초록 ▼

In internal combustion engines (1), the sealing of the combustion chamber by pistons and piston rings is not absolute. Throughout the working cycle, gases from the cylinder enter the crankcase (1a). These blow-by gases must be able to escape from the crankcase (1a). In a device for returning the blo

In internal combustion engines (1), the sealing of the combustion chamber by pistons and piston rings is not absolute. Throughout the working cycle, gases from the cylinder enter the crankcase (1a). These blow-by gases must be able to escape from the crankcase (1a). In a device for returning the blow-by gases into the system of an internal combustion engine (1) supercharged with a gas-dynamic pressure-wave supercharger (10), it is envisaged that a gas delivery unit designed as an ejector (20) generates a reduced pressure in the crankcase (1a). The ejector (20) is operated with a propellant gas from a line (16) which is taken from the supercharger airline (13), a control (8) placed in the propellant gas line (16) ensuring that the reduced pressure in the crankcase (1a) never exceeds a defined value. The blow-by gases in the line (2) flow through an oil separator (4) and, mixed with the propellant gas in the line (16), are then returned into the exhaust line (15) of the engine system.

대표청구항 ▼

1. Device for returning the blow-by gases from the crankcase into the system of a supercharged internal combustion engine, having a gas delivery unit which is driven by a propellant and which, when a control device placed in the extraction line is connected in, generates a reduced pressure in the cr

1. Device for returning the blow-by gases from the crankcase into the system of a supercharged internal combustion engine, having a gas delivery unit which is driven by a propellant and which, when a control device placed in the extraction line is connected in, generates a reduced pressure in the crankcase, wherein the internal combustion engine is supercharged by a gas-dynamic pressure-wave supercharger and the propellant for the gas delivery unit is gas which is taken from the output of the gas-dynamic pressure-wave supercharger in a propellant line and which is controllable by means of a controller placed in the propellant line in such a way that, throughout the operating range, a reduced pressure of not greater than -50 mbar prevails in the crankcase. 2. Device according to claim 1 wherein the propellant line branches off on the air side downstream of the gas-dynamic pressure-wave supercharger and upstream of a starter valve flap. 3. Device according to claim 1 wherein the propellant line is connected to one of the pockets of the gas-dynamic pressure-wave supercharger. 4. Device according to claim 1 wherein the gas delivery unit is an ejector. 5. Device according to claim 4 wherein the ejector is made of plastic. 6. Device according to claim 4 wherein the ejector is connected to the internal combustion engine system by hoses. 7. Device according to claim 1 wherein the oil separator is provided upstream of the gas delivery unit. 8. Device according to claim 1 wherein the degree of reduced pressure in the crankcase is controlled by means of a propellant gas rate control. 9. Device according to claim 1 wherein the degree of reduced pressure in the crankcase is controlled by means of a pressure-modulation control. 10. Device according to claim 1 wherein an exhaust line is operatively connected to the engine and the gas delivery unit is a venturi nozzle placed in the exhaust line. 11. Device according to claim 1 wherein the cleaned gases from the crankcase are returnable to a point in the gas-dynamic pressure-wave supercharger where a reduced pressure prevails. 12. Device according to claim 1 wherein, when the internal combustion engine is idling, valve lubrication is effected by the blow-by gases from the crankcase, a non-return valve preventing a flow of supercharging air into the line of the blow-by gases when the internal combustion engine picks up load.