Patent US4275090A successfully refreshed from Google Patents.
US4275090A
Expired / Lapsed
US
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Process for carbon bearing MCrAlY coating
Assignee: RTX Corp
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Filing: 1979-10-15
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Granted: 1981-06-23
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Expires: 1999-10-15
Abstract
Abstract A method of applying a wear resisting MCrAlY coating is comprised of plasma spraying a mixture of MCrAlY and Cr 3 C 2 powders to form a coating having both fine carbides and coarser Cr 3 C 2 carbides in an MCrAlY matrix. Heat treatment at 1080° C. after coating bonds the substrate and coating and forms further fine carbides. The coating desirably consists of by weight percent 18-80 Cr, 1.2-29 Al, up to 4.8 Y, 0.6-11 C, balance selected from the group consisting of Ni, Co, Fe, or mixtures thereof.
Inventors
- 👤 Charles C. McComas
- 👤 James W. Morris
- 👤 Larry S. Sokol
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 18:42
CPC Classifications
C; C23; C23C; C23C4/00; C23C4/04; C23C4/06; C23C4/073
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
180 words
A method of providing a coating having wear, corrosion, and oxidation resistance in a gas turbine environment, on a superalloy substrate, which comprises the steps of: (a) mixing MCrAlY powders with Cr 3 C 2 powders, wherein M is a metal selected from the group consisting of Ni, Co, Fe, or mixtures thereof, the powders having particle sizes less than 44 microns, with the Cr 3 C 2 having a first average particle size and being present in sufficient quantity in the mixture to produce the composition and structure after spraying which is indicated in step (b); (b) plasma spraying the powders so that they impinge on, adhere to the substrate, and interact during spraying to produce a coating which consists essentially of a MCrAlY matrix rich in carbon and containing fine carbides of the order of 1-2 microns size and coarse chromium carbides of the order of 12 microns size, the average size of the Cr 3 C 2 carbides being smaller than the said first average particle size, and the coating having at least 0.6 weight percent carbon.
Claim 2
Independent Claim
180 words
A method of providing a coating having wear, corrosion, and oxidation resistance in a gas turbine environment, on a superalloy substrate, which comprises the steps of: (a) mixing MCrAlY powders with Cr 3 C 2 powders, wherein M is a metal selected from the group consisting of Ni, Co, Fe, or mixtures thereof, the powders having particle sizes less than 44 microns, with the Cr 3 C 2 having a first average particle size and being present in sufficient quantity in the mixture to produce the composition and structure after spraying which is indicated in step (b); (b) plasma spraying the powders so that they impinge on, adhere to the substrate, and interact during spraying to produce a coating which consists essentially of a MCrAlY matrix rich in carbon and containing fine carbides of the order of 1-2 microns size and coarse chromium carbides of the order of 12 microns size, the average size of the Cr 3 C 2 carbides being smaller than the said first average particle size, and the coating having at least 0.6 weight percent carbon.
Claim 3
Dependent Claim
38 words
The method of claim 1 wherein the coating further consists essentially by weight percent of 18-80 Cr, 1.2-29 Al, up to 4.8 Y, 0.6-11 C, balance selected from the group consisting of Ni, Co, Fe, or mixtures thereof.
Claim 4
Dependent Claim
39 words
The method of claim 1 comprising the further step of heating the plasma sprayed substrate to form a diffusion bond between the coating and substrate and to form a MCrAlY matrix saturated in carbon and having additional fine carbides.
Claim 5
Independent Claim
64 words
The method of claims 1 or 2 wherein at least a portion of the mixture of MCrAlY powders with Cr 3 C 2 is replaced by a master alloy particulate consisting of MCrAlY and C and having a particle size less than 44 microns, any Cr 3 C 2 present within the master alloy particulate having an average particle size of about 15 microns.
Claim 6
Dependent Claim
21 words
The methods of claims 1, 2 or 3 wherein the matrix has a DPH hardness value of greater than about 725.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-06-22 | 1984-12-22 | 1985-06-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-06-22 | 1988-12-22 | 1989-06-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-06-22 | 1992-12-22 | 1993-06-23 | $7700.00 | Window Closed / Lapsed |