Fire containment coating system for titanium
US-9834835-B2 · Dec 5, 2017 · US
US10590516B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10590516-B2 |
| Application number | US-201414313997-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 24, 2014 |
| Priority date | Jun 24, 2014 |
| Publication date | Mar 17, 2020 |
| Grant date | Mar 17, 2020 |
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A vanadium alloy essentially consisting of: vanadium; and aluminium having a content of greater than 0 to 10 at %, and a process of producing thereof.
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The invention claimed is: 1. A process of producing a tube comprising a heat treated vanadium alloy, the process comprising: forming a vanadium alloy consisting of: aluminium having a content of greater than 0 to 10 at %; optionally a grain refining element selected from Ti, Cr, Fe, Ni or B having a content of greater than 0 to 5 at %, and the balance vanadium and unavoidable impurities; heat treating the formed vanadium alloy at temperatures of from 800 to 1500° C. and pressures from 50 to 500 MPa, thereby producing a heat treated vanadium alloy having a ductility of greater than 10% elongation; and subjecting the heat treated vanadium alloy to a deformation process so as to form the tube comprising the heat treated vanadium alloy and having a wall thickness of 0.05 to 1 mm. 2. The process of producing a tube comprising a heat treated vanadium alloy according to claim 1 , wherein said heat treated vanadium alloy has a ductility greater or equal to 12% elongation. 3. The process of producing a tube comprising a heat treated vanadium alloy according to claim 1 , wherein the heat treatment step comprises a Hot Isostatic Pressing (HIP) process. 4. The process of producing a tube comprising a heat treated vanadium alloy according to claim 1 , wherein the heat treatment step comprises subjecting the vanadium alloy to temperatures of from 1000 to 1400° C. 5. The process of producing a tube comprising a heat treated vanadium alloy according to claim 4 , wherein the heat treatment step comprises subjecting the vanadium alloy to pressures from 50 to 400 MPa. 6. The process of producing a tube comprising a heat treated vanadium alloy according to claim 4 , wherein the heat treatment step is undertaken for a duration of at least 30 min. 7. The process of producing a tube comprising a heat treated vanadium alloy according to claim 4 , wherein at least one of a heating rate or cooling rate of the heat treatment step is at least 4 K/min. 8. A process according to claim 1 , wherein the tube has an outer diameter of between 2 to 25 mm. 9. The process of producing a tube comprising a heat treated vanadium alloy according to claim 1 , wherein said heat treated vanadium alloy has a grain linear intercept of less than 5.0 mm, based upon a minimum sample size of 6 grains. 10. The process of producing a tube comprising a heat treated vanadium alloy according to claim 1 , wherein said heat treated vanadium alloy does not include any voids having an average size of greater than 0.5 mm. 11. A process of producing a tube comprising a heat treated vanadium alloy, the process comprising: forming a vanadium alloy consisting of: aluminium having a content of greater than 0 to 10 at %; a grain refining element selected from Ti, Cr, Fe, Ni or B having a content of 0 to 5 at %, and the balance vanadium and unavoidable impurities; heat treating the formed vanadium alloy at temperatures of from 800 to 1500° C. and pressures from 50 to 500 MPa, thereby producing a heat treated vanadium alloy having a ductility of greater than 10% elongation; and subjecting the heat treated vanadium alloy to a deformation process so as to form the tube comprising the heat treated vanadium alloy and having a wall thickness of 0.05 to 1 mm. 12. The process of producing a tube comprising a heat treated vanadium alloy according to claim 11 , wherein said heat treated vanadium alloy has a ductility greater or equal to 12% elongation. 13. The process of producing a tube comprising a heat treated vanadium alloy according to claim 11 , wherein the heat treatment step comprises a Hot Isostatic Pressing (HIP) process. 14. The process of producing a tube comprising a heat treated vanadium alloy according to claim 11 , wherein the heat treatment step comprises subjecting the vanadium alloy to temperatures of from 1000 to 1400° C. 15. The process of producing a tube comprising a heat treated vanadium alloy according to claim 14 , wherein the heat treatment step comprises subjecting the vanadium alloy to pressures from 50 to 400 MPa. 16. The process of producing a tube comprising a heat treated vanadium alloy according to claim 14 , wherein the heat treatment step is undertaken for a duration of at least 30 min. 17. The process of producing a tube comprising a heat treated vanadium alloy according to claim 14 , wherein at least one of a heating rate or cooling rate of the heat treatment step is at least 4 K/min. 18. A process according to claim 11 , wherein the tube has an outer diameter of between 2 to 25 mm. 19. The process of producing a tube comprising a heat treated vanadium alloy according to claim 11 , wherein said heat treated vanadium alloy has a grain linear intercept of less than 5.0 mm, based upon a minimum sample size of 6 grains. 20. The process of producing a tube comprising a heat treated vanadium alloy according to claim 11 , wherein said heat treated vanadium alloy does not include any voids having an average size of greater than 0.5 mm.
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