Turbocharger impeller, method of manufacturing the same, turbocharger, and turbocharger unit
US-2015354359-A1 · Dec 10, 2015 · US
US9140271B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9140271-B2 |
| Application number | US-201013381064-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 10, 2010 |
| Priority date | Dec 2, 2009 |
| Publication date | Sep 22, 2015 |
| Grant date | Sep 22, 2015 |
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Interference of a leakage vortex flow generated at the tip end side of the full blade with the leading edge of the splitter blade is avoided and high pressure ratio and enhanced efficiency can be achieved. A throat of am impeller is formed so that a distance from a leading edge of a rear side full blade on the rear side of the rotation direction of the compressor to a front side full blade adjacent to the rear side full blade is minimized, and the leading edge of the splitter blade is placed in a fluid flow streaming along the flow passage between the mutually adjacent full blades, on the downstream side of a leakage vortex line formed to connect the middle location of the throat to the leading edge of the front side full blade.
Opening claim text (preview).
The invention claimed is: 1. An impeller of a centrifugal compressor, the impeller comprising: a plurality of full blades provided from a fluid inlet side to a fluid outlet side on a hub surface, the full blades being provided side by side; a plurality of splitter blades provided in a flow passage formed between a pair of the mutual adjacent full blades from a part way of the flow passage to the outlet side, wherein, in a cross section view depicting a geometry along a tip e…
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
Mechanical Engineering · mapped topic
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