Internal combustion engine of a motor vehicle, with at least one
exhaust gas turbocharger (10, 11) comprising a
turbine (12, 13) and a compressor (14, 15), wherein
exhaust gas to be depressurized can be supplied to the
turbine (12, 13) of the respective
exhaust gas turbocharger (10, 11) and depressurized exhaust gas can be discharged from the
turbine (12, 13) of the respective exhaust gas
turbocharger (10, 11), wherein charge air (LL) to be compressed can be supplied to the compressor (14, 15) of the respective exhaust gas turbocharger (10, 11) via a first
air line (16, 17) and compressed charge air (LL) can be discharged from the compressor (14, 15) of the respective exhaust gas turbocharger (10, 11) via a second
air line (18, 19), with a venting
system for a
fuel tank of the motor vehicle, via which a
fuel tank leakage (KL) can be discharged via a vent line (25) towards at least one
activated carbon filter (26), and via which the
fuel tank leakage (KL) routed via the respective
activated carbon filter (26) can be mixed with charge air (LL) routed via a respective bypass line (27), which extends between the respective first
air line (16, 17) and second air line (18, 19), and the respective first air line (16, 17) can be supplied for mixing with the charge air (LL) to be compressed, characterized by the fact that A
check valve (29) is integrated into the respective first air line (16, 17), which prevents flow from the respective first air line (16, 17) towards the respective
activated carbon filter (26), and a venturi
nozzle (28) is integrated downstream of the
check valve (29) in the direction of flow of the fuel tank leakage (KL), which serves to mix the fuel tank leakage (KL) with charge air (LL) flowing via the bypass line (27), such that outside the respective first air line (16, 17) only those sections of the respective vent line (25) which extend upstream of the respective
check valve (29) in the direction of flow of the fuel tank leakage (KL), and those sections of the respective bypass line (27) which extend upstream of the respective venturi
nozzle (28) in the direction of flow of the charge air (LL) are accessible.