IP Library Granted Patent US 11,952,951
Granted Patent B2
US 11,952,951 · App. 17/735,923 · Granted Apr 9, 2024

Thermal management of aftertreatment devices of opposed-piston engines under motoring conditions

Inventors: Fabien G. Redon (San Diego, CA); Arunandan Sharma (San Diego, CA)
Assignee: Achates Power, Inc.
F02D41/0235F02B25/08F02B75/282F02D23/00F02D41/0007F02D43/00F02B37/04F02B2075/025F02D2200/0802
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Quick Facts
Patent No.
US 11,952,951
App. No.
17/735,923
Granted
Apr 9, 2024
Kind
B2
Abstract

A method of operating a two-stroke cycle, opposed-piston engine comprising a pumping device coupled to pump air to cylinders of the engine through a charge air cooler and an aftertreatment system of thermally-activated devices coupled to receive exhaust from the cylinders by which a thermal state of the exhaust sufficient to sustain thermal activation of one or more of the aftertreatment system devices may be maintained during a deceleration or motoring condition of operation by reducing the mass airflow to the engine.

Claims (36)

1. A method of operating a two-stroke cycle, opposed-piston engine comprising a control unit to execute the method, a supercharger coupled to pump air to cylinders of the engine through a charge air cooler, a bypass channel to recirculate charge air from an outlet of the supercharger to an inlet of the supercharger, and an aftertreatment system of thermally-activated devices coupled to receive exhaust from the cylinders, the method comprising:

injecting fuel into the engine while operating the engine in a two-stroke cycle mode;

operating the supercharger to provide a mass airflow into the engine;

transporting a mass exhaust flow from the engine to the aftertreatment system;

ceasing fuel injection into the engine while motoring the engine; and,

maintaining a thermal state of the mass exhaust flow sufficient to sustain thermal activation of one or more of the aftertreatment system devices during motoring of the engine by recirculating a portion of the mass airflow through the bypass channel to the inlet of the supercharger.

2. The method of claim 1 , wherein the portion of the mass airflow recirculated to the inlet of the supercharger is obtained downstream of an outlet of the charge air cooler.

3. The method of claim 2 , further including reducing the mass exhaust flow to the aftertreatment system during motoring of the engine.

4. The method of claim 1 , wherein the mass airflow includes recirculated exhaust flow and wherein the portion of the mass airflow recirculated to the supercharger is obtained downstream of the charge air cooler.

5. The method of claim 4 , further including reducing the mass exhaust flow to the inlet of the aftertreatment system during motoring of the engine.

6. The method of claim 5 , further including reducing the recirculated exhaust flow during motoring of the engine.

7. A method of operating a fuel-injected, opposed-piston engine comprising a control unit to execute the method, a supercharger coupled to pump air to cylinders of the engine through a charge air cooler, a bypass channel to recirculate charge air from an outlet of the supercharger to an inlet of the supercharger, and an aftertreatment system of thermally-activated devices coupled to receive exhaust from the cylinders, the method comprising:

injecting fuel into the engine while operating the engine in a two-stroke cycle mode;

operating the supercharger to provide a mass airflow to the engine;

transporting a mass exhaust flow from the engine to an inlet of the aftertreatment system;

ceasing fuel injection into the engine while operating the engine; and,

maintaining a thermal state of the mass exhaust flow sufficient to sustain thermal activation of one or more of the aftertreatment system devices during cessation of fuel injection by recirculating a portion of the mass airflow through the bypass channel to the inlet of the supercharger.

8. The method of claim 7 , wherein the mass airflow to the engine is reduced by recirculating a portion of the mass airflow obtained downstream of the outlet of the charge air cooler to the inlet of the supercharger.

9. The method of claim 8 , further including reducing the mass exhaust flow to the aftertreatment system during cessation of fuel injection.

10. The method of claim 7 , wherein the mass airflow includes recirculated exhaust flow.

11. The method of claim 10 , further including reducing the mass exhaust flow to the aftertreatment system during cessation of fuel injection.

12. The method of claim 11 , further including reducing the recirculated exhaust flow during cessation of fuel injection.

13. A method of operating a two-stroke, opposed-piston engine comprising a control unit to execute the method, a supercharger coupled to pump air to cylinders of the engine through a charge air cooler, a bypass channel to recirculate charge air from an outlet of the supercharger to an inlet of the supercharger, and an aftertreatment system of thermally-activated devices coupled to receive exhaust from the cylinders, the method comprising:

injecting fuel into the engine while operating the engine in a two-stroke cycle mode;

operating the supercharger to provide a mass airflow to the engine;

transporting a mass exhaust flow from the engine to an inlet of the aftertreatment system;

detecting an exhaust flow reduction condition of engine operation;

ceasing fuel injection in response to the exhaust flow reduction condition of engine operation; and,

maintaining a thermal state of the mass exhaust flow sufficient to sustain thermal activation of one or more of the aftertreatment system devices during the exhaust flow reduction condition of operation by recirculating a portion of the mass airflow through the bypass channel to the inlet of the supercharger.

14. The method of claim 13 , wherein the mass airflow to the inlet of the engine is reduced by recirculating a portion of the mass airflow to the inlet of the supercharger obtained downstream of the outlet of the charge air cooler.

15. The method of claim 14 , further including reducing the mass exhaust flow to the aftertreatment system during the exhaust reduction condition of operation.

16. The method of claim 13 , wherein the mass airflow includes recirculated exhaust flow.

17. The method of claim 16 , further including reducing the mass exhaust flow to the inlet of the aftertreatment system during the exhaust reduction condition of operation.

18. The method of claim 17 , further including reducing the recirculated exhaust flow during the exhaust reduction condition of operation.

19. The method of claim 7 , wherein the mass airflow recirculated to the inlet of the supercharger is obtained downstream of an outlet of the charge air cooler.

20. The method of claim 13 , wherein the mass airflow recirculated to the inlet of the supercharger is obtained downstream of an outlet of the charge air cooler.

Assignments (3)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Sep 23, 2025
From: ACHATES POWER, INC.
To: GENERAL ATOMICS AERONAUTICAL SYSTEMS, INC.
Reel/Frame 072956/0001 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 4, 2022
From: REDON, FABIEN G.
To: ACHATES POWER, INC.
Reel/Frame 059811/0414 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 4, 2022
From: SHARMA, ARUNANDAN
To: ACHATES POWER, INC.
Reel/Frame 059811/0459 →