IP Library › Granted Patent US 11,661,891
Granted Patent B1
US 11,661,891 · App. 17/814,334 · Granted May 30, 2023

Surface with shape memory alloy particles

Inventors: Narayanan Janakiraman (Bengaluru, IN); Paul Mathew (Bengaluru, IN); Sreerama Prasad Ramaswamy (Bengaluru, IN); Hiranya Nath (Bengaluru, IN); Ravindra Shankar Ganiger (Bengaluru, IN)
Assignee: GENERAL ELECTRIC COMPANY
F02C7/30F02C7/222F05D2220/323F05D2260/95F05D2300/505F05D2300/6111
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Quick Facts
Patent No.
US 11,661,891
App. No.
17/814,334
Granted
May 30, 2023
Kind
B1
Abstract

A component susceptible to the formation of deposits, such as a component of a hydrocarbon system in a gas turbine engine. The component includes a substrate having a surface susceptible to the formation of a deposit thereon. A shape memory alloy coating is formed on the surface of the substrate. The shape memory alloy coating is a plurality of particles formed on the surface, and each particle of the plurality of particles is formed from a shape memory alloy.

Claims (26)

1. A gas turbine engine comprising a component of a hydrocarbon system, the component including:

a fluid passage through which a hydrocarbon fluid flows;

a substrate having a surface facing the fluid passage to be wetted by the hydrocarbon fluid; and

a shape memory alloy coating formed on the surface of the substrate, the shape memory alloy coating being a plurality of particles formed on the surface, and each particle of the plurality of particles being formed from a shape memory alloy.

2. The gas turbine engine of claim 1 , wherein the shape memory alloy is one of a nickel-titanium alloy, a cobalt-nickel-aluminum alloy, nickel-iron-gallium alloy, an iron-manganese-gallium alloy, or a cobalt-nickel-gallium alloy.

3. The gas turbine engine of claim 1 , wherein each particle of the plurality of particles is irregularly shaped.

4. The gas turbine engine of claim 1 , wherein the substrate is formed from a metal alloy chosen from the group consisting of iron-based alloys, nickel-based alloys, and chromium-based alloys.

5. The gas turbine engine of claim 1 , wherein the hydrocarbon fluid is fuel, and the component is at least one of a fuel line and a fuel nozzle.

6. The gas turbine engine of claim 1 , wherein the hydrocarbon fluid is oil, and the component is an oil line.

7. The gas turbine engine of claim 1 , wherein each particle of the plurality of particles includes a particle diameter, and each particle of the plurality of particles is spaced apart from each other by a distance that is ten percent of the particle diameter or greater and is a diameter of the particle or less.

8. The gas turbine engine of claim 1 , wherein each particle of the plurality of particles is spaced apart from each other on the surface, and

wherein the surface has an area, and the plurality of particles has a surface density on the surface, the surface density being from twenty percent to ninety-five percent of the area of the surface.

9. A component susceptible to the formation of deposits, the component comprising:

a substrate having a surface susceptible to the formation of a deposit thereon; and

a shape memory alloy coating formed on the surface of the substrate, the shape memory alloy coating being a plurality of particles formed on the surface, and each particle of the plurality of particles being formed from a shape memory alloy.

10. The component of claim 9 , wherein the shape memory alloy is one of a nickel-titanium alloy, a cobalt-nickel-aluminum alloy, nickel-iron-gallium alloy, an iron-manganese-gallium alloy, or a cobalt-nickel-gallium alloy.

11. The component of claim 9 , wherein the particles of the plurality of particles are irregularly arranged on the surface.

12. The component of claim 9 , wherein the particles of the plurality of particles are arranged in an ordered array on the surface.

13. The component of claim 9 , wherein each particle of the plurality of particles is irregularly shaped.

14. The component of claim 9 , wherein each particle of the plurality of particles has a shape, the shape being one of hemispherical, conical, pyramidal, or cuboidal.

15. The component of claim 9 , wherein each particle of the plurality of particles has (i) a width at the surface, (ii) a height projecting from the surface, and (iii) an aspect ratio of the height to the width, the aspect ratio being twenty to one or less.

16. The component of claim 9 , wherein the surface includes a plurality of recesses, a particle of the plurality of particles being located in each one of the plurality of recesses.

17. The component of claim 9 , wherein each particle of the plurality of particles is spaced apart from each other on the surface.

18. The component of claim 17 , wherein the surface has an area, and the plurality of particles has a surface density on the surface, the surface density being from twenty percent to ninety-five percent of the area of the surface.

19. The component of claim 17 , wherein each particle of the plurality of particles includes a particle diameter, and each particle of the plurality of particles is spaced apart from each other by a distance that is ten percent of the particle diameter or greater.

20. The component of claim 19 , wherein each particle of the plurality of particles is spaced apart from each other by a distance that is a diameter of the particle or less.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jul 22, 2022
From: JANAKIRAMAN, NARAYANAN; MATHEW, PAUL; RAMASWAMY, SREERAMA PRASAD; NATH, HIRANYA; GANIGER, RAVINDRA SHANKAR
To: GENERAL ELECTRIC COMPANY
Reel/Frame 060596/0388 →
Priority Claims (1)
IN 202211019499 · Mar 31, 2022 · national
Cited By (1)
US 12,311,330