STABILIZER CHANNEL OF A COMPRESSOR

The invention relates to a stabilizer channel (10), in particular of a radial compressor or diagonal compressor, having an annular stabilizer chamber (12) which encloses a main flow channel (13) in the intake region of a compressor wheel (21) and is delimited from the main flow channel (13) by an annular bridge (14). The annular stabilizer channel (12) is connected to the main flow channel (13) via a downstream flow inlet (15) and an upstream flow outlet (16). At least one separating element (T) is arranged in at least one of the flow inlet (15) and the flow outlet (16), with the result that an inflow into the annular stabilizer chamber (12) and/or an outflow out of the annular stabilizer chamber (12) are/is split transversely with respect to the main flow direction (1) of the main flow channel (13). Furthermore, at least one flow guiding element (17) is arranged in at least one of the flow inlet (15) and the flow outlet (16). The invention furthermore relates to a compressor, in particular a radial compressor or diagonal compressor, comprising the stabilizer channel according to the invention and to a turbomachine, in particular a turbocharger, comprising the compressor.