초록 ▼

A reciprocating engine includes a turbocharging unit that: supplies the intake manifold with air via a coolant; is supplied with gas by the exhaust manifold; and has the turbine supply pressure substantially equal to the compressor discharge pressure. At constant air temperature, the turbocharging u

A reciprocating engine includes a turbocharging unit that: supplies the intake manifold with air via a coolant; is supplied with gas by the exhaust manifold; and has the turbine supply pressure substantially equal to the compressor discharge pressure. At constant air temperature, the turbocharging unit delivers a substantially constant volume of cooled air when the pressure varies, and the volume is substantially proportional to the turbine outlet section. The turbine pressure is maintained substantially equal to compressor pressure by a EGR bypass between the intake and exhaust manifold. In addition, the volume of air is less than the volume drawn in at the speed so that a flow of hot gases is drawn in again via the bypass above the speed, where the volume drawn in is equal to the volume, and a flow of air is deflected towards the turbine below the speed.

대표청구항 ▼

The invention claimed is: 1. A method of operating a 4-stroke reciprocating engine wherein the engine is operating between a minimum speed of rotation Nmin and a maximum speed Nmax and comprises: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with comp

The invention claimed is: 1. A method of operating a 4-stroke reciprocating engine wherein the engine is operating between a minimum speed of rotation Nmin and a maximum speed Nmax and comprises: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature, the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure substantially equal to a compressor discharge pressure; such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, wherein the EGR bypass has a gas cooler adjustable to control the temperature of the transferred flow of the hot exhaust gas, and wherein the method of operating includes controlling the EGR bypass temperature to create a desired excess of air for combustion in the engine; and wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 2. A method of operating a 4-stroke reciprocating engine wherein the engine is operating between a minimum speed of rotation Nmin and a maximum speed Nmax and comprises: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature, the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure is maintained substantially equal to a compressor discharge pressure; such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that, at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, and wherein the EGR bypass has a gas cooler adjustable to control the temperature of the transferred flow of the hot exhaust gas; and wherein the method of operating includes controlling the EGR bypass temperature so that a mass of the transferred hot exhaust gas remains substantially equal to a mass of the fresh air up to the speed at which this temperature returns to the exhaust temperature, the mass of the transferred hot exhaust gas becoming greater than the mass of the fresh air above this speed. 3. A method of operating a 4-stroke reciprocating engine as claimed in claim 2, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 4. A 4-stroke reciprocating engine operating between a minimum speed of rotation Nmin and a maximum speed Nmax comprising: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure is maintained substantially equal to a compressor discharge pressure, such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, wherein the EGR bypass has a gas cooler adjustable to control the temperature of the transferred flow of the hot exhaust gas, wherein the adjustment of the temperature is effected by controlling a bypass of the cooler, and wherein the gas cooler is totally bypassed when the engine does not deliver propulsive power. 5. A method of operating a 4-stroke reciprocating engine as claimed in claim 4, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 6. A 4-stroke reciprocating engine operating between a minimum speed of rotation Nmin and a maximum speed Nmax comprising: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature, the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure is maintained substantially equal to a compressor discharge pressure, such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, wherein the EGR bypass has a gas cooler adjustable to control the temperature of the transferred flow of the hot exhaust gas, wherein the adjustment of the temperature is effected by controlling a bypass of the cooler; and wherein for cold starting and operating at idling speed, the exhaust outlet section Sd and/or a timing of engine valves is adjusted so that the excess of combustion air is minimal for a desired level of depollution. 7. A method of operating a 4-stroke reciprocating engine as claimed in claim 6, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 8. A 4-stroke reciprocating engine operating between a minimum speed of rotation Nmin and a maximum speed Nmax comprising: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature, the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure is maintained substantially equal to a compressor discharge pressure, such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, wherein the EGR bypass has a gas cooler adjustable to control the temperature of the transferred flow of the hot exhaust gas, wherein the adjustment of the temperature is effected by controlling a bypass of the cooler, wherein the adaptation speed Na is substantially equal to Nmin/2 so that the volume of the transferred flow of the hot exhaust gas is at least equal to that of the fresh air, and wherein the minimum temperature of the transferred flow of the hot exhaust gas is close to the temperature of the fresh air so that a mass of the transferred flow of the hot exhaust gas is at least equal to that of the fresh air at the minimum speed used Nmin in order to depollute down to the minimum speed Nmin. 9. A 4-stroke reciprocating engine operating between a minimum speed of rotation Nmin and a maximum speed Nmax comprising: a turbocharging unit comprising: a compressor which supplies an intake manifold of the engine with compressed air via a cooler; a turbine which is supplied with a hot exhaust gas by an exhaust manifold of the engine at an exhaust temperature, the turbine defining an exhaust outlet section Sd offered to said hot exhaust gas; and an EGR bypass provided between the intake manifold and the exhaust manifold which EGR bypass is dimensioned to transfer a flow of gas between the intake manifold and the outlet manifold without substantial loss of pressure, such that a turbine inlet pressure is maintained substantially equal to a compressor discharge pressure; such that, at constant air temperature and with a constant value of the exhaust outlet section Sd, the turbocharging unit delivers a substantially constant volume of cooled air Vc when the compressor discharge pressure varies, the constant volume of cooled air Vc being substantially proportional to the exhaust outlet section Sd offered to the hot exhaust gas, wherein the exhaust outlet section Sd is selected such that, at a turbocharging adaptation speed Na, the volume drawn in by the engine is equal to the constant volume Vc, below the turbocharging adaptation speed Na, the volume drawn in by the engine is less than the constant volume of cooled air Vc, and a flow of the cooled air is deflected toward the turbocharging unit through the EGR bypass, and above the turbocharging adaptation speed Na and including the maximum speed Nmax, the volume drawn in by the engine is more than the constant volume of cooled air Vc, and a flow of exhaust gas is drawn in by the engine through the EGR bypass, wherein the turbocharging unit has a low-pressure LP turbocharger having an LP turbine and an LP compressor, and a high-pressure HP turbocharger having an HP turbine and an HP compressor, the LP and HP compressors working in series, wherein the exhaust outlet section Sd offered to the hot exhaust gases is adjustable between a minimum Sd min and a maximum Sd max by one or a combination of the following: adjustment of a variable section of a gas distributor of the turbines, opening of a bypass between an inlet and an outlet of the turbines, and passage from a series configuration to a parallel configuration of the turbines, the turbocharging adaptation speed Na thus being adjustable, in a continuous or discontinuous manner, between two values Na min and Na max. 10. A 4-stroke reciprocating engine as claimed in claim 9, wherein the minimum exhaust outlet section Sd min offered to the gases is formed by the two turbines mounted in series, with variable distributors being at maximum closure. 11. A 4-stroke reciprocating engine as claimed in claim 10 wherein the maximum exhaust outlet section Sd max is formed by two turbines with fully open variable distributors mounted in series, and wherein the distributors are opened simultaneously in order to maintain the intake pressure at a maximum desired value thereof on a full load curve. 12. A 4-stroke reciprocating engine as claimed in claim 9, wherein the minimum exhaust outlet section Sd min offered to the hot exhaust gas is formed by the two turbines with fixed distributors mounted in series, waste gates of the turbines being in a closed position. 13. A 4-stroke reciprocating engine as claimed in claim 12, wherein a timing of engine valves is controlled to displace a closure of an associated cylinder between the vicinity of the BDC and the mid-stroke of an associated piston, wherein the maximum exhaust outlet section Sd is formed by the HP turbine in series configuration; and wherein the turbines are dimensioned to permit the compressors thereof to reach maximum pressure ratios thereof simultaneously. 14. A method of operating a 4-stroke reciprocating engine as claimed in claim 13, wherein a full load curve as a function of the speed is operated as follows: from Nmin to 2 Nmin, an intake closure FA passes from the BDC to approximately 90 degrees of a crankshaft after the BDC to maintain a cycle pressure below a desired value thereof, and a distributor or an HP waste gate is closed; from 2 Nmin to approximately 3 Nmin, the HP distributor or the HP waste gate is open to maintain an intake pressure at a maximum desired value thereof, and the intake closure FA is maintained at 90 degrees of the crankshaft after the BDC; and from 3 Nmin to Nmax, a global flow rate of fuel is kept constant to maintain the intake pressure at a limiting value thereof, and at partial load, a timing of intake closure FA is controlled according to a map stored in an engine control computer. 15. A method of operating a 4-stroke reciprocating engine as claimed in claim 14, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 16. A 4-stroke reciprocating engine as claimed in claim 9, wherein the maximum exhaust outlet section Sd max offered to the gases is formed by the two turbines which have fixed distributors mounted in parallel, and wherein, in order to pass the turbines from the series configuration to the parallel configuration, the following manoeuvres are carried out successively: progressive partial opening of an HP waste gate between the inlet and the outlet of the HP turbine, progressive and simultaneous partial opening of the HP waste gate and an LP waste gate between the inlet and the outlet of the LP turbine, and simultaneously and rapidly: total opening of the HP waste gate, total closure of the LP waste gate, and putting the outlet of the HP turbine into communication with the outlet of the LP turbine. 17. A 4-stroke reciprocating engine as claimed in claim 16, wherein, in order to limit a frequency of changing a configuration, the turbines are maintained in a series configuration for a type of driving which implements a limited power range, and crossing power thresholds corresponding to this configuration for manoeuvres of short duration by opening of one or both of the waste gates. 18. A method of operating a 4-stroke reciprocating engine as claimed in claim 17, wherein, the EGR bypass has an EGR valve to increase the turbine inlet pressure above the compressor discharge pressure, and the method includes crossing of the power thresholds by closure of the EGR valve and by opening of one or both of the waste gate. 19. A method of operating a 4-stroke reciprocating engine as claimed in claim 18, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 20. A method of operating a 4-stroke reciprocating engine as claimed in claim 17, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer. 21. A 4-stroke reciprocating engine as claimed in claim 16, wherein the LP waste gate has a second seat in order simultaneously to effect a closure of the LP turbine inlet/outlet bypass and putting the HP turbine outlet into communication with the LP turbine outlet. 22. A 4-stroke reciprocating engine as claimed in claim 16, wherein the two waste gates are concentric and have stops such that simultaneous movements thereof are actuated by one and communicated to the other by the stops. 23. A 4-stroke reciprocating engine as in claim 16, wherein the section of the HP waste gate fully opened is smaller than the section of the LP turbine to increase the gas flow through the HP turbine in the parallel configuration. 24. A 4-stroke reciprocating engine as claimed in claim 9, wherein the maximum outlet section Sd max offered to the gases is formed by the LP turbine with fixed distributor and the HP turbine with variable distributor mounted in parallel, an HP variable distributor being fully open, and wherein, in order to pass the turbines from the series configuration to the parallel configuration, the following manoeuvres are carried out successively: progressive opening of a distributor of the HP turbine, progressive partial opening of an LP waste gate, simultaneously and rapidly: total opening of the LP waste gate and putting the outlet of the HP turbine into communication with the outlet of the LP turbine. 25. A 4-stroke reciprocating engine as claimed in claim 9, wherein the EGR bypass has an EGR valve to increase the turbine inlet pressure above the compressor discharge pressure; and wherein the method of operating includes, in order to limit a frequency of changing a configuration, maintaining the turbines in series configuration for a type of driving which implements a limited power range, and crossing power thresholds corresponding to this configuration for manoeuvres of short duration by closure of the EGR valve. 26. A method of operating a 4-stroke reciprocating engine as claimed in claim 25, wherein the exhaust outlet section Sd is selectively variable and is controlled: at full load, to maintain a parameter at a limiting desired value thereof; and at partial load, to optimize depollution and/or performance according to a map stored in an engine control computer.