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In an exhaust turbocharger for an internal combustion engine including a turbine and a compressor, which is driven by the turbine, wherein the compressor comprises a compressor impeller in a flow duct, a transfer component with flow passages extends radially around the compressor impeller in the axi

In an exhaust turbocharger for an internal combustion engine including a turbine and a compressor, which is driven by the turbine, wherein the compressor comprises a compressor impeller in a flow duct, a transfer component with flow passages extends radially around the compressor impeller in the axial direction of the impeller and provides for communication with the flow duct. To provide for variable adjustment of the effective flow cross-section of the transfer duct, a transfer ring is provided which comprises two component rings, which are rotatable relative to one another.

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1. A compressor for an exhaust turbocharger of an internal combustion engine, said compressor being a radial compressor and including a housing with an axial inlet area and a radial outlet area, a compressor impeller disposed in a compressor flow duct of said housing, a transfer component extending

1. A compressor for an exhaust turbocharger of an internal combustion engine, said compressor being a radial compressor and including a housing with an axial inlet area and a radial outlet area, a compressor impeller disposed in a compressor flow duct of said housing, a transfer component extending around the compressor inlet area of said impeller and including two component rings with transfer slots arranged directly adjacent said impeller and being open toward said impeller over their full axial length so as to be in communication with the compressor flow duct, said component rings being rotatable relative to each other for adjustment of the effective axial flow cross-section of said flow slots between an aligned overlapping position, in which the transfer slots in the two component rings are in alignment, and a blocking position, in which the transfer slots in the component rings are at least partially out of alignment. 2. A compressor according to claim 1, wherein each of said component rings includes a plurality of transfer slots uniformly distributed over the circumference of the component rings. 3. A compressor according to claim 1, wherein the transfer slots extend in the component rings at an angle (α) of 0° to 90° to the circumferential direction. 4. A compressor according to claim 1, wherein the transfer slots extend in the component rings so as to form an angle (α) of 90° to 180° to the circumferential direction. 5. A compressor according to claim 1, wherein the component rings are arranged concentrically and radially, one adjacent the other, so as to form an inner component ring disposed adjacent to the compressor impeller and an outer component ring being remote from the compressor impeller. 6. A compressor according to claim 5, wherein the transfer slots in the outer component ring have a depth which, measured in the radial direction, extends approximately as far as the center of the outer component ring. 7. A compressor according to claim 5, wherein the transfer slots in the inner component ring have a depth which, measured in the radial direction, is between 10% and 50% of the total depth of the transfer slots of the inner and outer component rings. 8. A compressor according to claim 5, wherein the inner component ring is arranged fixed in relation to the housing, and the outer component ring is rotatable around the inner component ring. 9. A compressor according to claim 1, wherein at least one component ring is adjustable by means of an actuating element as a function of the operating condition of the internal combustion engine.