Low CTE cordierite honeycomb article and method of manufacturing same
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B32B-003/12
B01D-039/06
B28B-003/20
C04B-035/64
출원번호
UP-0314431
(2005-12-20)
등록번호
US-7744980
(2010-07-19)
발명자
/ 주소
Boorom, James Albert
He, Lin
Merkel, Gregory Albert
출원인 / 주소
Corning Incorporated
대리인 / 주소
Homa, Joseph M.
인용정보
피인용 횟수 :
5인용 특허 :
29
초록▼
Disclosed is a honeycomb ceramic article that exhibits a primary crystalline phase of cordierite having a coefficient of thermal expansion (CTE), wherein CTE<1.5×10−7/° C. over the temperature range of about 25° C. to about 800° C.; a total porosity, P, of at least 28
Disclosed is a honeycomb ceramic article that exhibits a primary crystalline phase of cordierite having a coefficient of thermal expansion (CTE), wherein CTE<1.5×10−7/° C. over the temperature range of about 25° C. to about 800° C.; a total porosity, P, of at least 28%, a transverse I-ratio, IT, of less than 0.92; and a pore size distribution wherein at least 60% of the total pore volume is comprised of pores having diameters between 0.5 μm and 5.0 μm. Also provided is a ceramic honeycomb article comprising a phase of cordierite and exhibiting a mean CTE <1.0×10−7/° C. (from 25 to 800° C.) in at least one direction, and 28%≦P≦33%. Methods of manufacturing ceramic articles comprising the aforementioned cordierite compositions are also disclosed.
대표청구항▼
What is claimed is: 1. A ceramic honeycomb article, comprising: a ceramic with a phase of cordierite which exhibits a coefficient of thermal expansion in an axial direction <1.5×10−7/° C. across the temperature range from 25° C. to 800° C.; a total porosity, P, of
What is claimed is: 1. A ceramic honeycomb article, comprising: a ceramic with a phase of cordierite which exhibits a coefficient of thermal expansion in an axial direction <1.5×10−7/° C. across the temperature range from 25° C. to 800° C.; a total porosity, P, of ≧28%; an transverse I ratio, IT, of <0.87; and a pore size distribution wherein ≧60% of a total pore volume of the ceramic has a pore diameter of between 0.5 μm to 5 μm. 2. The ceramic honeycomb article of claim 1 wherein the ceramic consists essentially of: from about 49 to about 53 percent by weight SiO2, from about 33 to about 38 percent by weight Al2O3, and from about 12 to about 16 percent by weight MgO. 3. The ceramic honeycomb article of claim 1, further comprising a mean pore diameter, d50, in the range from 2.0 μm to 4.0 μm. 4. The ceramic honeycomb article of claim 1 wherein the coefficient of thermal expansion is ≦1.0×10−7/° C. across the temperature range from 25° C. to 800° C. 5. The ceramic honeycomb article of claim 4 wherein the coefficient of thermal expansion is ≦0.8×10−7/° C. across the temperature range from 25° C. to 800° C. 6. The ceramic honeycomb article of claim 5 wherein the coefficient of thermal expansion is ≦0.5×10−7/° C. across the temperature range from 25° C. to 800° C. 7. The ceramic honeycomb article of claim 1 wherein P≦40%. 8. The ceramic honeycomb article of claim 1 wherein P≧30%. 9. The ceramic honeycomb article of claim 8 wherein 30%≦P≦36%. 10. The ceramic honeycomb article of claim 1 wherein P≦33%. 11. The ceramic honeycomb article of claim 1, further comprising a modulus of rupture strength, MOR, wherein MOR>300 psi for a 600/4 cell geometry. 12. The ceramic article of claim 11, further comprising a modulus of rupture strength, MOR, wherein MOR>350 psi for a 600/4 cell geometry. 13. The ceramic article of claim 12, further comprising a modulus of rupture strength, MOR, wherein MOR>400 psi for a 600/4 cell geometry. 14. The ceramic article of claim 1, further comprising d90<15 μm. 15. The ceramic article of claim 1, further comprising: CTE≦1.0×10−7/° C.; and P≧30%. 16. A ceramic honeycomb article, comprising: a ceramic with a phase of cordierite which exhibits a transverse I ratio, IT, of ≦0.87; a coefficient of thermal expansion in an axial direction <1.0×10−7/° C. across the temperature range from 25° C. to 800° C.; and a total porosity, P, of 28%≦P≦33%. 17. The ceramic honeycomb article of claim 16, wherein the ceramic consists essentially of: from about 49 to about 53 percent by weight SiO2, from about 33 to about 38 percent by weight Al2O3, and from about 12 to about 16 percent by weight MgO. 18. The ceramic honeycomb article of claim 16, further comprising a mean pore diameter, d50, in the range from 2.0 μm to 6.0 μm. 19. The ceramic honeycomb article of claim 16, wherein the coefficient of thermal expansion is ≦0.9×10−7/° C. across the temperature range from 25° C. to 800° C. 20. The ceramic honeycomb article of claim 16, wherein the coefficient of thermal expansion is ≦0.3×10−7/° C. across the temperature range from 25° C. to 800° C. 21. The ceramic honeycomb article of claim 16, wherein the coefficient of thermal expansion is ≦−0.4×10−7/° C. across the temperature range from 25° C. to 800° C. 22. The ceramic honeycomb article of claim 16, wherein P≧30%. 23. The ceramic honeycomb article of claim 16, exhibiting a modulus of rupture strength, MOR, wherein MOR>300 psi for a 600/4 cell geometry. 24. The ceramic article of claim 16, further comprising: CTE≦0.5×107/° C.; and P≧30%. 25. A method of manufacturing a ceramic honeycomb article having a sintered phase cordierite composition, comprising the steps of: providing a plasticized cordierite precursor batch composition having an inorganic powder batch composition containing at least one talc source having a mean particle size of at least 8 μm and a morphology index of not more than 0.70; one or more alumina-forming sources, wherein the alumina-forming sources have a weighted average median particle size that does not exceed 5 μm; and at least 20 weight percent of an alumino-silicate source comprising at least one raw kaolin and, optionally, at least one calcined kaolin, wherein the weighted average median particle size of the kaolin+calcined kaolin mixture does not exceed 6 μm; and a binder system; forming an extruded green body from the plasticized cordierite precursor batch composition; and firing the green body under conditions effective to convert the green body into a ceramic article comprising a sintered phase cordierite composition, wherein the sintered phase cordierite composition exhibits a coefficient of thermal expansion, CTE, in an axial direction <1.5×10−7/° C. across a temperature range from 25° C. to 800° C.; and a total porosity, P, of ≧28%. 26. The method of claim 25, wherein the conditions effective further comprise: i) firing the green body at a temperature of at least 1390° C. when the weighted average median particle size of the alumina-forming sources is less than 1 μm; ii) firing the green body at a temperature of at least 1400° C.; when the weighted average median particle size of the alumina-forming source is in the range of from 1 μm to 3 μm; and iii) firing the green body at a temperature of at least 1405° C. when the weighted average median particle size of the alumina-forming source is greater than 3 μm. 27. The method of claim 25, further comprising at least one dispersible alumina-forming source having a dispersed median particle size of not more than 0.5 μm. 28. The method of claim 27, wherein the dispersible alumina-forming source is present in an amount of from 1 wt % to 5 wt % of the inorganic powder batch composition. 29. The method of claim 27, wherein the dispersible alumina-forming source has a specific surface area of at least 50 m2/g. 30. The method of claim 25, wherein the talc source has a morphology index of at least 0.40 and not more than 0.70. 31. The method of claim 25, wherein the talc source has a morphology index of at least 0.50 and not more than 0.70. 32. The method of claim 25, wherein the sintered phase cordierite composition has a mean pore diameter in the range of from 2.0 μm to 6.0 μm. 33. The method of claim 25, wherein the sintered phase cordierite composition comprises: 28%≦P≦40%, and CTE <1.5×10−7/° C. 34. The method of claim 25, wherein the sintered phase cordierite composition comprises: 28%≦P≦33%, and CTE<1.0×10−7/° C. 35. The method of claim 25, wherein the plasticized cordierite precursor batch composition does not comprise a non-crystalline silica. 36. The ceramic honeycomb article of claim 1 wherein the ceramic exhibits an axial I ratio, IA, of >0.41. 37. The ceramic honeycomb article of claim 1 wherein the ceramic exhibits an axial I ratio, IA, of >0.42. 38. The ceramic honeycomb article of claim 1 wherein the ceramic exhibits an axial I ratio, IA, of >0.46. 39. The ceramic honeycomb article of claim 1, further comprising a mean pore diameter, d50, greater than 2.0 μm. 40. The ceramic honeycomb article of claim 1 wherein P≧30.5%. 41. The ceramic honeycomb article of claim 16, further comprising a mean pore diameter, d50, greater than 2.0 μm.
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이 특허에 인용된 특허 (29)
Hamanaka Toshiyuki (Suzuka JPX) Watanabe Keiichiro (Nagoya JPX) Harada Takashi (Nagoya JPX) Asami Seiichi (Okazaki JPX), Catalyst carrier of cordierite honeycomb structure and method of producing the same.
Beall Douglas M. (Corning NY) DeLiso Evelyn M. (Elmira NY) Guile Donald L. (Horseheads NY) Murtagh Martin J. (Trumansburg NY), Fabrication of cordierite bodies.
Andou Yosiyasu,JPX ; Koike Kazuhiko,JPX ; Nakanishi Tomohiko,JPX, Process for producing cordierite honeycomb structural body and honeycomb structural body molding aid.
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