Spark ignited engine load extension with low pressure exhaust gas recirculation and delta pressure valve
10823120 ยท 2020-11-03
Assignee
Inventors
Cpc classification
F02B47/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B75/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0052
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/1038
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/703
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2250/26
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D11/105
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10255
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/40
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10222
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/0404
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/005
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2041/0017
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B2075/1824
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2009/0272
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/48
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/001
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/43
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Y02T10/12
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
F02D2200/0406
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10236
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0065
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/0007
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D2200/101
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/23
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F02M26/06
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B75/18
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D41/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02D9/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02B37/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M35/10
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/48
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/08
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/23
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F02M26/43
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Techniques for controlling a forced-induction engine having a low pressure exhaust gas recirculation (LPEGR) system comprise determining a desired differential pressure (dP) at an inlet of a boost device based on an engine mass air flow (MAF) and a speed of the engine, wherein the engine further comprises a dP valve disposed upstream from an EGR port and a throttle valve disposed downstream from the boost device, determining a desired EGR mass fraction based on at least the engine MAF and the engine speed, determining a maximum throttle inlet pressure (TIP) based on the engine speed, the desired EGR mass fraction, and a barometric pressure, and performing coordinated control of the dP valve and the throttle valve based on the desired dP and the maximum TIP, respectively, thereby extending EGR operability to additional engine speed/load regions and increasing engine efficiency.
Claims
1. A control system for a forced-induction engine having a low pressure exhaust gas recirculation (LPEGR) system configured to recirculate exhaust gas produced by the engine to an induction system of the engine via an EGR port, the control system comprising: a differential pressure (dP) valve disposed upstream from the EGR port, wherein the EGR port is disposed upstream from an inlet of a boost device of the engine; a throttle valve disposed downstream from the boost device; and a controller configured to: determine a desired dP based on an engine mass air flow (MAF) and a speed of the engine; determine a desired EGR mass fraction based on at least the engine MAF and the engine speed; determine a maximum throttle inlet pressure (TIP) based on the engine speed, the desired EGR mass fraction, and a barometric pressure; and perform coordinated control of the dP valve and the throttle valve based on the desired dP and the maximum TIP, respectively, thereby extending EGR operability to additional engine speed/load regions and increasing engine efficiency.
2. The control system of claim 1, wherein the controller is configured to determine the desired EGR mass fraction by: determining a nominal desired EGR mass fraction using a two-dimensional calibrated surface based on the engine MAF and the engine speed; and multiplying the nominal desired EGR mass fraction by a downstream modifier value indicative of at least one of induction system pressures, temperatures, and valve positions.
3. The control system of claim 2, wherein the valve positions include at least one of the dP valve's position, a surge or bypass valve's position, the throttle valve's position, intake/exhaust valve positions, a wastegate valve's position, and an EGR valve's position.
4. The control system of claim 2, wherein the controller is configured to determine the maximum TIP by: determining a nominal maximum TIP using a two-dimensional calibrated surface based on the engine speed and the barometric pressure; and multiplying the nominal maximum TIP by a maximum TIP EGR correction value.
5. The control system of claim 4, wherein the controller is configured to determine the maximum TIP EGR correction value using a two-dimensional calibrated surface based on the engine speed and a ratio of the desired EGR mass fraction to the nominal desired EGR mass fraction.
6. The control system of claim 1, wherein the coordinated dP and throttle valve control extends EGR operability to additional engine speed/load regions by mitigating or eliminating low-speed pre-ignition (LSPI) and knock.
7. The control system of claim 1, wherein the controller is further configured to decrease or limit a maximum achievable engine torque when EGR flow cannot be delivered.
8. The control system of claim 1, wherein the coordinated dP and throttle valve control extends EGR operability to additional engine speed/load regions without using blow-through scavenging or in-cylinder fuel enrichment.
9. The control system of claim 1, wherein the engine is a twin-turbocharged, six cylinder engine and the LPEGR system is a low pressure cooled EGR (LPCEGR) system that is associated with one turbocharger loop of the engine.
10. A method of controlling a forced-induction engine having a low pressure exhaust gas recirculation (LPEGR) system configured to recirculate exhaust gas produced by the engine to an induction system of the engine via an EGR port upstream from a boost device of the engine, the method comprising: determining, by a controller of the engine, a desired differential pressure (dP) at an inlet of the boost device based on an engine mass air flow (MAF) and a speed of the engine, wherein the engine further comprises a dP valve disposed upstream from the EGR port and a throttle valve disposed downstream from the boost device; determining, by the controller, a desired EGR mass fraction based on at least the engine MAF and the engine speed; determining, by the controller, a maximum throttle inlet pressure (TIP) based on the engine speed, the desired EGR mass fraction, and a barometric pressure; and performing, by the controller, coordinated control of the dP valve and the throttle valve based on the desired dP and the maximum TIP, respectively, thereby extending EGR operability to additional engine speed/load regions and increasing engine efficiency.
11. The method of claim 10, wherein the determining the desired EGR mass fraction comprises: determining a nominal desired EGR mass fraction using a two-dimensional calibrated surface based on the engine MAF and the engine speed; and multiplying the nominal desired EGR mass fraction by a downstream modifier value indicative of at least one of induction system pressures, temperatures, and valve positions.
12. The method of claim 11, wherein the valve positions include at least one of the dP valve's position, a surge or bypass valve's position, the throttle valve's position, intake/exhaust valve positions, a wastegate valve's position, and an EGR valve's position.
13. The method of claim 11, wherein determining the maximum TIP comprises: determining a nominal maximum TIP using a two-dimensional calibrated surface based on the engine speed and the barometric pressure; and multiplying the nominal maximum TIP by a maximum TIP EGR correction value.
14. The method of claim 13, wherein determining the maximum TIP EGR correction value comprises using a two-dimensional calibrated surface based on the engine speed and a ratio of the desired EGR mass fraction to the nominal desired EGR mass fraction.
15. The method of claim 10, wherein the coordinated dP and throttle valve control extends EGR operability to additional engine speed/load regions by mitigating or eliminating low-speed pre-ignition (LSPI) and knock.
16. The method of claim 10, further comprising decreasing or limiting, by the controller, a maximum achievable engine torque when EGR flow cannot be delivered.
17. The method of claim 10, wherein the coordinated dP and throttle valve control extends EGR operability to additional engine speed/load regions without using blow-through scavenging or in-cylinder fuel enrichment.
18. The method of claim 10, wherein the engine is a twin-turbocharged, six cylinder engine and the LPEGR system is a low pressure cooled EGR (LPCEGR) system that is associated with one turbocharger loop of the engine.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1)
(2)
(3)
DETAILED DESCRIPTION
(4) As previously discussed, spark-ignition (SI) engine systems, particularly turbocharged SI engines having low pressure exhaust gas recirculation (EGR) systems, are often unable to provide the required high level of EGR in low speed, high load operating regions of the engine to prevent low-speed pre-ignition (LSPI) and knock. As a result, engine torque output is often limited at these operating conditions. Conventional solutions to this problem include blow-through scavenging, in-cylinder fuel enrichment, combustion chamber design changes (e.g., redesign), and fuel/oil qualities changes (e.g., requiring a different quality fuel and/or oil). Each of these solutions decreases fuel economy or efficiency or increases costs. Accordingly, techniques are presented for extended EGR operation of a turbocharged SI engine having a low pressure EGR (LPEGR) system (e.g., a low pressure cooled EGR, or LPCEGR system) to additional engine speed/load regions by introducing a delta or differential pressure (dP) valve upstream from an EGR port in an induction system of the engine. These techniques utilize a ratio of nominal desired EGR to current desired EGR to limit a full-load engine torque/speed curve. This results in a maximum throttle inlet pressure (TIP) modifier based on achievable EGR flow when compared to nominal EGR flow. The requested EGR keeps the request stable, reducing boost request oscillation potential. Actual EGR, which is susceptible to oscillations, also protects against instances where actual EGR flow isn't meeting the request prior to on-board diagnostic (OBD) intervention (EGR valve wide open, EGR valve stuck etc.). The throttle and dP valves are then controlled accordingly. Potential benefits of these techniques include improved drivability/performance due to the extended EGR operation at higher torque levels.
(5) Referring now to
(6) While six cylinders are shown, it will be appreciated that the engine 102 could include any suitable number of cylinders (4, 8, etc.). An engine speed sensor 131 measures a rotational speed of the crankshaft 127, also known as a speed of the engine 102. In one exemplary implementation, the fuel system 130 comprises a fuel tank that houses fuel (e.g., gasoline), a fuel rail that houses pressurized fuel, fuel injectors that open/close to inject the pressurized fuel into the engine 102, and a fuel pump that pumps the fuel from the fuel tank to the fuel rail to generate the pressurized fuel. The fuel system 130 could also optionally include an evaporative emissions (EVAP) system that captures fuel or purge vapor that evaporates from the fuel in the fuel tank and stores it in a vapor canister and provides the fuel vapor to any suitable point in the induction system 104 (e.g., after the dP valve 110) via an EVAP line and a purge valve. Fuel vapor is highly combustible and therefore is able to increase engine power and/or efficiency. Exhaust gas resulting from combustion is expelled from the cylinders 128 via respective exhaust valves (not shown) into exhaust manifolds 134a, 134b. Each exhaust manifold 134a, 134b, for example, could be associated with three of the six cylinders 128. The exhaust gas in exhaust manifold 134a flows through exhaust path 136a and its kinetic energy drives a turbine 138a of turbocharger 114a. The turbine 138a drives compressor 116a via a shaft 140a. Similarly, the exhaust gas in exhaust manifold 134b flows through exhaust path 136b and its kinetic energy drives a turbine 138b of turbocharger 114b, which in turn drives compressor 116b via a shaft 140b. Wastegate valves 141a, 141b regulate turbocharger speed/boost pressure.
(7) The exhaust gas flows from turbines 138a, 138b through exhaust paths 142a, 142b and is treated by exhaust treatment systems (ETS) 144a, 144b to decrease or eliminate emissions before being released into the atmosphere. Non-limiting example components include gasoline particulate filters (GPFs), three-way catalytic converters (TWCs), and mufflers. It will be appreciated that each ETS 144a, 144b could include other exhaust treatment components. A low pressure EGR (LPEGR) system 146 recirculates exhaust gas from an EGR pickup point 147 downstream of ETS 144b through an EGR path 148 that is regulated by an EGR valve 150. The EGR path 148 splits into separate EGR paths 152a, 152b which direct the exhaust gas to ports in induction paths 112a, 112b downstream of the dP valve 110 and upstream of the compressors 116a, 116b. In one implementation, the LPEGR system 146 is an LPCEGR system that also includes an EGR cooler (EGRC) 154 that cools the exhaust gas. Because turbocharged gasoline engines operate at very high temperatures, cooling of the recirculated exhaust gas could provide for increased performance. A controller 156 controls operation of the engine system 101. It will be appreciated that the term controller as used herein refers to any suitable control device or set of multiple control devices that is/are configured to perform at least a portion of the techniques of the present disclosure. Non-limiting examples include an application-specific integrated circuit (ASIC) and one or more processors and a non-transitory memory having instructions stored thereon that, when executed by the one or more processors cause the controller to perform a set of operations. The one or more processors could be a single processor or two or more processors operating in a parallel or distributed architecture.
(8) Optional inlet air temperature and mass air flow (MAF) sensors 109, 111 measure intake air temperature and intake mass air flow. It will be appreciated that these sensors 109, 111 could also be arranged in other suitable positions of the induction system 104. An optional charge air temperature sensor 123 measures ACT at an outlet of the throttle valve 122. An optional EGRC outlet temperature sensor 155 measures a temperature of EGR at an outlet of the EGRC 154. The controller 156 includes a barometric pressure sensor 158 that measures barometric pressure. It will be appreciated that the barometric sensor 158 could be external to the controller 156. An EGR valve delta pressure sensor 160 is disposed proximate to the EGR valve 150 and measures a delta pressure across the EGR valve 150. A dP valve outlet pressure sensor 162 measures a pressure at an outlet of the dP valve 110. As previously mentioned, this dP valve outlet pressure also corresponds to inlet pressures of the compressors 116a, 116b. Lastly, exhaust gas concentration sensors 164a, 164b measure exhaust gas concentration. In one exemplary implementation, the exhaust gas concentration sensors 164a, 164b are WRO2 sensors configured to measure an air/fuel ratio (FA) of the exhaust gas. It will be appreciated that the engine system 101 could include other suitable sensors, such as an exhaust gas or back pressure sensor (not shown). All of these sensors provide their measurements to the controller 156, e.g., via a controller area network (CAN, not shown). The controller 156 is also able to control the various valves and other devices/systems described herein, e.g., via the CAN. The controller 156 is also configured to implement at least a portion of the techniques of the present disclosure, which are now described in greater detail.
(9) Referring now to
(10) Referring now to
(11) It should be understood that the mixing and matching of features, elements, methodologies and/or functions between various examples may be expressly contemplated herein so that one skilled in the art would appreciate from the present teachings that features, elements and/or functions of one example may be incorporated into another example as appropriate, unless described otherwise above.