Internal combustion engine and method for detecting a leak from a crankcase and/or a tank ventilation system
An internal combustion engine has a tank ventilation system and a crankcase ventilation system. The tank ventilation system is connectable to an intake system downstream of a throttle element via a first non-return valve in a first line and upstream of a compressor via a second non-return valve in a second line and a third non-return valve in a second sub-line. The crankcase ventilation system is connectable to the intake system downstream of the throttle element via a fourth non-return valve in a third line and upstream of the compressor via a fourth line and the third non-return valve. The intake system is connectable to the second line downstream of the throttle element at a transitional point between the second line and the second sub-line via a fifth nonreturn valve in a fifth line. A nozzle is formed at the transitional point from the fifth line to the second line and the second sub-line, and the second line opens into the nozzle downstream of the second non-return valve. A first pressure sensor for measuring the pressure in the second line is provided in the second line between the second non-return valve and the nozzle. Only a single pressure sensor is required to diagnose or detect a leak.
1. An internal combustion engine, comprising:
a combustion air induction system in which a compressor is arranged and in which a throttle element is arranged downstream of the compressor in a flow direction of the combustion air:
a tank ventilation system, wherein the tank ventilation system is connectable to the induction system downstream of the throttle element via a first non-return valve in a first line and upstream of the compressor via a second non-return valve in a second line and a third non-return valve in a second sub-line;
a crankcase ventilation system, wherein the crankcase ventilation system is connectable to the induction system downstream of the throttle element via a fourth non-return valve in a third line, and upstream of the compressor via a fourth line and the third non-return valve; wherein
the induction system is connectable downstream of the throttle element via a fifth non-return valve in a fifth line to the second line at a transition point between the second line and the second sub line;
a nozzle is formed at the transition point from the fifth line to the second line and the second sub line, wherein the second line opens into the nozzle downstream of the second non-return valve; and
a first pressure sensor measures pressure in the second line, the first pressure sensor being provided in the second line between the second non-return valve and the nozzle.
2. The internal combustion engine according to claim 1 , further comprising:
a second pressure sensor provided in the second sub line or in the fourth line.
3. The internal combustion engine according to claim 2 , further comprising:
a diagnostic device that evaluates pressures sensed by the first and second pressure sensors.
4. The internal combustion engine according to claim 1 , further comprising:
a tank ventilation valve provided in the first line between a tank and the first and second non-return valves.
5. The internal combustion engine according to claim 2 , further comprising:
a tank ventilation valve provided in the first line between a tank and the first and second non-return valves.
6. The internal combustion engine as claimed in claim 1 ,
further comprising:
a second throttle element provided between the fourth non-return valve and the fourth line.
7. The internal combustion engine as claimed in claim 5 ,
further comprising:
a second throttle element provided between the fourth non-return valve and the fourth line.
8. The internal combustion engine according to claim 1 ,
further comprising:
a diagnostic device that evaluates pressure sensed by the first pressure sensor.
9. A method for detecting a leak from a crankcase ventilation system and/or a tank ventilation system of an internal combustion engine, wherein
the internal combustion engine comprises a combustion air induction system in which a compressor is arranged and in which a throttle element is arranged downstream of the compressor in a flow direction of the combustion air;
the tank ventilation system is connectable to the induction system downstream of the throttle element via a first non-return valve in a first line and upstream of the compressor via a second non-return valve in a second line and a third non-return valve in a second sub-line;
the crankcase ventilation system is connectable to the induction system downstream of the throttle element via a fourth non-return valve in a third line, and upstream of the compressor via a fourth line and the third non-return valve;
the induction system is connectable downstream of the throttle element via a fifth non-return valve in a fifth line to the second line at a transition point between the second line and the second sub line;
a nozzle is formed at the transition point from the fifth line to the second line and the second sub line, wherein the second line opens into the nozzle downstream of the second non-return valve;
a first pressure sensor measures pressure in the second line, the first pressure sensor being provided in the second line between the second non-return valve and the nozzle,
the method comprising the steps of:
starting the internal combustion engine;
measuring a first sensor pressure with the first pressure sensor;
comparing, via a diagnostic device, the first sensor pressure with a first model pressure;
evaluating whether the first sensor pressure differs from the first model pressure or not;
in an event of no difference of the first sensor pressure from the first model pressure, no fault signal is output by the diagnostic device; and
in an event of a difference of the first sensor pressure from the first model pressure, a fault signal is output by the diagnostic device.
10. A method for detecting a leak from a crankcase ventilation system and/or a tank ventilation system of an internal combustion engine, wherein
the internal combustion engine comprises a combustion air induction system in which a compressor is arranged and in which a throttle element is arranged downstream of the compressor in a flow direction of the combustion air;
the tank ventilation system is connectable to the induction system downstream of the throttle element via a first non-return valve in a first line and upstream of the compressor via a second non-return valve in a second line and a third non-return valve in a second sub-line;
the crankcase ventilation system is connectable to the induction system downstream of the throttle element via a fourth non-return valve in a third line, and upstream of the compressor via a fourth line and the third non-return valve;
the induction system is connectable downstream of the throttle element via a fifth non-return valve in a fifth line to the second line at a transition point between the second line and the second sub line;
a nozzle is formed at the transition point from the fifth line to the second line and the second sub line, wherein the second line opens into the nozzle downstream of the second non-return valve;
a first pressure sensor measures pressure in the second line, the first pressure sensor being provided in the second line between the second non-return valve and the nozzle;
a second pressure sensor is provided in the second sub line or the fourth line,
the method comprising the steps of:
measuring the first and second sensor pressures with the first pressure sensor and the second pressure sensor;
comparing, via a diagnostic device, the first and second sensor pressures with a first and a second model pressure;
evaluating whether the first and second sensor pressures differ from the first and second model pressures or not; and
in an event of a difference of the first sensor pressure from the first model pressure, and of the second sensor pressure from the second model pressure, outputting via the diagnostic device a fault signal indicating a leak in the crankcase ventilation system.
11. The method according to claim 10 , further comprising
the step of:
in an event of a difference of the first sensor pressure from the first model pressure and no difference of the second sensor pressure from the second model pressure, outputting by the diagnostic device a fault signal indicating a leak in the tank ventilation system.