications
B; B23; B23P; B23P6/00; B23P6/002; B23P6/007; C; C23; C23C; C23C26/00; C23C26/02; C23C4/00; C23C4/18; C23C4/185; F; F01; F01D; F01D5/00; F01D5/005

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 126 words
Method of repairing surface defects in superalloy articles including the steps of a. preparing the article substrate surface by removing contamination, b. plasma spraying a first material into the defect area to fill the defect, said first material having a composition similar to that of the substrate being repaired except that from 1-4% boron has been added to depress the melting point, c. plasma spraying a layer of a second material over the first material, said second material having a melting point which approximates or exceeds that of the substrate, d. heating the article to a temperature which melts said first material without melting said substrate or said second material and holding at that temperature until isothermal solidification occurs, e. removing at least said second material.
Claim 2
Dependent Claim 126 words
Method of repairing surface defects in superalloy articles including the steps of a. preparing the article substrate surface by removing contamination, b. plasma spraying a first material into the defect area to fill the defect, said first material having a composition similar to that of the substrate being repaired except that from 1-4% boron has been added to depress the melting point, c. plasma spraying a layer of a second material over the first material, said second material having a melting point which approximates or exceeds that of the substrate, d. heating the article to a temperature which melts said first material without melting said substrate or said second material and holding at that temperature until isothermal solidification occurs, e. removing at least said second material.
Claim 3
Dependent Claim 140 words
Method of repairing surface defects in superalloy articles including the steps of a. preparing the article substrate surface by removing contamination, b. plasma spraying a first material into the defect area to fill the defect, said first material comprising a mixture of two species of powders, one of said powder species containing 1-4% boron and the overall composition of the two powder species being similar to that of the area being repaired except for boron content, c. plasma spraying a layer of a second material over the first material, said second material having a melting point which aproximates or exceeds that of the substrate, d. heating the article to a temperature which melts said first material without melting said substrate or said second material and holding at that temperature until isothermal solidification occurs, e. removing at least said second material.
Claim 4
Dependent Claim 140 words
Method of repairing surface defects in superalloy articles including the steps of a. preparing the article substrate surface by removing contamination, b. plasma spraying a first material into the defect area to fill the defect, said first material comprising a mixture of two species of powders, one of said powder species containing 1-4% boron and the overall composition of the two powder species being similar to that of the area being repaired except for boron content, c. plasma spraying a layer of a second material over the first material, said second material having a melting point which aproximates or exceeds that of the substrate, d. heating the article to a temperature which melts said first material without melting said substrate or said second material and holding at that temperature until isothermal solidification occurs, e. removing at least said second material.

References Cited (Backward Citations)

US3947606A Cited
US4008844A Cited
US4078977A Cited
US4233490A Cited
US4285459A Cited
US4382169A Cited
US4442968A Cited
US4459062A Cited
US4493451A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1990-11-09 1991-05-11 1991-11-10 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1994-11-09 1995-05-11 1995-11-10 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1998-11-09 1999-05-11 1999-11-10 $7700.00 Window Closed / Lapsed

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