초록 ▼

In an exhaust gas turbocharger including a compressor wheel, the compressor wheel is cooled by at least one nozzle which is arranged in close axial proximity to the axis of rotation of the compressor wheel for spraying the backside of the compressor wheel near the center thereof with coolant whereby

In an exhaust gas turbocharger including a compressor wheel, the compressor wheel is cooled by at least one nozzle which is arranged in close axial proximity to the axis of rotation of the compressor wheel for spraying the backside of the compressor wheel near the center thereof with coolant whereby the coolant, utilizing the centrifugal forces of the rotating compressor wheel, is completely distributed over the entire wheel back surfaces.

대표청구항 ▼

What is claimed is: 1. An exhaust-gas turbocharger for an internal combustion engine, including a compressor (5) having a compressor wheel ( 8) with a shaft (7) and a wheel back (32) which is cooled by a coolant, and at least one nozzle (35) arranged in a first cooling space (46) adjacent the shaft

What is claimed is: 1. An exhaust-gas turbocharger for an internal combustion engine, including a compressor (5) having a compressor wheel ( 8) with a shaft (7) and a wheel back (32) which is cooled by a coolant, and at least one nozzle (35) arranged in a first cooling space (46) adjacent the shaft (7) of the compressor wheel (8) for spraying coolant directly onto the wheel back (32) adjacent the radially inner end thereof, so that the coolant flows radially outwardly along the rear wall of the compressor wheel, said nozzle (35) being arranged such that a radial distance (a) between the center of the nozzle (35) and an outer surface ( 37) of the shaft of the compressor (5) does not exceed the radius of the shaft (7). 2. An exhaust-gas turbocharger according to claim 1, wherein there is a transition area from a front side (18) to the wheel back (32) of the compressor wheel (8) which is stepped to form of a labyrinth seal. 3. An exhaust-gas turbocharger according to claim 2, wherein the steps of the transition area from the front side (18) to the wheel back (32) of the compressor wheel (8) are provided by means of a stepped diameter structure at the radially outer end of the compressor wheel (8). 4. An exhaust-gas turbocharger according to claim 1, wherein a second cooling space (28) surrounds a spiral housing (21) of the compressor (5), and means are provided for supplying a coolant to said second cooling space (28) for cooling the compressor (5). 5. An exhaust-gas turbocharger according to claim 1, wherein the compressor (5) includes a housing with an annular duct ( 30) forming a diffuser area (29) and a coolant for cooling the diffuser area (29) and the compressor (5) is conducted through said annular duct (30). 6. An exhaust-gas turbocharger according to claim 1, wherein at least two nozzles (35) are provided, which are arranged in an angular range α of approximately 0째-60째 to the axis of rotation ( 36) of the compressor wheel (8). 7. An exhaust-gas turbocharger according to claim 1, wherein the coolant is one of oil and water. 8. An exhaust-gas turbocharger according to claim 1, wherein the coolant is a refrigerant which is capable of boiling or vaporizing in a low temperature range. 9. Exhaust-gas turbocharger according to claim 8, wherein the vaporization temperature of the refrigerant is lower than 120째 Celsius. 10. An exhaust-gas turbocharger according to claim 1, wherein the coolant is removed from an isolated area of said first cooling space (46) of the compressor wheel (8) via a siphon duct ( 55) in the exhaust-gas turbocharger (2). 11. An exhaust-gas turbocharger according to claim 1, wherein the compressor wheel (8) is designed without any bored holes. 12. An exhaust-gas turbocharger according to claim 1, wherein there is no dividing wall between a space (46) for cooling the compressor wheel and a space (61) for a rotor bearing (60). 13. An exhaust-gas turbocharger according to claim 1, wherein the heat dissipation from the compressor area due to cooling of the air in the compressor (5) Qcompressor is more than 20% of the total heat dissipation Qtotal from the compressed air, the total heat dissipation Qtotal being obtained from the sum of the heat dissipated from the compressor Qcompressor and the heat dissipated from an intercooler (12) Qintercooler as: Q total=Qcompressor+Qintercooler.