Ceramic base material, ceramic support, and separation membrane complex
US-2024399316-A1 · Dec 5, 2024 · US
US2019300440A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2019300440-A1 |
| Application number | US-201916363155-A |
| Country | US |
| Kind code | A1 |
| Filing date | Mar 25, 2019 |
| Priority date | Mar 30, 2018 |
| Publication date | Oct 3, 2019 |
| Grant date | — |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A coating material for a silicon carbide-based honeycomb structure, the coating material including from 20 to 75% by mass of ceramic powder (A), the ceramic powder (A) including from 55 to 95% by mass of silicon carbide and from 5 to 30% by mass of silicon dioxide as chemical components.
Opening claim text (preview).
What is claimed is: 1 . A coating material for a silicon carbide-based honeycomb structure, the coating material comprising from 20 to 75% by mass of ceramic powder (A), the ceramic powder (A) comprising from 55 to 95% by mass of silicon carbide and from 5 to 30% by mass of silicon dioxide as chemical components. 2 . The coating material according to claim 1 , wherein the ceramic powder (A) has a D50 on volume basis of from 8 to 30 μm, based on a particle size distribution measurement by a laser diffraction/scattering method. 3 . The coating material according to claim 1 , wherein the ceramic powder (A) has a D10 on volume basis of from 1 to 4 μm, and D90 of from 20 to 75 μm (D90>D50), based on a particle size distribution measurement by a laser diffraction/scattering method. 4 . The coating material according to claim 1 , wherein the ceramic powder (A) is grinding scrap or crushed powder of the silicon carbide-based honeycomb structure. 5 . The coating material according to claim 1 , further comprising from 20 to 50% by mass of white or light colored ceramic powder (B). 6 . The coating material according to claim 5 , wherein the ceramic powder (B) comprises at least one selected from the group consisting of cordierite, silicon nitride, alumina, mullite, zirconia, zirconium phosphate, titania and aluminum titanate. 7 . The coating material according to claim 5 , wherein the ceramic powder (B) has a D50 on volume basis of from 1 to 40 μm, based on a particle size distribution measurement by a laser diffraction/scattering method. 8 . The coating material according to claim 1 , wherein a ratio of a thermal expansion coefficient after drying the coating material at 600° C. for 30 minutes to a thermal expansion coefficient of the silicon carbide honeycomb structure is from 0.8 to 1.1. 9 . The coating material according to claim 1 , wherein the coating material further comprises from 0.1 to 4% of hollow particles containing an organic substance, and wherein the hollow particles have a D50 on volume basis of from 35 to 55 μm, based on a particle size distribution measurement by a laser diffraction/scattering method. 10 . An outer periphery-coated silicon carbide-based honeycomb structure, comprising: a silicon carbide-based honeycomb structure; and an outer periphery-coated layer covering an outer periphery of the silicon carbide-based honeycomb structure, wherein the outer periphery-coated layer comprises from 20 to 75% by mass of ceramic powder (A), the ceramic powder (A) comprising from 55 to 95% by mass of silicon carbide and from 5 to 30% by mass of silicon dioxide as chemical components. 11 . The outer periphery-coated silicon carbide-based honeycomb structure according to claim 10 , wherein the ceramic powder (A) has the same composition as that of the silicon carbide-based honeycomb structure. 12 . The outer periphery-coated silicon carbide-based honeycomb structure according to claim 10 , wherein a ratio of a thermal expansion coefficient of the outer periphery-coated layer to a thermal expansion coefficient of the silicon carbide-based honeycomb structure is from 0.8 to 1.1. 13 . A method for coating an outer periphery of a silicon carbide-based honeycomb structure, the method comprising: applying the coating material according to claim 1 onto an outer periphery of the silicon carbide-based honeycomb structure and drying the applied coating material to form an outer peripheral coated layer.
Alumino-silicates other than clay, e.g. mullite · CPC title
Composites · CPC title
Silicon carbide · CPC title
Silicon oxide, silicic acids or oxide forming salts thereof, e.g. silica sol, fused silica, silica fume, cristobalite, quartz or flint · CPC title
Titanates, not containing zirconia · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.