Method and system for turbocharging an engine

• US 8,069,663 B2
• Filed: 09/09/2010
• Issued: 12/06/2011
• Est. Priority Date: 09/09/2010
• Status: Active Grant

• Current Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Original Assignee: Ford Global Technologies, LLC (Ford Motor Company)
• Inventors: Ulrey, Joseph Norman, Pursifull, Ross Dykstra
• Primary Examiner(s): Trieu, Thai Ba
• Application Number:
  US12/878,838
• Publication Number:
  US 20110167815A1
• Time in Patent Office: 453 Days
• Field of Search: 606/02, 606051-6052, 602/80, 602/78, 123/568.12, 123 9015- 9018, 123/316
• US Class Current: 60/605.2
• CPC Class Codes: F02B 2075/1816 four
• CPC Class Codes: F02B 37/00 Engines characterised by provision of pumps driven at least for part of the time by exhaust
• CPC Class Codes: F02B 37/18 by bypassing exhaust from the inlet to the outlet of turbine or to the atmosphere
• CPC Class Codes: F02D 13/02 during engine operation
• CPC Class Codes: F02D 13/0242 Variable control of the exhaust valves only
• CPC Class Codes: F02D 13/0249 changing the valve timing only
• CPC Class Codes: F02D 13/0257 Independent control of two or more intake or exhaust valves respectively, i.e. one of two intake valves remains closed or is opened partially while the other is fully opened
• CPC Class Codes: F02D 43/00 Conjoint electrical control of two or more functions, e.g. ignition, fuel-air mixture, recirculation, supercharging or exhaust-gas treatment
• CPC Class Codes: F02M 26/04 with a single turbocharger
• CPC Class Codes: F02M 26/05 High pressure loops, i.e. wherein recirculated exhaust gas is taken out from the exhaust system upstream of the turbine and reintroduced into the intake system downstream of the compressor
• CPC Class Codes: F02M 26/13 Arrangement or layout of EGR passages, e.g. in relation to specific engine parts or for incorporation of accessories
• CPC Class Codes: F02M 26/15 in relation to engine exhaust purifying apparatus
• CPC Class Codes: F02M 26/22 with coolers in the recirculation passage
• CPC Class Codes: F02M 26/27 with air-cooled heat exchangers
• CPC Class Codes: F02M 26/28 with liquid-cooled heat exchangers
• CPC Class Codes: F02M 26/44 in which a main EGR passage is branched into multiple passages
• CPC Class Codes: F02M 35/1085 the combustion chamber having multiple intake valves modifying induction systems for imparting a rotation to the charge in the cylinder and having multiple air inlets F02B31/08; shape or arrangement of intake or exhaust channels in cylinder heads F02F1/42
• CPC Class Codes: F02M 35/112 for engines with cylinders all in one line
• CPC Class Codes: F05B 2220/40 in turbochargers
• CPC Class Codes: Y02T 10/12 Improving ICE efficiencies

Abstract

A method for improving operation of a turbocharged engine is presented. In one embodiment, the method may reduce engine emissions and improve engine efficiency during an engine start.

Claims

1. An engine method, comprising:

opening a first exhaust valve of a cylinder before a piston of the cylinder reaches BDC compression stroke of the cylinder;

directing exhaust gases across the first exhaust valve into a first conduit;

recovering heat from the exhaust gases in the first conduit to a liquid; and

returning the exhaust gases after recovering exhaust heat to a second conduit that is in communication with a second exhaust valve of the cylinder.

2. The engine method of claim 1, where the exhaust gases directed across the first exhaust valve are separated from exhaust gases directed across the second exhaust valve at least until the exhaust gases directed across the first exhaust valve pass through a valve.

3. The engine method of claim 1, where the second exhaust valve of the cylinder opens after BDC exhaust stroke of the cylinder.

4. The engine method of claim 1, where a portion of the exhaust gases are directed to an intake manifold of a turbocharged engine.

5. The engine method of claim 1, where the heat is recovered via a gas-to-liquid heat exchanger.

6. The engine method of claim 5, where a portion of the exhaust gases are directed to a turbine and bypass the gas-to-liquid heat exchanger.

7. The engine method of claim 1, where the portion of the exhaust gases are returned to the exhaust passage in communication with the second exhaust valve at a location upstream of a first catalyst in a direction of exhaust flow.

8. An engine method, comprising:

during a first mode,

opening a first exhaust valve of a cylinder before a piston of the cylinder reaches BDC compression stroke of the cylinder;

flowing exhaust gases from a first combustion in the cylinder across the first exhaust valve;

recovering heat from the exhaust gases from the first combustion to a liquid;

returning the exhaust gases after recovering exhaust heat from the first combustion to an exhaust passage in communication with a second exhaust valve of the cylinder, the exhaust gases from the first combustion bypassing a turbine;

during a second mode,

opening a first exhaust valve of a cylinder before a piston of the cylinder reaches BDC compression stroke of the cylinder;

flowing exhaust gases from a second combustion in the cylinder across the first exhaust valve; and

returning the exhaust gases after recovering exhaust heat from the second combustion to the exhaust passage in communication with the second exhaust valve of the cylinder bypassing a gas-to-liquid heat exchanger.

9. The engine method of claim 8, where during the second mode, the exhaust gases from the second combustion are introduced to the exhaust passage in communication with the second exhaust valve at a location downstream of a first catalyst in a direction of exhaust flow from the second exhaust valve.

10. The engine method of claim 8, where during the first mode, a turbine shut-off valve is in a closed position, and where during the second mode the turbine shut-off valve is in an open position.

11. The engine method of claim 8, where during the first mode, an EGR valve downstream of the gas-to-liquid heat exchanger in a direction of exhaust flow is closed.

12. The engine method of claim 8, where during the first mode, the exhaust gases from the first combustion are returned to the exhaust passage in communication with the second exhaust valve of the cylinder at a location upstream of a first catalyst in a direction of exhaust flow from the second exhaust valve.

13. The engine method of claim 12, where during the second mode, the exhaust gases from the first combustion are returned to the exhaust passage in communication with the second exhaust valve of the cylinder at a location downstream of a first catalyst in a direction of exhaust flow from the second exhaust valve.

14. The engine method of claim 8, further comprising directing a portion of the exhaust gases from the first combustion to an intake manifold.

15. An engine system, comprising:

a first exhaust conduit extending from a first exhaust port of a cylinder;

a second exhaust conduit extending from a second exhaust port of the cylinder,

the second exhaust port isolated from the first exhaust port;

a gas-to-liquid heat exchanger located in a first branch of the first exhaust conduit,

an outlet of the gas-to-liquid heat exchanger directed exhaust flow to an intake manifold and the second conduit;

a turbocharger located in a second branch of the first exhaust conduit; and

a first catalyst and a second catalyst located along the second conduit.

16. The engine system of claim 15, further comprising:

a first valve located downstream of the turbocharger in a direction of the exhaust flow, and

a second valve located between the gas-to-liquid heat exchanger and the intake manifold, and

a third valve located between the gas-to-liquid heat exchanger and the second conduit.

17. The engine system of claim 16, further comprising a controller including instructions for operating the first, second, and third valves such that a first portion of exhaust gases from the cylinder are directed to the intake manifold, and a second portion of the exhaust gases from the cylinder are directed to the turbocharger.

18. The engine system of claim 16, further comprising a controller including instructions for closing the first valve during a start of an engine where a temperature of the engine is less than a threshold amount.

19. The engine system of claim 15,

where the outlet of the gas-to-liquid heat exchanger is directed to a location in the second conduit upstream of the first catalyst in a direction of the exhaust flow from the second exhaust port of the cylinder, and

where an outlet of the turbocharger is directed to a location in the second conduit downstream of the first catalyst and upstream of the second catalyst in a direction of the exhaust flow from the second exhaust port to the first catalyst.

20. The engine system of claim 19, further comprising an EGR valve positioned intermediate the intake manifold and the gas-to-liquid heat exchanger.