Abstract: A compressor arrangement for an internal combustion engine, having a compressor which is arranged in a compressor housing and has a low pressure side and a high pressure side, and having a negative pressure provision unit, which has a propellant channel that is fluidically connected, on the one hand, via a propellant inlet fitting to the high pressure side of the compressor and, on the other hand, via a propellant outlet fitting to the low pressure side of the compressor and has a nozzle, and which has a negative pressure channel opening into the propellant channel fluidically between the propellant inlet fitting and the propellant outlet fitting.

Abstract: A compressor arrangement for an internal combustion engine, including a compressor which is located in a compressor housing and has a low pressure side and a high pressure side, and includes a vacuum supply device which has: a propellant channel which has a nozzle and is fluidically connected on one side via a propellant inlet connection to the high pressure side of the compressor and on the other side via a propellant outlet connection to the low pressure side of the compressor; and a vacuum channel opening into the propellant channel fluidically between the propellant inlet connection and the propellant outlet connection.

Abstract: A compressor arrangement for an internal combustion engine, including a compressor which is located in a compressor housing and has a low pressure side and a high pressure side, and includes a vacuum supply device which has: a propellant channel which has a nozzle and is fluidically connected on one side via a propellant inlet connection to the high pressure side of the compressor and on the other side via a propellant outlet connection to the low pressure side of the compressor; and a vacuum channel opening into the propellant channel fluidically between the propellant inlet connection and the propellant outlet connection.

Abstract: An exhaust gas turbocharger for an internal combustion engine, includes a turbine; a bypass line fluidly arranged parallel to the turbine; and a cross section adjustment element for adjusting a flow cross section of the bypass line, wherein the cross section adjustment element being configured as a ball valve having a valve housing, two bearing shells arranged in the valve housing and a valve element. The valve element is floatingly supported in the valve housing and arranged between the two bearing shells with a tolerance in a direction which is angled with respect to a rotation axis of the valve element.

Abstract: A compressor arrangement for an internal combustion engine, having a compressor which is arranged in a compressor housing and has a low pressure side and a high pressure side, and having a negative pressure provision unit, which has a propellant channel that is fluidically connected, on the one hand, via a propellant inlet fitting to the high pressure side of the compressor and, on the other hand, via a propellant outlet fitting to the low pressure side of the compressor and has a nozzle, and which has a negative pressure channel opening into the propellant channel fluidically between the propellant inlet fitting and the propellant outlet fitting.

Abstract: An exhaust turbocharger includes a turbine housing having a flange rim, and a bearing housing having a flange rim. Arranged between the flange rim of the turbine housing and the flange rim of the bearing housing is a ring which is made of sheet metal. The flange rim of the turbine housing and the flange rim of the bearing housing are connected to one another to form a flange.