Rapid processing of laminar composite components
US-12180120-B2 · Dec 31, 2024 · US
US10279573B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10279573-B2 |
| Application number | US-201615297488-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 19, 2016 |
| Priority date | Mar 31, 2015 |
| Publication date | May 7, 2019 |
| Grant date | May 7, 2019 |
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 manufacturing method of a honeycomb structure includes a forming step of forming a quadrangular pillar-shaped honeycomb formed body, a firing step of firing the honeycomb formed body and forming a quadrangular pillar-shaped honeycomb fired body, a coating step of coating at least a part of side surfaces of the honeycomb fired body with a paste-like bonding material, a honeycomb block body preparing step of bonding the plurality of honeycomb fired bodies while performing pressurizing, to prepare a honeycomb block body, and a circumference grinding step of grinding a circumferential surface of the honeycomb block body and obtaining the honeycomb structure, and in the honeycomb block body preparing step, the bonding is performed without interposing any member other than the bonding material between the honeycomb fired bodies, and the bonding material has a shear thinning property.
Opening claim text (preview).
The invention claimed is: 1. A manufacturing method of a honeycomb structure which comprises: a forming step of forming a forming material to form a quadrangular pillar honeycomb formed body having partition walls defining and forming a plurality of cells which become through channels for fluid and extend from one end face to the other end face; a firing step of firing the honeycomb formed body obtained by the forming step and forming a quadrangular pillar honeycomb fired body; a coating step of coating a side surface of at least a part of the honeycomb fired body with a paste bonding material; a honeycomb block body preparing step of bringing the side surfaces of the plurality of honeycomb fired bodies into contact with one another and performing bonding while performing pressurizing, to prepare a honeycomb block body in which the plurality of honeycomb fired bodies are laminated; and a grinding step of grinding a circumferential portion of the honeycomb block body and obtaining the honeycomb structure, wherein in the honeycomb block body preparing step, the bonding is performed without interposing any member other than the bonding material between the honeycomb fired bodies, wherein the bonding material contains a thickener, and wherein the bonding material has a shear thinning property and a viscosity of from 1500 to 5000 poise. 2. The manufacturing method of the honeycomb structure according to claim 1 , wherein the coating step and the honeycomb block body preparing step are performed without performing a mask treatment on the end faces of the honeycomb fired body. 3. The manufacturing method of the honeycomb structure according to claim 1 , wherein in the coating step, the side surface of the honeycomb fired body before coated with the bonding material is not coated with an undercoat material. 4. The manufacturing method of the honeycomb structure according to claim 1 , wherein a thixotropic index indicating the shear thinning property of the bonding material is in a range of 18 to 30. 5. The manufacturing method of the honeycomb structure according to claim 1 , wherein the bonding material contains at least two types of pore forming agents. 6. A bonding material for use in the manufacturing method of the honeycomb structure according to claim 1 , wherein the thickener is at least one of xanthan gum, diutan gum, and a synthetic inorganic polymer with a saponite structure. 7. The bonding material according to claim 6 , wherein a thixotropic index indicating the shear thinning property of the bonding material is in a range of 18 to 30.
Ceramic interlayers · CPC title
consisting of glass or ceramic material · CPC title
Magnesium oxides or oxide-forming salts thereof · CPC title
lining the outer wall of hollow objects, e.g. pipes · CPC title
Carbide interlayers, e.g. silicon carbide interlayers · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.