FIELD: machine building.
SUBSTANCE: invention relates to the turbomachine assembly, in particular to the integral turbo-expander turbine assembly. Turbomachine assembly comprises the following: the shaft, the radial gas expander, which is held on the shaft between the first and second bearing, and the compressor, which is held on the shaft in a cantilever position adjacent to one of the mentioned bearings, where the compressor comprises a plurality of movable input nozzles, and the radial gas expander comprises a plurality of movable guide vanes.
EFFECT: invention is aimed at increasing device productivity.
10 cl, 3 dwg
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Authors
Dates
2018-09-26—Published
2015-03-09—Filed