Method for engine condition control with turbocompressor controllable bypass
View Patent ↗A system for a turbocharged internal combustion engine includes an engine having a charge inlet connected to the compressor outlet and an exhaust outlet connected to the turbine inlet for driving the turbocharger with hot exhaust gas and supplying compressed air to the engine for combustion. A bypass duct connects the compressor outlet to the turbine inlet for diverting a portion of the compressed air around the engine to the turbine inlet or exhaust. A control device selectively controls the diversion of air. An operating method for the system involves controlling peak cylinder firing pressure and/or maximum turbine inlet temperature, optionally with exhaust NOx and smoke in order to limit these variables to acceptable limits with a minimum of operational limitations.
1. A method of controlling peak firing pressure and turbine inlet temperature in a diesel engine having a turbocharger, the method comprising:
sensing inlet charge air pressure and charge air temperature;
obtaining fuel injection timing, engine speed and load;
determining current peak firing pressure;
computing charge air density and turbine inlet temperature;
transmitting charge air density, turbine inlet temperature and peak firing pressure to an electronic bypass valve control unit (BVCU);
comparing transmitted values of the turbine inlet temperature and the peak firing pressure with allowable maximums of these values stored in the BVCU; and
controlling the bypass valve to divert a sufficient portion of compressed air from a compressor outlet around the engine to maintain at least one of the peak firing pressure and the turbine inlet temperature within maximum allowable values.
2. A method as in claim 1 wherein the obtaining step includes obtaining the fuel injection timing, engine speed and load from an engine control unit.
3. A method as in claim 1 wherein the determining step includes measuring the peak firing pressure.
4. A method as in claim 1 wherein the determining step includes computing the peak firing pressure.
5. A method as in claim 4 wherein the peak firing pressure is computed from engine parameters, the engine speed, the computed charge density and the fuel injection timing.
6. A method as in claim 1 wherein the turbine inlet temperature is computed from the computed charge air density, the engine speed, the engine load and the fuel injection timing.
7. A method as in claim 1 including:
determining a NOx exhaust emission value and transmitting the NOx exhaust emission value to the BVCU, and
controlling the bypass valve to divert a sufficient portion of compressed air from the compressor outlet around the engine to maintain NOx exhaust emissions within maximum allowable values stored in the BVCU.
8. A method as in claim 1 including:
determining a visible exhaust smoke value;
transmitting the visible exhaust smoke value to the BVCU, and
controlling the bypass valve to divert a sufficient portion of compressed air from the compressor outlet around the engine to maintain allowable smoke emissions within maximum allowable values stored in the BVCU.
9. A method as in claim 1 including conducting compressed air diverted around the engine to a turbine inlet of the turbocharger to utilize the energy in the diverted gas to maintain compressor speed while reducing the temperature of exhaust gas driving the turbine.
10. A method as in claim 1 including conducting compressed air diverted around the engine to an engine exhaust outlet to maximize the effectiveness of the controlling step.