| 摘要 |
Representative embodiments provide for a flow laminarizing device including a plurality of walls defining a plurality of passageways, each passageway defining a hexagonal cross-sectional area and configured to permit fluid flow there through, a casing configured to mechanically support the plurality of walls, and at least one support extension mechanically coupled to the casing, the at least one support extension and the casing cooperatively configured to support the flow laminarizing device in a substantially fixed slidingly received position relative to a fluid flow port of a fluid impelling device. A method includes the steps of decoupling an air line from a turbocharger, installing a flow laminarizing device in fluid communication with the turbocharger, and recoupling the air line to the turbocharger.
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