Claims
- 1. An improved shaft suitable for use in the treatment of molten aluminum including pumping or fluxing employing an impeller, comprised of:
- (a) a shaft comprised of a carbon or graphite material having an exterior surface; and
- (b) a refractory layer comprised of consolidated particles to cover said exterior surface of said shaft, the refractory layer resistant to attack by said molten metal, said refractory layer and said carbon or graphite material having a coefficient of thermal expansion less than 5.times.10.sup.-6 in/in/.degree. F., said refractory layer and said carbon or graphite material having a ratio of coefficient of thermal expansion in the range of 5:1 to 1:5.
- 2. The shaft in accordance with claim 1 wherein a bond layer is provided between said carbon or graphite surface and said refractory layer.
- 3. The shaft in accordance with claim 1 wherein said refractory coating is a ceramic coating selected from one of the group consisting of Al.sub.2 O.sub.3, ZrO.sub.2, Y.sub.2 O.sub.3, stabilized ZrO.sub.2, Al.sub.2 O.sub.3 --TiO.sub.2 and MgO--ZrO.sub.2.
- 4. The shaft in accordance with claim 2 wherein said bond layer has a thickness in the range of 0.1 to 5 mils.
- 5. The shaft in accordance with claim 1 wherein said refractory layer has a thickness in the range of 2 to 30 mils.
- 6. The shaft in accordance with claim 2 wherein said bond layer is comprised of an alloy selected from the group consisting of Cr--Ni--Al alloy and Cr--Ni alloy.
- 7. The shaft in accordance with claim 1 wherein said refractory layer is thermally applied.
- 8. The shaft in accordance with claim 1 wherein said refractory layer is applied by flame spray or plasma spray.
- 9. The shaft in accordance with claim 1 wherein said refractory layer has a porosity of 1 to 20%.
- 10. The shaft in accordance with claim 9 wherein said porosity is sealed to provide pore closure.
- 11. The shaft in accordance with claim 1 wherein said refractory layer has pores sealed using a material selected from the group consisting of pyrolyzed aluminum and hydrolyzed titanium tetrachloride or silicon tetrachloride.
- 12. An improved shaft for use in the treatment of molten aluminum comprised of:
- (a) a carbonaceous material, said shaft being circular in cross section and having an exterior surface;
- (b) a bond coat bonded to said exterior surface;
- (c) a refractory layer thermally applied to said bond coat of said shaft, the refractory layer selected from one of the group consisting of Al.sub.2 O.sub.3, ZrO.sub.2, Y.sub.2 O.sub.3, stabilized ZrO.sub.2, Al.sub.2 O.sub.3 --TiO.sub.2 and MgO--ZrO.sub.2, the carbonaceous material having a coefficient of thermal expansion of less than 5.times.10.sup.-6 in/in/.degree. F., said refractory layer and said carbonaceous material having a ratio of coefficient of thermal expansion in the range of 5:1 to 1:5, the refractory having pores; and
- (d) a sealant applied to said pores to prevent intrusion of said pores.
- 13. The shaft in accordance with claim 12 wherein said sealant is selected from the group consisting of pyrolyzed aluminum and hydrolyzed titanium tetrachloride or silicon tetrachloride.
- 14. The shaft in accordance with claim 12 wherein said bond layer has a thickness in the range of 0.1 to 5 mils.
- 15. The shaft in accordance with claim 12 wherein said refractory layer has a thickness in the range of 4 to 22 mils.
- 16. The shaft in accordance with claim 12 wherein said bond layer is comprised of an alloy selected from the group consisting of Cr--Ni--Al alloy and Cr--Ni alloy.
- 17. A method for processing a body of molten aluminum using an impeller, the method comprising the steps of:
- (a) providing a body of molten aluminum having a surface;
- (b) projecting an impeller on a shaft into said body through said surface, said shaft comprised of:
- (i) a carbonaceous material having an outside surface and having a coefficient of thermal expansion of less than 5.times.10.sup.-6 in/in/.degree. F.;
- (ii) a bond coating applied to said outside surface; and
- (iii) a refractory coating thermally applied to said bond coating, said refractory coating having a coefficient of thermal expansion of less than 5.times.10.sup.-6 in/in/.degree. F., said refractory coating extending above and below said surface to protect said shaft against wear and oxidation degradation at said surface; and
- (c) processing said body by rotating said impeller in an uni-directional mode or bi-directional mode.
- 18. The method in accordance with claim 17 wherein said refractory coating is a ceramic coating selected from one of the group consisting of Al.sub.2 O.sub.3, ZrO.sub.2, Y.sub.2 O.sub.3, stabilized ZrO.sub.2, Al.sub.2 O.sub.3 --TiO.sub.2 and MgO--ZrO.sub.2.
- 19. The method in accordance with claim 17 wherein said bond layer has a thickness in the range of 0.1 to 5 mils.
- 20. The method in accordance with claim 17 wherein said refractory layer has a thickness in the range of 2 to 30 mils.
- 21. The method in accordance with claim 17 wherein said bond coating is comprised of an alloy selected from the group consisting of Cr--Ni--Al alloy and Cr--Ni alloy.
- 22. The method in accordance with claim 17 wherein said refractory layer is thermally applied.
- 23. The method in accordance with claim 17 wherein said refractory layer is applied by flame spray or plasma spray.
- 24. The method in accordance with claim 17 wherein said refractory layer has pores sealed using a material selected from the group consisting of pyrolyzed aluminum and hydrolyzed titanium tetrachloride or silicon tetrachloride.
- 25. An improved composite suitable for use in contacting molten aluminum, the composite comprised of:
- (a) a base layer of a carbonaceous material having a coefficient of thermal expansion of less than 5.times.10.sup.-6 in/in/.degree. F.;
- (b) a bond coating applied to a surface of said base layer, the bond coating having a coefficient of thermal expansion of less than 10.times.10.sup.-6 in/in/.degree. F.; and
- (c) a refractory layer bonded to said bond coating, the refractory layer resistant to attack by said molten aluminum, said refractory layer and said carbonaceous material having a ratio of coefficient of thermal expansion in the range of 5:1 to 1:5.
- 26. The composite in accordance with claim 25 wherein said carbonaceous material is graphite.
- 27. The composite in accordance with claim 25 wherein said refractory coating is a coating selected from one of the group consisting of Al.sub.2 O.sub.3, ZrO.sub.2, Y.sub.2 O.sub.3, stabilized ZrO.sub.2, Al.sub.2 O.sub.3 --TiO.sub.2 and MgO--ZrO.sub.2.
- 28. The composite in accordance with claim 2 wherein said bond layer has a thickness in the range of 0.1 to 5 mils.
- 29. The composite in accordance with claim 25 wherein said refractory layer has a thickness in the range of 4 to 22 mils.
- 30. The composite in accordance with claim 2 wherein said bond layer is comprised of an alloy selected from the group consisting of Cr--Ni--Al alloy and Cr--Ni alloy.
- 31. The composite in accordance with claim 25 wherein said refractory layer is a thermally applied layer.
- 32. The composite in accordance with claim 25 wherein said refractory layer is a flame or plasma sprayed layer.
- 33. The composite in accordance with claim 25 wherein said refractory layer has a porosity of 1 to 20%.
- 34. The composite in accordance with claim 33 wherein said seal is applied to provide pore closure to prevent intrusion.
- 35. The composite in accordance with claim 25 wherein said refractory layer has pores sealed using a material selected from the group consisting of pyrolyzed aluminum and hydrolyzed titanium tetrachloride or silicon tetrachloride.
- 36. An improved composite suitable for use in contacting molten aluminum having improved resistance to degradation at the molten aluminum surface, the composite comprised of:
- (a) a base layer of carbonaceous material having a coefficient of thermal expansion of less than 5.times.10.sup.-6 in/in/.degree. F.; and
- (b) a refractory layer thermally applied to said bond coat, the refractory layer selected from one of the group consisting of Al.sub.2 O.sub.3, ZrO.sub.2, Y.sub.2 O.sub.3, stabilized ZrO.sub.2, Al.sub.2 O.sub.3 --TiO.sub.2 and MgO--ZrO.sub.2, said refractory layer and said carbonaceous material having a ratio of coefficient of thermal expansion in the range of 5:1 to 1:5, the refractory having pores, said pores sealed to prevent intrusion of said pores by vapors.
- 37. The composite in accordance with claim 36 wherein said pores are sealed with a sealant selected from the group consisting of pyrolyzed aluminum and hydrolyzed titanium tetrachloride or silicon tetrachloride.
- 38. The composite in accordance with claim 36 wherein said bond layer has a thickness in the range of 0.1 to 5 mils.
- 39. The composite in accordance with claim 36 wherein said refractory layer has a thickness in the range of 4 to 22 mils.
- 40. The composite in accordance with claim 36 wherein said bond layer is comprised of an alloy selected from the group consisting of Cr--Ni--Al alloy and Cr--Ni alloy.
CROSS REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of U.S. Ser. No. 09/105,942, filed, Jun. 26, 1998, which is a continuation-in-part of U.S. Ser. No. 09/059,924, filed Apr. 14, 1998, now U.S. Pat. No. 6,066,289 which is a continuation-in-part of U.S. Ser. No. 08/882,921, filed Jun. 26, 1997 now U.S. Pat. No. 5,968,223.
US Referenced Citations (18)
Foreign Referenced Citations (3)
Number |
Date |
Country |
1107378 |
Sep 1978 |
JPX |
0420889 |
Mar 1974 |
SUX |
0586343 |
Dec 1977 |
SUX |
Non-Patent Literature Citations (1)
Entry |
Derwent Abstract of Japanese Document 57209885A Acc No 1983-13241k Dec. 23, 1982. |
Continuation in Parts (3)
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Number |
Date |
Country |
Parent |
105942 |
Jun 1998 |
|
Parent |
059924 |
Apr 1998 |
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Parent |
882921 |
Jun 1997 |
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