Method and apparatus for modularized inlet silencer baffles
US-2018073432-A1 · Mar 15, 2018 · US
US10468010B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10468010-B2 |
| Application number | US-201715590673-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 9, 2017 |
| Priority date | May 9, 2017 |
| Publication date | Nov 5, 2019 |
| Grant date | Nov 5, 2019 |
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An apparatus is provided. The apparatus includes a plurality of flow guiding structures spatially aligned in a first row, each of the plurality of flow guiding structures comprising a fin-shape to funnel airflow at a trailing edge of each of the plurality of flow guiding structures. The apparatus also includes a plurality of flow separating structures spatially aligned in a second row interleaved between each of the plurality of flow guiding structures, each of the plurality of flow separating structures comprising a fin-shape configured to split airflow received from the plurality of flow guiding structures.
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The invention claimed is: 1. An apparatus comprising: a plurality of flow guiding structures spatially aligned in a first row, each of the plurality of flow guiding structures comprising a fin to funnel airflow at a trailing edge of each of the plurality of flow guiding structures; and a plurality of flow separating structures spatially aligned in a second row partially interleaved between each of the plurality of flow guiding structures, each of the plurality of flow separating structures comprising a fin configured to split airflow received from the plurality of flow guiding structures, wherein a leading edge of each of the plurality of flow separating structure is aligned with a midpoint of a distance between two adjacent storage arrays. 2. The apparatus of claim 1 , wherein each of the plurality of flow separating structures comprises a supporting rod encased by a sound absorber material. 3. The apparatus of claim 1 , wherein each of the plurality of flow guiding structures comprises a supporting rod encased by a sound absorber material. 4. The apparatus of claim 1 , wherein the fin of each of the plurality of flow separating structures comprises a rounded leading edge and a sharp trailing edge. 5. The apparatus of claim 4 , wherein the rounded leading edge comprises a supporting feature. 6. The apparatus of claim 1 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a sharp trailing edge. 7. The apparatus of claim 1 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a rounded trailing edge. 8. A computing device comprising: a housing having an inlet side, an outlet side, a first sidewall, and a second sidewall, the first sidewall and the second sidewall extending from the inlet side to the outlet side; at least one row of drive bays extending at least partially from the first sidewall to the second sidewall, the at least one row of drive bays configured to receive a plurality of hard disk drives and to provide a plurality of gaps between the plurality of hard disk drives; a plurality of flow guiding structures disposed between the at least one row of drive bays and the outlet side, wherein: each of the plurality of flow guiding structures is directly coupled to a corresponding one of the plurality of hard disk drives, and each of the plurality of flow guiding structures comprises a fin to funnel airflow through the plurality of gaps between the plurality of hard disk drives to a trailing edge; and a plurality of flow separating structures interleaved between each of the plurality of flow guiding structures, each of the plurality of flow separating structures comprising a fin configured to split airflow received from the plurality of flow guiding structures. 9. The computing device of claim 8 , wherein each of the plurality of flow separating structures comprises a supporting rod encased by a sound absorber material. 10. The computing device of claim 8 , wherein each of the plurality of flow guiding structures comprises a supporting rod encased by a sound absorber material. 11. The computing device of claim 8 , wherein the fin of each of the plurality of flow separating structures comprises a rounded leading edge and a sharp trailing edge. 12. The computing device of claim 11 , wherein the rounded leading edge comprises a supporting feature. 13. The computing device of claim 8 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a sharp trailing edge. 14. The computing device of claim 8 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a rounded trailing edge. 15. A storage array module, comprising: a plurality of storage arrays; a plurality of flow guiding structures spatially aligned in a first row, each of the plurality of flow guiding structures comprising a fin to funnel airflow at a trailing edge of each of the plurality of flow guiding structures, wherein each of the plurality of flow guiding structures is configured to directly couple to a corresponding one of the plurality of storage arrays; and a plurality of flow separating structures spatially aligned in a second row partially interleaved between each of the plurality of flow guiding structures, each of the plurality of flow separating structures comprising a fin configured to split airflow received from the plurality of flow guiding structures. 16. The storage array module of claim 15 , wherein a leading edge of each of the plurality of flow separating structure is aligned with a midpoint of a distance between two adjacent storage arrays of the plurality of storage arrays. 17. The storage array module of claim 15 , wherein the fin of each of the plurality of flow separating structures comprises a rounded leading edge and a sharp trailing edge. 18. The storage array module of claim 17 , wherein the rounded leading edge comprises a supporting feature. 19. The storage array module of claim 15 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a sharp trailing edge. 20. The storage array module of claim 15 , wherein the trailing edge of each of the plurality of flow guiding structures comprises a rounded trailing edge.
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