Process and device for producing molded foam
US-2020223122-A1 · Jul 16, 2020 · US
US11504891B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11504891-B2 |
| Application number | US-201917270135-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 23, 2019 |
| Priority date | Aug 27, 2018 |
| Publication date | Nov 22, 2022 |
| Grant date | Nov 22, 2022 |
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The present disclosure relates to a screw of an injection molding machine in which a heating cylinder is formed with a first compression section, a starvation section, and a second compression section, and in which an inert gas is to be introduced into the starvation section. At a portion of the screw corresponding to the first compression section, a barrier flight as a double flight including a combination of a main flight and a sub-flight having a lead angle larger than that of the main flight is formed, and a dam flight having a predetermined-width ring shape is formed, downstream of, i.e., in front of the barrier flight. A seal structure to prevent backflow of the resin may be provided between the dam flight and the starvation section.
Opening claim text (preview).
The invention claimed is: 1. A screw of an injection molding machine for foam molding comprising: a main flight; a sub-flight having a lead angle larger than that of the main flight; a barrier flight comprising the main flight and the sub-flight; a dam flight having a ring shape formed in front of the barrier flight; a first compression section in which a resin is to be compressed; a starvation section in which a pressure of the resin is to be lowered; and a second compression section in which the resin is to be compressed, wherein the first compression section, the starvation section and the second compression section are provided from a rear side to a front side of the screw in a heating cylinder, wherein the starvation section is configured to have a gas introduced therein, and wherein the barrier flight and the dam flight are provided at a portion corresponding to the first compression section of the screw. 2. The screw according to claim 1 , wherein the screw is provided with a predetermined seal structure to prevent backflow of the resin between the dam flight and the starvation section. 3. The screw according to claim 2 , wherein the seal structure comprises: a seal configured to liquid-tightly separate the first compression section from the starvation section; a communication passage configured to communicate the first compression section and the starvation section; and a valve mechanism configured to close the communication passage and cause a molten resin to flow into the starvation section when the molten resin in the first compression section exceeds a predetermined pressure. 4. The screw according to claim 2 , wherein the seal structure comprises: a diameter-reduced portion in which a diameter of the screw is reduced; and a seal ring which is fitted to the diameter-reduced portion with a predetermined gap therebetween and which is liquid-tightly slid with respect to a bore of the heating cylinder, wherein a tapered surface is formed on the diameter-reduced portion to block communication between the first compression section and the starvation section when the seal ring is seated. 5. An injection molding machine comprising the screw according to claim 1 , wherein the heating cylinder is provided with an introduction port which introduces gas at a predetermined position corresponding to the starvation section. 6. The screw according to claim 1 , wherein the dam flight is formed in front of the barrier flight continuous with the barrier flight or at a predetermined interval with respect to the barrier flight.
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