Return stage of a multi-stage turbocompressor or turboexpander having rough wall surfaces
A turbo compressor and turbine technology, which is applied to machines/engines, components of pumping devices for elastic fluids, mechanical equipment, etc., can solve the problems of high processing costs and other problems, and achieve the effect of reducing pressure loss
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[0030] figure 1 A schematic longitudinal section through the return stage RS of the turbocompressor TCO from the first impeller IMP1 to the second impeller IMP2 is shown.
[0031] The two impellers IMP1 , IMP2 are integral parts of the rotor R, wherein the impellers IMP1 , IMP2 are mounted on a shaft SH extending along the axis X in a non-positive manner. The rotor R is surrounded by flow-guiding, stationary components, of which the return stage RS is shown here. A multi-stage turbine generally comprises a plurality of return stages RS, viewed in the flow direction from the first impeller IMP1, which turn the process fluid PF by 180° immediately after the radial diffuser section and towards the radially inward back-directed and then diverted in the axial direction in order to feed the process fluid PF to the second downstream impeller IMP2, which in the case of the turbocompressor TCO draws the process fluid PF axially and radially output it.
[0032] The return stage gener...
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