Nanoparticle powders, methods for forming braze pastes, and methods for modifying articles

Patent metadata

Field	Value
Publication number	US-10668571-B2
Application number	US-201715842038-A
Country	US
Kind code	B2
Filing date	Dec 14, 2017
Priority date	Dec 14, 2017
Publication date	Jun 2, 2020
Grant date	Jun 2, 2020

Abstract

A nanoparticle powder is disclosed including a plurality of stabilized nanoparticles having a superalloy composition. At least about 90% of the particles have a convexity between about 0.980-1 and a circularity between about 0.850-1. A method for forming a braze paste is disclosed including mixing the plurality of stabilized nanoparticles with at least one organometallic precursor and up to about 5 wt % binder. A method for modifying an article is disclosed including applying the braze paste to a substrate including at least one crack, removing at least about 70% of the binder in the braze paste, and then applying additional braze paste over the first portion. Under vacuum or inert gas atmosphere, essentially all remaining binder is evaporated. The braze paste is brazed to the article at about 40-60% of the superalloy's bulk liquidus temperature, forming a brazed material and thereby sealing the at least one crack.

First claim

What is claimed is:

1. A method for modifying an article, comprising:
mixing a plurality of stabilized nanoparticles including a superalloy composition and an essentially spherical conformation with at least one organometallic precursor and up to about 5 wt % binder to form a braze paste, the superalloy composition being selected from the group consisting of nickel-based superalloys, cobalt-based superalloys, and combinations thereof;
applying a first portion of the braze paste to a substrate of the article including at least one crack;
removing at least about 70% of the binder in the first portion of the braze paste;
following removing the at least about 70% of the binder in the first portion of the braze paste, applying a second portion of the braze paste over the first portion of the braze paste;
placing the article and the braze paste under vacuum or an inert gas atmosphere;
evaporating essentially all of any remaining binder at an evaporation temperature of the binder; and
brazing the braze paste to the article at a brazing temperature between about 40% to about 60% of the bulk liquidus temperature of the superalloy for a brazing time of less than about 120 min,
wherein the brazing of the braze paste to the article forms a brazed material and seals the at least one crack.

2. The method of claim 1 , wherein the brazed material is essentially free of pores with diameters greater than about 5 μm within the at least one sealed crack.

3. The method of claim 1 , wherein removing at least about 70% of the binder in the first portion of the braze paste includes at least one drying cycle at a drying temperature of between about 100° C. to about 300° C. for a drying cycle duration of about 10 min to about 60 min.

4. The method of claim 3 , wherein the at least one drying cycle includes at least one of an air drying cycle under air atmosphere with the drying temperature between about 100° C. to about 220° C. and an inert drying cycle under vacuum or inert gas with the drying temperature between about 200° C. to about 300° C.

5. The method of claim 1 , wherein the plurality of stabilized nanoparticles further includes a range of particle size of up to about 50 nm.

6. The method of claim 1 , wherein a carbon-bound metal of the at least one organometallic precursor is a base metal of the superalloy composition.

7. The method of claim 1 , wherein the plurality of stabilized nanoparticles includes a tapped density of at least about 4 g/cm 3 .

8. The method of claim 1 , wherein at least about 90% of the plurality of nanoparticles includes a convexity of between about 0.980 to 1 and a circularity of between about 0.850 to 1.

9. The method of claim 1 , wherein the brazing temperature is between about 700° C. to about 1,000° C.

10. The method of claim 1 , wherein the at least one crack includes a crack width of less than about 0.25 mm when the substrate is conventionally cast or less than about 0.10 mm when the substrate is directionally solidified or single crystal, and the brazing time is between about 10 min to about 60 min.

11. The method of claim 1 , wherein the at least one crack includes a crack width of greater than about 0.25 mm when the substrate is conventionally cast or greater than about 0.10 mm when the substrate is directionally solidified or single crystal, and the brazing time is between about 45 min to about 120 min.

12. The method of claim 1 , wherein the braze paste further includes a plurality of microparticles, and the plurality of microparticles include the superalloy composition.

13. A method for forming a braze paste, comprising:
mixing a plurality of stabilized nanoparticles with at least one organometallic precursor and up to about 5 wt % binder,
wherein the plurality of stabilized nanoparticles includes a superalloy composition and an essentially spherical conformation, the superalloy composition being selected from the group consisting of nickel-based superalloys, cobalt-based superalloys, and combinations thereof.

14. The method of claim 13 , further including forming the plurality of stabilized nanoparticles, wherein forming the plurality of stabilized nanoparticles includes precipitating the plurality of stabilized nanoparticles with at least one stabilizer.

15. The method of claim 14 , wherein the at least one stabilizer is selected from the group consisting of fatty acids, thiols, and combinations thereof.

16. The method of claim 13 , further including forming the plurality of stabilized nanoparticles, wherein forming the plurality of stabilized nanoparticles includes a sol-gel process.

17. The method of claim 13 , further including forming the plurality of stabilized nanoparticles, wherein forming the plurality of stabilized nanoparticles includes sintering the plurality of stabilized nanoparticles at a sintering temperature for a sintering cycle duration.

18. The method of claim 17 , wherein the sintering temperature is about one-quarter of the bulk liquidus temperature of the superalloy.

19. The method of claim 17 , wherein the sintering temperature is between about 200° C. to about 300° C. and the sintering cycle duration is between about 10 min to about 60 min.

Assignees

• Gen Electric

Inventors

• Puidokas Sabrina Michelle

Classifications

• B23K20/233

  without ferrous layer · CPC title

• B23K35/025 Primary

  Pastes, creams or slurries · CPC title

• B23K1/203

  Fluxing, i.e. applying flux onto surfaces · CPC title

• B22F1/0059

  Operations & Transport · mapped topic

• B23K2101/001

  Turbines · CPC title