Engine braking method for an internal combustion engine having two serially arranged exhaust-gas turbochargers
View Patent ↗In an engine braking method and an internal combustion engine including an engine braking arrangement, wherein the engine has high pressure and low pressure exhaust gas turbochargers connected in series, with a bypass ( 12 ) around the high-pressure compressor allowing the air mass flow selectively to bypass the high pressure compressor which is arranged near the engine, and bypasses around both turbines permitting the exhaust gas mass flow selectively to bypass the high-pressure exhaust gas turbine which is near the engine and also the low pressure turbine the intake air and the exhaust gas flow are controlled so as to accurately provide for a desired engine braking power for example for maintaining a desired vehicle speed.
1. An engine braking method for an internal combustion engine ( 1 ) having two exhaust gas turbochargers ( 2 , 6 ), each of the two exhaust gas turbochargers ( 2 , 6 ) having an exhaust gas turbine ( 3 , 7 ) arranged in series in the an exhaust tract of the engine ( 1 ) and each of the two exhaust gas turbines ( 3 , 7 ) including a fixed geometry turbine inlet passage, a bypass line ( 10 , 14 ) extending around each exhaust gas turbine ( 3 , 7 ) with a control valve ( 11 , 15 ) in each bypass line ( 10 , 14 ) for selectively permitting the exhaust gas flow to bypass at least one of the turbines, and each of the two exhaust gas turbochargers ( 2 , 6 ) including a first compressor ( 4 ) and a second compressor ( 8 ) arranged in series in an intake tract of the engine ( 1 ) and the first compressor ( 4 ) arranged in the intake tract nearer the engine ( 1 ) including a bypass line ( 12 ) with a valve ( 13 ) for selectively permitting the compressed intake air to bypass the first compressor ( 4 ) arranged nearer the engine, said method comprising the steps of:
controlling the air mass flow bypassing the first compressor ( 4 ) arranged nearer the engine and the exhaust gas mass flow through at least one of the bypass lines ( 10 , 14 ) around the two exhaust gas turbines ( 3 , 7 ) depending on the desired engine braking power, and, for increasing the engine braking power, opening the valve ( 15 ) of the bypass of the turbine ( 7 ) remote from the engine ( 1 ) to permit exhaust gas to flow through the bypass line ( 14 ) past the turbine ( 7 ) remote from the engine ( 1 ).
2. The engine braking method as claimed in claim 1 , further including, for providing a constant downhill vehicle velocity controlling the exhaust gas mass flowing through the bypass line ( 14 ) which bypasses the exhaust gas turbine ( 7 ) arranged remote from the engine and controlling the air flowing through the bypass line ( 12 ) which bypasses the first compressor ( 4 ) which is near the engine so as to maintain a vehicle at constant velocity in a braking cruise control mode.
3. The engine braking method as claimed in claim 1 , wherein for reducing the engine braking power starting from a high engine braking power value, the following steps are performed:
I. closing the bypass ( 14 ) which bypasses the exhaust gas turbine ( 7 ) which is remote from the engine and, for further braking power reduction,
II. opening the bypass ( 12 ) which bypasses the first compressor ( 4 ) which is near to the engine, and, for still further braking power reduction,
III. opening the bypass ( 10 ) which bypasses the exhaust gas turbine ( 3 ) which is near the engine.
4. The engine braking method as claimed in claim 3 , and further including opening the bypass ( 14 ) which bypasses the exhaust gas turbine ( 7 ) which is remote from the engine upon opening of the bypass ( 10 ) which bypasses the exhaust gas turbine ( 3 ) which is near the engine.