Turbocompressor with adapted meridian contour of blades and compressor wall
A technology of turbo compressors, compressors, applied in the direction of machines/engines, components of pumping devices for elastic fluids, mechanical equipment, etc.
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[0025] exist figure 1 with figure 2 The turbocompressor 1 schematically shows a section cut along a meridian plane. Only the area of the turbocompressor relevant to the invention is shown; otherwise, a person skilled in the art can reconstruct it from structures known from the prior art.
[0026] The turbocompressor 1 comprises a compressor housing 2 and a compressor wheel 4 having blades 5 distributed in the circumferential direction. The compressor wheel is Figure 4 shown in . Said compressor wheel 4 is driven by an electric motor (not shown) in rotation about an axis of rotation RA. The compressor wheel 4 sucks in air axially and discharges it radially. The corresponding main airflow HS is at figure 2 shown in .
[0027] Between the fixed housing wall 3 of the compressor housing 2 and the blade upper edges of the blades 5 there is provided a top gap 7 which enables the rotation of the compressor wheel 4 . The upper edges of the blades are not covered, ie not co...
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