IP Library › Granted Patent US 12,345,220
Granted Patent B1
US 12,345,220 · App. 18/400,474 · Granted Jul 1, 2025

Air-handling system for fuel-efficient low load thermal promotion and high load operation for heavy duty engines

Inventors: Praveen Kumar (New Hudson, MI); Yu Zhang (Novi, MI); David Cleary (West Bloomfield, MI)
Assignee: SAUDI ARABIAN OIL COMPANY
F02M26/04F02B37/00F02B37/12F02B37/22F02M26/01F02M26/05F01N2260/14F02M2026/004
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Quick Facts
Patent No.
US 12,345,220
App. No.
18/400,474
Granted
Jul 1, 2025
Kind
B1
Abstract

Described is an engine with a camshaft having a single cam profile, a gas intake manifold, and an exhaust gas rebreather system for receiving an exhaust gas from the engine. The exhaust gas rebreather system includes a main exhaust gas outlet configured to receive the exhaust gas. An exhaust gas rebreather line of the exhaust gas rebreather system returns a portion of the exhaust gas in the main exhaust gas outlet to the gas intake manifold. A variable nozzle turbocharger having one or more variable nozzle vanes is in fluid connection with the main exhaust gas outlet. The exhaust rebreather system further includes an exhaust gas recirculation valve and a back pressure valve. The exhaust gas recirculation valve is disposed in the exhaust gas rebreather line and in fluid connection with the main exhaust gas outlet, and the back pressure valve downstream of the variable nozzle turbocharger.

Claims (43)

1. An exhaust gas rebreather system, comprising:

a main exhaust gas outlet configured to receive an exhaust gas from an engine, the engine having a plurality of cylinders, a camshaft having a single cam profile in the absence of a variable valvetrain mechanism, and a gas intake manifold for providing an air inlet to the engine;

an exhaust gas rebreather line configured to return at least a portion of the exhaust gas in the main exhaust gas outlet to the gas intake manifold;

a variable nozzle turbocharger in fluid connection with the main exhaust gas outlet, the variable nozzle turbocharger comprising one or more variable nozzle vanes;

an exhaust gas recirculation valve disposed in the exhaust gas rebreather line and in fluid connection with the main exhaust gas outlet;

a back pressure valve downstream of the variable nozzle turbocharger; and

at least one temperature sensor disposed proximate to the main exhaust gas outlet,

wherein the one or more variable nozzle vanes is configured to at least partially close in response to a temperature threshold indicated by the at least one temperature sensor.

2. The exhaust gas rebreather system of claim 1 , wherein the one or more variable nozzle vanes is configured to close between 50% and 90%.

3. The exhaust gas rebreather system of claim 1 , wherein the temperature threshold is 200° C.

4. The exhaust gas rebreather system of claim 1 , wherein the exhaust gas recirculation valve is configured to at least partially close in response to a temperature threshold indicated by the at least one temperature sensor.

5. The exhaust gas rebreather system of claim 4 , wherein the exhaust gas recirculation valve is configured to close between 60% and 100%.

6. The exhaust gas rebreather system of claim 1 , wherein the one or more variable nozzle vanes is configured to at least partially open in response to a temperature threshold indicated by the at least one temperature sensor.

7. The exhaust gas rebreather system of claim 1 , wherein the exhaust recirculation valve is configured to at least partially open in response to a temperature threshold indicated by the at least one temperature sensor.

8. The exhaust gas rebreather system of claim 1 , comprising a compressor in fluid communication with the variable nozzle turbocharger.

9. The exhaust gas rebreather system of claim 8 , comprising an air cooler disposed downstream of the compressor.

10. A method of operating an exhaust gas rebreather system, the exhaust gas rebreather system comprising:

a main exhaust gas outlet configured to receive an exhaust gas from an engine having a plurality of cylinders, a camshaft having a single cam profile in the absence of a variable valvetrain mechanism, and a gas intake manifold for providing an air inlet to the engine;

an exhaust gas rebreather line configured to return at least a portion of the exhaust gas in the main exhaust gas outlet to the gas intake manifold;

a variable nozzle turbocharger in fluid connection with the main exhaust gas outlet, the variable nozzle turbocharger comprising one or more variable nozzle vanes;

an exhaust gas recirculation valve disposed in the exhaust gas rebreather line and in fluid connection with the main exhaust gas outlet; and

a back pressure valve downstream of the variable nozzle turbocharger,

wherein the method comprises:

partially closing the one or more variable nozzle vanes in response to a temperature, as indicated by at least one temperature sensor, being below a threshold value; and

partially closing the exhaust gas recirculation valve in response to the temperature being below the threshold value.

11. The method of claim 10 , wherein the threshold value is 200° C.

12. The method of claim 10 , further comprising partially opening the one or more variable nozzle vanes in response to a temperature, as indicated by the at least one temperature sensor, being above the threshold value.

13. The method of claim 10 , further comprising partially opening the exhaust gas recirculation valve in response to a temperature, as indicated by the at least one temperature sensor, being above the threshold value.

14. The method of claim 10 , further comprising partially opening the one or more variable nozzle vanes in response to torque demand not being met.

15. The method of claim 10 , wherein the exhaust gas rebreather system further comprises a selective catalytic reduction system, the method further comprising adjusting urea dosing in the selective catalytic reduction system in response to a tail-pipe emissions target not being met.

16. The method of claim 10 , further comprising applying a timing and split injection strategy in response to a rate of rise of pressure exceeding a predetermined maximum manifold pressure rise rate.

17. The method of claim 16 , wherein the timing and split injection strategy comprises adjusting fuel injection timing.

18. The method of claim 16 , wherein the timing and split injection strategy comprises splitting a fuel injection operation into at least two injection events.

19. A method of operating an exhaust gas rebreather system, the exhaust gas rebreather system comprising:

a main exhaust gas outlet configured to receive an exhaust gas from an engine having a plurality of cylinders, a camshaft having a single cam profile, and a gas intake manifold for providing an air inlet to the engine;

an exhaust gas rebreather line configured to return at least a portion of the exhaust gas in the main exhaust gas outlet to the gas intake manifold;

a variable nozzle turbocharger in fluid connection with the main exhaust gas outlet, the variable nozzle turbocharger comprising one or more variable nozzle vanes;

an exhaust gas recirculation valve disposed in the exhaust gas rebreather line and in fluid connection with the main exhaust gas outlet; and

a back pressure valve downstream of the variable nozzle turbocharger,

wherein the method comprises:

partially closing the one or more variable nozzle vanes in response to a temperature, as indicated by at least one temperature sensor, being below a threshold value;

partially closing the exhaust gas recirculation valve in response to the temperature being below the threshold value; and

applying a timing and split injection strategy in response to a rate of rise of pressure exceeding a predetermined maximum manifold pressure rise rate.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 25, 2024
From: ARAMCO SERVICES COMPANY
To: SAUDI ARAMCO TECHNOLOGIES COMPANY
Reel/Frame 069440/0486 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 25, 2024
From: SAUDI ARAMCO TECHNOLOGIES COMPANY
To: SAUDI ARABIAN OIL COMPANY
Reel/Frame 069440/0618 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Apr 25, 2024
From: KUMAR, PRAVEEN; CLEARY, DAVID
To: ARAMCO SERVICES COMPANY
Reel/Frame 067229/0433 →
References Cited (40)
US 3232043A · Birmann · 1966 [cited by examiner]
US 4445488A · Tanaka et al. · 1984 [cited by applicant]
US 6988365B2 · Sasaki · 2006 [cited by applicant]
US 8544266B2 · Bruck et al. · 2013 [cited by applicant]
US 9038376B2 · Petrovic et al. · 2015 [cited by applicant]
US 9670841B2 · Mittricker et al. · 2017 [cited by applicant]
US 9695729B2 · Light-Holets · 2017 [cited by applicant]
US 10704436B2 · Jozsa et al. · 2020 [cited by applicant]
US 11828220B1 · Zhang · 2023 [cited by examiner]
US 20080148720A1 · Tahara · 2008 [cited by applicant]
US 20090293453A1 · Sujan · 2009 [cited by applicant]
US 20100300089A1 · Gibble et al. · 2010 [cited by applicant]
US 20110048389A1 · Hsia · 2011 [cited by examiner]
US 20110120123A1 · Dickerson et al. · 2011 [cited by applicant]
US 20160312689A1 · Kemmerling · 2016 [cited by examiner]
US 20190107066A1 · Kurtz et al. · 2019 [cited by applicant]
US 20190178187A1 · Smith · 2019 [cited by examiner]
US 20200018243A1 · Baltrucki · 2020 [cited by examiner]
US 20200224614A1 · Hu · 2020 [cited by examiner]
US 20220056854A1 · Robel · 2022 [cited by examiner]
US 20230139973A1 · Kurtz · 2023 [cited by examiner]
US 20230384183A1 · Worms · 2023 [cited by examiner]
CN 113530665A · 2021 [cited by applicant]
EP 2588727B1 · 2018 [cited by applicant]
JP H0953456A · 1997 [cited by applicant]
JP 2009002275A · 2009 [cited by examiner]
KR 100982225B1 · 2010 [cited by applicant]
KR 101132379B1 · 2012 [cited by applicant]
WO 2014175816A1 · 2014 [cited by applicant]
Zhang Y. et al.l “An Experimental and Computational Investigation of Tailor-Developed Combustion and Air-Handling System Concepts in a Heavy-Duty Gasoline Compression Ignition Engine,” Energies, 2022 (23 pages). [cited by applicant]
Kumar, P, et al., “Variable Valve Strategy Evaluation for Low-Load Operation in a Heavy-Duty Gasoline Compression Ignition Engine,” Energies, 2017 (25 pages). [cited by applicant]
Ding, C., et al., “Fuel efficient exhaust thermal management for compression ignition engines during idle via cylinder deactivation and flexible valve actuation,” International Journal of Engine Research, 2016, pp. 619-… [cited by applicant]
Gosala DB, et al., “Diesel engine aftertreatment warm-up through early exhaust valve opening and internal exhaust gas recirculation during idle operation,” International Journal of Engine Research, 2018, pp. 758-773 (16… [cited by applicant]
Ramesh AK, et al., “Reverse breathing in diesel engines for aftertreatment thermal management,” International Journal of Engine Research, 2019, pp. 862-876 (15 pages). [cited by applicant]
California Air Resources Board (CARB), Heavy-Duty Low-NOx Program, <https://www.arb.ca.gov/msprog/hdlownox/> , Sep. 26, 2019 (10 pages). [cited by applicant]
Sharp, C., Webb, et al., “Achieving Ultra Low NOX Emissions Levels with a 2017 Heavy-Duty on-Highway TC Diesel Engine and an Advanced Technology Emissions System-Thermal Management Strategies,” SAE Int. J. Engines, 2017… [cited by applicant]
Ratzberger, R., et al., “Evaluation of Valve Train Variability in Diesel Engines,” SAE Int. J. Engines, 2015 (16 pages). [cited by applicant]
Kovacs, D., et al., “Modeling Heavy-Duty Engine Thermal Management Technologies to Meet Future cold Start Requirements,” SAE Technical Paper, 2019 (17 pages). [cited by applicant]
International Search Report issued for corresponding international patent application No. PCT/US2024/061168, mailed Mar. 27, 2025 (6 pages). [cited by applicant]
Written Opinion issued for corresponding international patent application No. PCT/US2024/061168, mailed Mar. 27, 2025 (10 pages). [cited by applicant]