Device and method for the homogenisation of plastics material melts
US-2015266208-A1 · Sep 24, 2015 · US
US11938657B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11938657-B2 |
| Application number | US-201916548132-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 22, 2019 |
| Priority date | Feb 22, 2017 |
| Publication date | Mar 26, 2024 |
| Grant date | Mar 26, 2024 |
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 multi-screw kneader is configured to exhibit an extensional flow function before and behind holes of a disk-shaped segment and a method for producing a nano-composite uses the multi-screw kneader. The multi-screw kneader includes a plurality of kneading screws and the disk-shaped segment in a barrel. The disk-shaped segment partitions the inside of the barrel downstream of a part for supplying a kneading material and includes shaft receiving parts through which rotating shafts of the kneading screws are to rotatably pass and the holes are defined in a periphery of the shaft penetrating parts and are configured to serve as flow channels of the kneading material. The method for producing the nano-composite includes charging nanoparticles as a resin additive using the multi-screw kneader.
Opening claim text (preview).
What is claimed is: 1. A multi-screw kneader comprising: a barrel; an input port for supplying a kneading material into the barrel; a plurality of full-flight screws for transferring the kneading material; and a disk-shaped segment for promoting extensional flow of the kneading material in the barrel, wherein: helical threads of the plurality of full-flight screws extend from a first position at or adjacent to a first terminal end of the barrel to a second position at or adjacent to a second terminal end of the barrel; the disk-shaped segment is fixed in the barrel so as to partition an inside of the barrel; the disk-shaped segment is at an intermediate position of the plurality of full-flight screws and on a downstream side of the input port; the disk-shaped segment has: (i) a disk body with holes configured to serve as flow channels of the kneading material; (ii) a plurality of rolling bearings mounted on the disk body; and (iii) a plurality of rings fitted to the plurality of rolling bearings, respectively, such that mating structures on respective shafts of the plurality of full-flight screws are fitted to mating structures of the plurality of rings, respectively, whereby the disk-shaped segment is configured to suppress leakage of the kneading material between the plurality of rolling bearings; the mating structures of the plurality of rings are holes with cross sections matching the mating structures on the respective shafts of the plurality of full-flight screws, respectively; an upstream shape, an upstream diameter, and an upstream size of each of the plurality of full-flight screws on an upstream side of the disk-shaped segment are the same as a downstream shape, a downstream diameter, and a downstream size of each of the plurality of full-flight screws on a downstream side of the disk-shaped segment, respectively; the disk-shaped segment is adjacent to the helical thread of each of the plurality of full-flight screws on both the upstream side of the disk-shaped segment and the downstream side of the disk-shaped segment; and the holes of the disk body are constantly in communication with both the upstream side of the disk-shaped segment and the downstream side of the disk-shaped segment. 2. The multi-screw kneader according to claim 1 , wherein each of the holes has a diameter of 0.5 mm to 1.5 mm, and the number of the holes is 2 to 64. 3. The multi-screw kneader according to claim 1 , wherein a total area of openings of the holes on a kneading material flow inlet side is 20% or less of an inner cross-sectional area of the barrel. 4. The multi-screw kneader according to claim 1 , wherein the kneading material contains a resin and a resin additive. 5. A method for producing a nano-composite, the method using the multi-screw kneader according to claim 4 and comprising supplying nanoparticles as the resin additive. 6. The method according to claim 5 , wherein the nanoparticles are selected from the group consisting of carbon nanotubes, carbon nanofibers, cellulose nanofibers, graphenes, nanoclays, and carbon blacks. 7. The multi-screw kneader according to claim 1 , wherein the kneading material contains two or more different resins. 8. The multi-screw kneader according to claim 1 , wherein the disk-shaped segment consists of the disk body configured to be fixed in the barrel, the plurality of rolling bearings mounted on the disk body, and the plurality of rings fitted to the plurality of rolling bearings, respectively. 9. The method according to claim 5 , wherein a diameter of each of the holes is within a range of 0.5 mm to 1.5 mm, a depth of each of the holes in an axial direction is within a range such that a ratio of the depth (L) to a diameter (D) of each of the plurality of full-flight screws, L/D, is 1/12 to 1/4, and the number of the holes is within a range of 2 to 64. 10. The multi-screw kneader according to claim 1 , wherein the mating structures of the plurality of rings and the mating structures on the respective shafts of the plurality of full-flight screws are splined structures. 11. The multi-screw kneader according to claim 1 , wherein the plurality of full-flight screws are juxtaposed such that the helical thread of a first of the plurality of full-flight screws is intermeshed with the helical thread of a second of the plurality of full-flight screws. 12. The multi-screw kneader according to claim 1 , wherein the disk-shaped segment has a cross-sectional shape of two circles partially overlapped such that a medial portion of the disk-shaped segment extends fully across an area between the plurality of rolling bearings. 13. A disk-shaped segment for use in a multi-screw kneader including a plurality of full-flight screws for transferring a kneading material in a barrel, helical threads of the plurality of full-flight screws extending from a first position at or adjacent to a first terminal end of the barrel to a second position at or adjacent to a second terminal end of the barrel, the disk-shaped segment being configured to be fixed in the barrel so as to partition an inside of the barrel, the disk-shaped segment being configured to be at an intermediate position of the plurality of full-flight screws and on a downstream side of an input port of the multi-screw kneader for supplying the kneading material into the barrel, an upstream shape, an upstream diameter, and an upstream size of each of the plurality of full-flight screws on an upstream side of the disk-shaped segment being the same as a downstream shape, a downstream diameter, and a downstream size of each of the plurality of full-flight screws on a downstream side of the disk-shaped segment, respectively, and the disk-shaped segment comprising: a disk body with holes configured to serve as flow channels of the kneading material and material; a plurality of rolling bearings mounted on the disk body; a plurality of rings fitted to the plurality of rolling bearings, respectively, such that mating structures on respective shafts of the plurality of full-flight screws are configured to be fitted to mating structures of the plurality of rings, respectively, whereby the disk-shaped segment is configured to suppress leakage of the kneading material between the plurality of rolling bearings, wherein: the mating structures of the plurality of rings are holes with cross sections configured to match the mating structures on the respective shafts of the plurality of full-flight screws, respectively; the disk-shaped segment is configured to be adjacent to the helical thread of each of the plurality of full-flight screws on both the upstream side of the disk-shaped segment and the downstream side of the disk-shaped segment; and the holes of the disk body are constantly in communication with both the upstream side of the disk-shaped segment and the downstream side of the disk-shaped segment. 14. The disk-shaped segment according to claim 13 , wherein the mating structures of the plurality of rings are splined structures. 15. The disk-shaped segment according to claim 13 , wherein the disk-shaped segment has a cross-sectional shape of two circles partially overlapped such that a medial portion of the disk-shaped segment extends fully across an area between the plurality of rolling bearings.
provided with screw parts in addition to other mixing parts, e.g. paddles, gears, discs · CPC title
Parts, e.g. casings, sealings; Accessories, e.g. flow controlling or throttling devices (discharging B29B7/582; feeding B29B7/60) · CPC title
Screws · CPC title
the other mixing parts being discs perpendicular to the screw axis · CPC title
Screws (B29B7/482 takes precedence) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.