Composite components for use in high temperature applications
View Patent ↗Fibrous monolith composites suitable for use in high temperature environments and/or harsh chemical environments are provided, along with methods of preparation thereof. The fibrous monolith composites exhibit such beneficial properties as enhanced strength, corrosion resistance, thermal shock resistance and thermal cycling tolerance.
1. A high temperature fibrous monolith composite comprising:
a primary phase selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide and combinations thereof; and
an interface phase selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide and combinations thereof and generally surrounding the primary phase,
the phases being generally discrete in the composite and each phase being selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 1000° C. or more.
2. The high temperature fibrous monolith composite of claim 1 , wherein each phase is selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 1600° C. or more.
3. The high temperature fibrous monolith composite of claim 1 , wherein each phase is selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 2500° C. or more.
4. The high temperature fibrous monolith composite of claim 1 , wherein each phase is selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 3000° C. or more.
5. An article of manufacture suitable for use in a high temperature environment comprising fibrous monolith composite materials, fibrous monolith composite materials comprising:
a first composition selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and suicide and combinations thereof; and
a second composition generally surrounding the first composition and selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide and combinations thereof,
the compositions being generally discrete in the composite materials and each composition being selected from the group consisting of materials that remain in the solid state to allow use of the article at an operating temperature of at least about 1000° C. or more.
6. The article of manufacture of claim 5 , wherein the article is an anti-matter containment vessel.
7. The article of manufacture of claim 5 , wherein the article is a furnace furniture radiant burner panel.
8. The article of manufacture of claim 5 , wherein the article is a rocket nozzle.
9. The article of manufacture of claim 5 , wherein the article is an internal combustion engine component.
10. The article of manufacture of claim 5 , wherein the article is a steering vane for vectored thrust control.
11. The article of manufacture of claim 5 , wherein the article is a cutting tool.
12. The article of manufacture of claim 5 , wherein the article is a radiant burner tube.
13. The article of manufacture of claim 5 , wherein the article is an x-ray target for CT Scanner X-ray tubes.
14. The article of manufacture of claim 5 , wherein the article is high temperature furnace equipment.
15. The article of manufacture of claim 5 , wherein the article is a solid hot gas containment tube.
16. The article of claim 5 , wherein each composition is selected from the group consisting of materials that remain in the solid state to allow use of the article at an operating temperature of at least about 1600° C. or more.
17. The article of claim 5 , wherein each composition is selected from the group consisting of materials that remain in the solid state to allow use of the article at an operating temperature of at least about 2500° C. or more.
18. The article of claim 5 , wherein each composition is selected from the group consisting of materials that remain in the solid state to allow use of the article at an operating temperature of at least about 3000° C. or more.
19. A method of producing an X-ray target comprising the step of:
extruding a fibrous monolith material through a deposition nozzle; and depositing the fibrous monolith material onto a substrate.
20. A method of manufacturing a high temperature fibrous monolith composite comprising:
blending a first composition of one or more powders selected from the group consisting of metal, metal alloy, carbide, nitride, boride oxide, phosphate and silicide and combinations thereof with a processing compound to provide a core material;
blending a second composition of one or more powders selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide and combinations thereof with a processing compound to provide a shell material;
forming a feed rod from the core material and shell material, the core material and shell material having a volume ratio in the range of about 50:50 to about 99:1;
extruding the formed feed rod to create a reduced diameter filament; and
sintering the filament to provide the high temperature fibrous monolith composite,
the core material and shell material being generally discrete in the composite and each composition being selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 1000° C. or more.
21. The method of in claim 20 , wherein the processing compound includes a polymer binder and wherein the polymer binder is removed from the filament after extrusion.
22. A method of manufacturing a high temperature fibrous monolith composite comprising:
blending a first composition of one or more powders selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and suicide and combinations thereof with a processing compound to provide a core material;
blending a second composition of one or more powders selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and suicide and combinations thereof with a processing compound to provide a shell material;
forming a feed rod from the core material and shell material, the core material and shell material having a volume ratio in the range of about 50:50 to about 99:1;
extruding the formed feed rod to create a reduced diameter first filament;
consolidating two or more first filaments to create a multi-filament rod;
extruding the multi-filament rod to create a reduced diameter second filament; and
sintering the filament to provide the high temperature fibrous monolith composite,
the core material and shell material being generally discrete in the composite and each composition being selected from the group consisting of materials that remain in the solid state to allow use of the composite at an operating temperature of at least about 1000° C. or more.
23. An X-ray target comprising:
a layer of fibrous monolith material; and
a substrate.
24. The X-ray target of claim 23 wherein the fibrous monolith material is selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide.
25. An X-ray target comprising:
a substrate having a first and second side;
a first layer of fibrous monolith material deposited on the first side of the graphite substrate; and
a second layer of fibrous monolith material deposited on the second side of the graphite substrate.
26. The X-ray target of claim 25 wherein the fibrous monolith material is selected from the group consisting of metal, metal alloy, carbide, nitride, boride, oxide, phosphate and silicide.