Nano-structured refractory metals, metal carbides, and coatings and parts fabricated therefrom

Patent metadata

Field	Value
Publication number	US-9469543-B2
Application number	US-201414269019-A
Country	US
Kind code	B2
Filing date	May 2, 2014
Priority date	Dec 27, 2007
Publication date	Oct 18, 2016
Grant date	Oct 18, 2016

Abstract

Refractory metal and refractory metal carbide nanoparticle mixtures and methods for making the same are provided. The nanoparticle mixtures can be painted onto a surface to be coated and heated at low temperatures to form a gas-tight coating. The low temperature formation of refractory metal and refractory metal carbide coatings allows these coatings to be provided on surfaces that would otherwise be uncoatable or very difficult to coat, whether because they are carbon-based materials (e.g., graphite, carbon/carbon composites) or temperature sensitive materials (e.g., materials that would melt, oxidize, or otherwise not withstand temperatures above 800° C.), or because the high aspect ratio of the surface would prevent other coating methods from being effective (e.g., the inner surfaces of tubes and nozzles). The nanoparticle mixtures can also be disposed in a mold and sintered to form fully dense components.

First claim

What is claimed is:

1. A method for forming a refractory metal carbide component, the method comprising the steps of:
providing a refractory metal nanoparticle mixture, the refractory metal nanoparticle mixture including a solvent and a plurality of refractory metal nanoparticles, each of the plurality of refractory metal nanoparticles being surrounded by a layer of surfactant molecules in which the surfactant molecules are bonded to a surface of the refractory metal nanoparticles;
disposing the refractory metal nanoparticle mixture in a mold;
heating the refractory metal nanoparticle mixture to a first temperature to evaporate the solvent and leave the plurality of refractory metal nanoparticles surrounded by the surfactant molecules and bonded thereto in the mold; and
heating the plurality of refractory metal nanoparticles and the surfactant molecules while in the mold to a second temperature to thermally decompose the surfactant molecules and to react the plurality of refractory metal nanoparticles with carbon from the decomposed surfactant molecules to provide a refractory metal carbide component.

2. The method according to claim 1 , wherein the refractory metal carbide component comprises a carbide of a refractory metal chosen from the group consisting of titanium (Ti), zirconium (Zr), hafnium (Hf), niobium (Nb), tantalum (Ta), tungsten (W), and silicon (Si).

3. The method according to claim 1 , wherein the surfactant molecules comprise a hydrocarbon.

4. The method according to claim 1 , wherein heating to the second temperature occurs in an inert gas chamber.

5. The method of claim 1 , wherein the refractory metal nanoparticle mixture further comprises a secondary carbon source admixed with the plurality of refractory metal nanoparticles and the solvent.

6. The method of claim 5 , wherein the secondary carbon source comprises a hydrocarbon.

7. The method of claim 1 , wherein the surfactant molecules comprise more than 10 carbon atoms.

Assignees

• Lockheed Corp

Inventors

• Zinn Alfred A

Classifications

• B22F1/0545

  Dispersions or suspensions of nanosized particles · CPC title

• C04B35/522

  Graphite (C04B35/536 takes precedence) · CPC title

• C04B35/632

  Organic additives · CPC title

• B22F1/0062

  Operations & Transport · mapped topic

• B22F3/10

  Sintering only · CPC title