Tuning porous surface coatings using a plasma spray torch

Patent metadata

Field	Value
Publication number	US-11932946-B2
Application number	US-202217978892-A
Country	US
Kind code	B2
Filing date	Nov 1, 2022
Priority date	Nov 10, 2021
Publication date	Mar 19, 2024
Grant date	Mar 19, 2024

Abstract

A system and method are provided to create porous surface coatings. In use, a method is included for receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles, using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials, and flowing the synthesized carbon-containing composite materials onto a substrate. Some or all of the synthesized carbon-containing composite materials may include a surface layer and/or a bonding layer. Additionally, the method may include tuning the inputs based on tuning characteristics, the tuning characteristics including one or more of: porosity, heat transfer, or resistance to corrosion. Further, the method may include tuning the inputs to optimize temperature redistribution across a surface layer of some or all of the synthesized carbon-containing composite materials.

First claim

What is claimed is:

1. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials; and
flowing the synthesized carbon-containing composite materials onto a substrate, wherein the synthesized carbon-containing composite materials form a surface layer and are tuned based on tuning characteristics to allow for electron emissive cooling via the surface layer.

2. The method of claim 1 , further comprising tuning the inputs based on tuning characteristics, wherein the tuning characteristics include porosity, heat transfer, and/or resistance to corrosion.

3. The method of claim 2 , wherein the synthesized carbon-containing composite materials are tuned to allow for repeated thermal stress.

4. The method of claim 2 , wherein the synthesized carbon-containing composite materials are tuned to be electrically conductive.

5. The method of claim 2 , wherein the synthesized carbon-containing composite materials are tuned to allow for passive thermal control and active thermal control, wherein:
the passive thermal control is based, at least in part, on a porosity of the synthesized carbon-containing composite materials; and
the active thermal control is based, at least in part, on electron emissive cooling.

6. The method of claim 1 , wherein the synthesized carbon-containing composite materials have a RMS roughness within a range between 2.1 mm to 4.7 mm.

7. The method of claim 1 , wherein the synthesized carbon-containing composite materials have a melting point greater than 1500° C.

8. The method of claim 1 , wherein the synthesized carbon-containing composite materials are resistance to oxidation at a temperature greater than 1500° C.

9. The method of claim 1 , wherein the synthesized carbon-containing composite materials are tuned to have a low thermal conductivity.

10. The method of claim 1 , wherein a thickness of the synthesized carbon-containing composite materials is less than 4 mm.

11. The method of claim 1 , wherein some or all of the synthesized carbon-containing composite materials include a bonding layer.

12. The method of claim 11 , wherein the bonding layer is bonded by a metal-to-carbon bond to the substrate.

13. The method of claim 11 , wherein the bonding layer is a non-uniform deposition of the synthesized carbon-containing composite materials.

14. The method of claim 11 , wherein the bonding layer of the synthesized carbon-containing composite materials comprises a metal lattice.

15. The method of claim 1 , wherein the surface layer is hydraulically smooth.

16. The method of claim 15 , wherein the hydraulic smoothness of the surface layer reduces turbulent fluid flow on the surface layer.

17. The method of claim 15 , wherein the hydraulic smoothness of the surface layer causes laminar fluid flow on the surface layer.

18. The method of claim 1 , further comprising tuning the inputs to optimize temperature redistribution across a surface layer of some or all of the synthesized carbon-containing composite materials.

19. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials;
flowing the synthesized carbon-containing composite materials onto a substrate; and
forming a hydraulically smooth surface layer based on the synthesized carbon-containing composite materials, wherein the hydraulically smooth surface layer is configured to reduce turbulent flow on the surface layer or is configured to cause laminar flow on the surface layer.

20. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials, wherein the synthesized carbon-containing composite materials have a RMS roughness within a range between 2.1 mm to 4.7 mm; and
flowing the synthesized carbon-containing composite materials onto a substrate.

21. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials, wherein the synthesized carbon-containing composite materials are tuned to have a low thermal conductivity; and
flowing the synthesized carbon-containing composite materials onto a substrate.

22. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials;
flowing the synthesized carbon-containing composite materials onto a substrate; and
tuning the inputs to optimize temperature redistribution across a surface layer of some or all of the synthesized carbon-containing composite materials.

23. A method, comprising:
receiving, at a plasma spray torch, inputs comprising metallic particles and carbon particles;
using the plasma spray torch to cause in-situ nucleation of the inputs to synthesize carbon-containing composite materials;
flowing the synthesized carbon-containing composite materials onto a substrate; and
forming a hydraulically smooth surface layer of the substrate based on the synthesized carbon-containing composite materials, wherein the hydraulically smooth surface layer is configured to reduce turbulent flow on the substrate or is configured to cause laminar flow on the substrate.

24. The method of claim 23 , wherein the substrate is at least one of: an aircraft wing, an aircraft surface, a control surface, a vehicle surface, a drone wing, or a drone surface.

Assignees

• Lyten Inc

Inventors

• Stowell Michael
• Lanning Bruce

Classifications

• C23C6/00 Primary

  Coating by casting molten material on the substrate · CPC title

• C23C4/134 Primary

  Plasma spraying · CPC title

• C23C4/04

  characterised by the coating material · CPC title

• H05H1/42

  with provisions for introducing materials into the plasma, e.g. powder or liquid {(arc stabilising or constricting arrangements H05H1/3405; coaxial protecting fluids H05H1/341)} · CPC title

• C23C16/26

  Deposition of carbon only · CPC title