EXHAUST-GAS-TURBOCHARGED INTERNAL COMBUSTION ENGINE HAVING AT LEAST TWO TURBINES AND SWITCHABLE OUTLET OPENINGS, AND METHOD FOR OPERATING AN INTERNAL COMBUSTION ENGINE OF SAID TYPE

• US 20160290220A1
• Filed: 03/17/2016
• Published: 10/06/2016
• Est. Priority Date: 03/31/2015
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Smiljanovski, Vanco, Kindl, Helmut Matthias, Kemmerling, Joerg, Brinkmann, Franz J., Sommerhoff, Franz Arnd
• Granted Patent: US 9,896,991 B2
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: F01L 1/34 characterised by the provision of means for changing the timing of the valves without changing the duration of opening and without affecting the magnitude of the valve lift
• CPC Class Codes: F01L 13/0005 Deactivating valves
• CPC Class Codes: F01L 13/0015 for optimising engine performances by modifying valve lift according to various working parameters, e.g. rotational speed, load, torque
• CPC Class Codes: F01L 2800/00 Methods of operation using a variable valve timing mechanism
• CPC Class Codes: F01L 2800/08 Timing or lift different for valves of different cylinders
• CPC Class Codes: F01N 5/04 the devices using kinetic energy
• CPC Class Codes: F02B 37/001 using exhaust drives arranged in parallel
• CPC Class Codes: F02B 37/007 with exhaust-driven pumps arranged in parallel , e.g. at least one pump supplying alternatively
• CPC Class Codes: F02B 37/013 with exhaust-driven pumps arranged in series
• CPC Class Codes: F02B 37/025 Multiple scrolls or multiple gas passages guiding the gas to the pump drive
• CPC Class Codes: F02B 37/16 by bypassing charging air
• CPC Class Codes: F02B 37/18 by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

Systems and methods are provided for controlling boost pressure in an engine system with a parallel turbocharger. One example method includes, responsive to a first condition, deactivating a first compressor of a first turbocharger, activating each first exhaust valve of each cylinder of an engine, and deactivating each second exhaust valve of each cylinder of the engine to flow exhaust gas from the engine to a second turbocharger. The method further includes, responsive to boost pressure exceeding a threshold, maintaining deactivation of the first compressor, reactivating each second exhaust valve to flow exhaust gas from the engine to both the first turbocharger and second turbocharger, and driving an electric assist device via a first turbine of the first turbocharger.

Claims

1. An engine system, comprising:

an intake system for supplying charge air to an engine having at least two cylinders, each cylinder including at least two outlet openings for discharge of exhaust gases, at least one of the at least two outlet openings of each cylinder being a switchable outlet opening, each outlet opening being adjoined by an exhaust line for the discharge of the exhaust gases via an exhaust-gas discharge system;

a first exhaust-gas turbocharger and a second exhaust-gas turbocharger, each exhaust-gas turbocharger comprising a turbine arranged in the exhaust-gas discharge system and a compressor arranged in the intake system;

a first exhaust manifold formed from a first overall exhaust line, the exhaust line of at least one switchable outlet opening of each cylinder issuing into the first overall exhaust line, said first overall exhaust line being connected to a first turbine of the first exhaust-gas turbocharger;

a second exhaust manifold formed from a second overall exhaust line, the exhaust lines of the other outlet openings of the at least two cylinders merging to form the second overall exhaust line, said second overall exhaust line being connected to a second turbine of the second exhaust-gas turbocharger;

a first compressor of the first exhaust-gas turbocharger is arranged in a first intake line of the intake system, a shut-off element being arranged in the first intake line, and at least each switchable outlet opening whose exhaust line issues into the first overall exhaust line is equipped with an at least partially variable valve drive having a switchable outlet valve which opens up an associated outlet opening between an open position and a closed position, forming a valve lift Δ

h, during an opening duration Δ

t;

an electric machine which is at least connectable in terms of drive to the first turbine of the first exhaust-gas turbocharger and which is operable, as a generator, for receiving power from the first turbine; and

the second turbine of the second exhaust-gas turbocharger does not have a bypass line.

2. The engine system as claimed in claim 1, wherein the at least two cylinders are arranged into a first cylinder group and a second cylinder, where at least one cylinder of the first cylinder group has only one switchable outlet opening, an exhaust line of which issues into the first overall exhaust line.

3. The engine system as claimed in claim 1, wherein the at least two cylinders are arranged into a first cylinder group and a second cylinder, where all of outlet openings of the at least one cylinder of the first cylinder group are in the form of switchable outlet openings.

4. The engine system as claimed in claim 1, wherein the at least two cylinders are configured in such a way that they form at least two cylinder groups with in each case at least one cylinder, the at least one cylinder of a first cylinder group being a cylinder which is operational during a partial deactivation of the internal combustion engine, and the at least one cylinder of a second cylinder group being formed as a load-dependently switchable cylinder, and all of outlet openings of the at least one cylinder of the second cylinder group are in the form of switchable outlet openings.

5. The engine system as claimed in claim 1, wherein at least each switchable outlet valve of each switchable outlet opening whose exhaust line issues into the first overall exhaust line is an outlet valve which is adjustable with regard to the valve lift Ah.

6. The engine system as claimed in claim 5, wherein at least each switchable outlet valve of each switchable outlet opening whose exhaust line issues into the first overall exhaust line is an outlet valve which is adjustable in a two-stage fashion, a multi-stage fashion, or a continuously adjustable fashion, with regard to the valve lift Ah.

7. The engine system as claimed in claim 1, wherein at least each switchable outlet valve of each switchable outlet opening whose exhaust line issues into the first overall exhaust line is an outlet valve which is adjustable with regard to the opening duration Δ

t.

8. The engine system as claimed in claim 7, wherein the engine has at least four cylinders in an in-line arrangement along a longitudinal axis of a cylinder head of the engine, and wherein the outer cylinders form one cylinder group and the at least two inner cylinders form another cylinder group.

9. The engine system as claimed in one claim 1, wherein the overall exhaust lines merge to form a common exhaust line downstream of the turbines, and wherein the electric machine, which is connectable in terms of drive to the first turbine of the first exhaust-gas turbocharger, is operable as an auxiliary drive for assisting the first exhaust-gas turbocharger, for making additional power available for drive purposes.

10. The engine system as claimed in claim 1, wherein at least one turbine has a variable turbine geometry.

11. The engine system as claimed in claim 1, wherein the second turbine of the second exhaust-gas turbocharger is of smaller dimensions than the first turbine of the first exhaust-gas turbocharger.

12. A method, comprising:

responsive to a first condition, deactivating a first compressor of a first turbocharger, activating each first exhaust valve of each cylinder of an engine, and deactivating each second exhaust valve of each cylinder of the engine to flow exhaust gas from the engine to a second turbocharger; and

responsive to boost pressure exceeding a threshold, maintaining deactivation of the first compressor, reactivating each second exhaust valve to flow exhaust gas from the engine to both the first turbocharger and second turbocharger, and driving an electric assist device via a first turbine of the first turbocharger.

13. The method of claim 12, wherein the first condition comprises engine load above a threshold load and engine speed below a threshold speed.

14. The method of claim 12, wherein deactivating the first compressor comprises closing a compressor shut-off valve to block flow of intake air through the first compressor.

15. The method of claim 12, further comprising during both the first condition and responsive to boost pressure exceeding the threshold, flowing intake air through a second compressor of the second turbocharger.

16. A system, comprising:

an engine having a first cylinder group and a second cylinder group, each cylinder of the engine including a first exhaust valve controlling a first exhaust port and a second exhaust valve controlling a second exhaust port;

a first exhaust manifold fluidically coupled to each second exhaust port;

a second exhaust manifold fluidically coupled to each first exhaust port;

a first turbocharger including a first turbine fluidically coupled to the first exhaust manifold and a first compressor coupled to the first turbine, flow of intake air through the first compressor controlled by compressor recirculation valve coupled in parallel to the first compressor and a compressor shut-off valve coupled downstream of the first compressor;

a second turbocharger including a second turbine fluidically coupled to the second exhaust manifold and a second compressor coupled to the second turbine;

an electric assist device coupled to the first turbine; and

a controller including instructions to, during a first condition, provide boost pressure only via the second turbocharger, and responsive to the boost pressure exceeding a threshold pressure, reactivate each second exhaust valve to divert excess exhaust gas from the engine to the first turbine, close the compressor shut-off valve, and drive the electric assist device in a generator mode.

17. The system of claim 16, wherein during the first condition when the boost pressure does not exceed the threshold pressure, the controller includes instructions to deactivate each second exhaust valve in order to provide boost pressure only via the second turbocharger.

18. The system of claim 17, wherein the controller includes further instructions to, during a second condition, deactivate each cylinder of the second cylinder group, open the compressor shut-off valve, and flow exhaust gas from the first cylinder group to the first turbocharger and the second turbocharger.

19. The system of claim 18, wherein the controller includes further instructions to, during a third condition, activate each cylinder of the engine, activate each first exhaust valve and second exhaust valve of each cylinder, open the compressor shut-off valve, and flow exhaust gas from the first cylinder group and the second cylinder group to the first turbocharger and the second turbocharger.

20. The system of claim 19, wherein the first condition comprises engine load above a threshold load and engine speed below a threshold speed, the second condition comprises engine load below the threshold load, and the third condition comprises engine load above the threshold load and engine speed above the threshold speed.