Exhaust gas turbocharger

Claim 2

An exhaust gas turbocharger for a vehicle engine, the exhaust gas turbocharger including a turbine means, a compressor means, the turbine means including a rotor means operatively connected to the compressor means, and a spiral housing means, a plurality of inlet channel means provided in said spiral housing means, the inlet channel means are combined only directly ahead of and at a periphery of the turbine rotor means, characterized in that a circumferential substantially circular edge is formed in an outer surface of the rotor means, annular channel means are provided for conducting a flow of exhaust gases, and annular gap is provided within an area of the circular edge for enabling a part of the exhaust gases to flow from the spiral housing means into the annular channel means, the compressor means includes a charging air channel means, a return line communicating the annular channel means with the charging air channel means, a turbine exhaust gas line is provided, and a bypass line means for bypassing the turbine means leads to the turbine exhaust gas line, and in that said return line and the bypass line means branch off from the annular channel means.

Claim 3

An exhaust gas turbocharger according to claim 1, wherein the exhaust gas turbocharger comprises means for pulse turbocharging of the vehicle engine.

Claim 4

An exhaust gas turbocharger according to claim 1, characterized in that the outer surface of the rotor means is a rotor back surface, the annular gap is provided within an area in which the rotor backsurface and a periphery of the turbine rotor means form the circumferential, substantially circular edge.

Claim 5

An exhaust gas turbocharger for a vehicle engine, the exhaust gas turbocharger including a turbine means, a compressor means, the turbine means including a rotor means operatively connected to the compressor means, and a spiral housing means, a plurality of inlet channel means provided in said spiral housing means, the inlet channel means are combined only directly ahead of and at a periphery of the turbine rotor means, characterized in that a circumferential substantially circular edge is formed in an outer surface of the rotor means, annular channel means are provided for conducting a flow of exhaust gases, and annular gap is provided within an area of the circular edge for enabling a part of the exhaust gases to flow from the spiral housing means into the annular channel means, the compressor means includes a charging air channel means, a return line communicating the annular channel means with the charging air channel means, a turbine exhaust gas line is provided, and a bypass line means for bypassing the turbine means leads to the turbine exhaust gas line, said return line and the bypass line means branch off from the annular channel means, and in that the annular gap and annular channel means begin in the spiral housing means of the turbine means at a place at which the rotor means of the turbine means passes over from the periphery into the area of smaller outside diameter.

Claim 6

An exhaust gas turbocharger for a vehicle engine, the exhaust gas turbocharger including a turbine means, a compressor means, the turbine means including a rotor means operatively connected to the compressor means, and a spiral housing means, a plurality of inlet channel means provided in said spiral housing means, the inlet channel means are combined only directly ahead of and at a periphery of the turbine rotor means, characterized in that a circumferential substantially circular edge is formed in an outer surface of the rotor means, annular channel means are provided for conducting a flow of exhaust gases, and annular gap is provided within an area of the circular edge for enabling a part of the exhaust gases to flow from the spiral housing means into the annular channel means, the compressor means includes a charging air channel means, a return line communicating the annular channel means with the charging air channel means, a turbine exhaust gas line is provided, and a bypass line means for bypassing the turbine means leads to the turbine exhaust gas line, said return line and the bypass line means branch off from the annular channel means, and in that the annular gap and annular channel means begin in the spiral housing means of the turbine means at a place at which the rotor means of the turbine means passes over from the periphery into the area of smaller outside diameter.

Claim 7

An exhaust gas turbocharger according to one of claims 1, 2, 3, or 4, characterized in that a throttle valve means is arranged in the turbine exhaust gas line, and comprising means for controlling the throttle valve means in dependence on specific engine operating parameter magnitudes.

Claim 8

An exhaust gas turbocharger according to claim 5, characterized in that the specific engine magnitude is at least one of mean effective pressure and rotational speed of the engine.

Claim 9

An exhaust gas turbocharger according to claim 5, characterized in that the specific engine magnitudes are mean effective pressures and rotational speed of the engine.

Claim 10

An exhaust gas turbocharger according to claim 6, characterized in that a by-pass valve means is arranged in the turbine by-pass line means, and an exhaust gas recirculation valve means is arranged in the exhaust gas return line and comprising means for controlling the exhaust gas recirculation valve means in dependence on the specific engine operating parameter magnitudes.

Claim 11

An exhaust gas turbocharger according to claim 8, characterized in that the by-pass valve means is a diaphragm valve.

Claim 12

An exhaust gas turbocharger according to claim 8, comprising means for controlling the turbine by-pass valve means in dependence on surpercharging pressure.

Claim 13

An exhaust gas turbocharger according to claim 8, comprising means for controlling the turbine by-pass valve means to be closed at low load and increasingly opened at middle and higher loads of the engine.

Claim 14

An exhaust gas turbocharger according to claim 11, wherein the exhaust gas recirculation valve means comprises means for opening the exhaust gas recirculation means at low load and increasingly closing at higher loads of the engine.

Claim 15

An exhaust gas turbocharger according to one of claims 1, 2, 3 or 4, characterized in that by-pass valve means is arranged in the turbine by-pass line means, and an exhaust gas recirculation valve means is arranged in the exhaust gas return line and comprising means for controlling the exhaust gas recirculation valve means in dependence on the specific engine operating parameter magnitudes.

Claim 16

An exhaust gas turbocharger according to claim 13, comprising means for controlling the turbine by-pass valve means in dependence on supercharging pressure.

Claim 17

An exhaust gas turbocharger according to claim 13, comprising means for controlling the turbine by-pass valve means to be closed at low load and increasingly opened at middle and higher loads of the engine.

Claim 18

An exhaust gas turbocharger according to claim 13, wherein the exhaust gas return valve means comprises means for opening the exhaust gas recirculation means at low load and increasingly closing at higher loads.

Claim 19

An exhaust gas turbocharger according to claim 8, comprising means for controlling the turbine bypass valve means in dependence on exhaust gas pressure.

Claim 20

An exhaust gas turbocharger according to claim 13, comprising means for controlling the turbine bypass valve means in dependence on exhaust gas pressure.