Intake duct for internal combustion engine
US-11319868-B2 · May 3, 2022 · US
US11156150B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11156150-B2 |
| Application number | US-202016915521-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 29, 2020 |
| Priority date | Jul 5, 2019 |
| Publication date | Oct 26, 2021 |
| Grant date | Oct 26, 2021 |
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An inlet duct includes a tubular main body formed by a compression-molded fibrous molded body. The main body includes an alternate layout region in which an air-impermeable high-compression portion and an air-permeable low-compression portion hat is compression-molded at a lower compressibility than a compressibility of the high-compression portion are alternately laid out in an axial direction of the main body. The alternate layout region is configured such that an arbitrary pair of points at an equal distance in the axial direction to a central position in an upstream region and a downstream region of the alternate layout region include only points that are both located in the low-compression portions and points one of which is located in the low-compression portion and the other one of which is located in the high-compression portion.
Opening claim text (preview).
The invention claimed is: 1. An inlet duct for an internal combustion engine, the inlet duct comprising a tubular main body formed by a compression-molded fibrous molded body, wherein the main body includes an alternate layout region in which an air-impermeable high-compression portion and an air-permeable low-compression portion that is compression-molded at a lower compressibility than a compressibility of the high-compression portion are alternately laid out in an axial direction of the main body, the alternate layout region is divided into an upstream region and a downstream region of a central position in an axial direction of the inlet duct in a flow direction of intake air, and the alternate layout region is configured such that an arbitrary pair of points at an equal distance in the axial direction to the central position in the upstream region and the downstream region include only points that are both located in the low-compression portions and points one of which is located in the low-compression portion and the other one of which is located in the high-compression portion. 2. The inlet duct according to claim 1 , wherein the low-compression portion is a first low-compression portion, a part of the main body in a circumferential direction is provided with an air-permeable second low-compression portion that is extended in the axial direction and compression-molded at a lower compressibility than the compressibility of the high-compression portion, and the alternate layout region is adjacent to the second low-compression portion in the circumferential direction of the main body. 3. The inlet duct according to claim 2 , wherein the alternate layout region is one of a plurality of alternate layout regions, the alternate layout regions are spaced apart from one another by a predetermined distance in the circumferential direction of the main body, and the second low-compression portion is arranged between adjacent ones of the alternate layout regions in the circumferential direction. 4. The inlet duct according to claim 1 , wherein the alternate layout region is one of a plurality of alternate layout regions, and the alternate layout regions are spaced apart from one another by a predetermined distance in a circumferential direction of the main body. 5. The inlet duct according to claim 1 , wherein the main body includes a first halved body and a second halved body that have a half cylinder shape, and the high-compression portions are arranged differently in the first halved body and the second halved body on a downstream side or an upstream side of the central position.
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