IP Library Granted Patent US 8,596,252
Granted Patent B2
US 8,596,252 · App. 12/612,384 · Granted Dec 3, 2013

Emission control system for an engine having a two-stage turbocharger

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Quick Facts
Patent No.
US 8,596,252
App. No.
12/612,384
Granted
Dec 3, 2013
Kind
B2
Abstract

While an engine ( 10, 10 A, 10 B, 10 C, 10 D, 10 E) is operating, a control system ( 22 ) processes data for certain engine operating parameters to calculate a quantity of exhaust gas needed to satisfy an exhaust gas recirculation requirement. If a primary EGR control loop ( 34 ) alone can satisfy the calculated quantity of exhaust gas, a secondary EGR control loop ( 36 ) is closed while the primary EGR control loop is controlled to satisfy the calculated quantity. When the processing determines that the primary EGR control loop alone cannot satisfy the calculated quantity, the secondary EGR control loop is open concurrently with the primary EGR control loop and both the primary EGR loop and the secondary EGR loop are controlled to cause the combined flow of exhaust gas through the primary EGR control loop and flow of exhaust gas through the secondary EGR control loop to satisfy the calculated quantity.

Claims (19)

1. A compression ignition engine comprising:

engine cylinders within which combustion occurs to operate the engine;

an intake system for introducing charge air into the engine cylinders;

a fueling system for introducing fuel into the engine cylinders to combust with the charge air;

an exhaust system through which exhaust gas resulting from combustion of fuel in the engine cylinders exits;

a turbocharger comprising a high-pressure turbine and a low-pressure turbine downstream of the high-pressure turbine through which exhaust gas exiting through the exhaust system successively passes and a low-pressure compressor operated by the low-pressure turbine and a high-pressure compressor downstream of the low-pressure compressor and operated by the high-pressure turbine through which air that has entered the intake system successively passes to create the charge air;

a primary EGR control loop having a pierce point to the exhaust system upstream of the high-pressure turbine and a pierce point to the intake system downstream of the high-pressure compressor for conveying some of the exhaust gas to the intake system;

a secondary EGR control loop having a pierce point to the exhaust system downstream of the high-pressure turbine and a pierce point to the intake system upstream of the high-pressure compressor for conveying some of the exhaust gas to the intake system;

a control system for processing data for certain engine operating parameters while the engine is operating to calculate a quantity of exhaust gas needed to satisfy an exhaust gas recirculation requirement for the engine based on those engine operating parameters to determine if the primary EGR control loop alone can satisfy the calculated quantity of exhaust gas, for causing the secondary EGR control loop to be closed while the primary EGR loop is controlled to satisfy the calculated quantity of exhaust gas when the processing determines that the primary EGR control loop alone can satisfy the calculated quantity of exhaust gas, and for causing the secondary EGR control loop to be open concurrently with the primary EGR control loop and both the primary EGR loop and the secondary EGR loop controlled to cause the combined flow of exhaust gas through the primary EGR control loop and flow of exhaust gas through the secondary EGR control loop to satisfy the calculated quantity of exhaust gas when the processing determines that the primary EGR control loop alone cannot satisfy the calculated quantity of exhaust gas, wherein the pierce point of the secondary EGR control loop to the exhaust system is upstream of the low-pressure turbine and the pierce point of the secondary EGR control loop to the intake system is downstream of the low-pressure compressor, the intake system comprises a cooler having an inlet downstream of the pierce point of the secondary EGR control loop to the intake system and an outlet to the high-pressure compressor and the intake system comprises a throttle valve under control of the control system for selectively throttling air flow from the low-pressure compressor to the high-pressure compressor, and the pierce point of the secondary EGR control loop to the intake system is downstream of the throttle valve and upstream of the cooler.

2. A compression ignition engine as set forth in claim 1 in which the primary EGR control loop comprises a primary EGR valve under control of the control system for controlling flow of exhaust gas through the primary EGR control loop and a primary EGR cooler upstream of the primary EGR valve.

3. A compression ignition engine as set forth in claim 2 in which the intake system comprises a charge air cooler downstream of the high-pressure compressor, and the pierce point of the primary EGR control loop to the intake system is downstream of the charge air cooler.

4. A compression ignition engine as set forth in claim 3 in which the intake system comprises an inter-stage cooler through which air from the low-pressure compressor passes to the high-pressure compressor.

5. A method of exhaust emission control in a compression ignition engine that has engine cylinders within which combustion occurs to operate the engine, an intake system for introducing charge air into the engine cylinders, a fueling system for introducing fuel into the engine cylinders to combust with the charge air, an exhaust system through which exhaust gas resulting from combustion of fuel in the engine cylinders exits, and a turbocharger comprising a high-pressure turbine and a low-pressure turbine downstream of the high-pressure turbine through which exhaust gas exiting through the exhaust system successively passes and a low-pressure compressor operated by the low-pressure turbine and a high-pressure compressor downstream of the low-pressure compressor and operated by the high-pressure turbine through which air that has entered the intake system successively passes to create the charge air, the method comprising:

as the engine is operating, processing data for certain engine operating parameters to calculate a quantity of exhaust gas needed to satisfy an exhaust gas recirculation requirement for the engine based on those engine operating parameters to determine if a primary EGR control loop having a pierce point to the exhaust system upstream of the high-pressure turbine and a pierce point to the intake system downstream of the high-pressure compressor alone can satisfy the calculated quantity of exhaust gas, when the processing determines that the primary EGR control loop alone can satisfy the calculated quantity of exhaust gas, causing a secondary EGR control loop having a pierce point to the exhaust system downstream of the high-pressure turbine and a pierce point to the intake system upstream of the high-pressure compressor to be closed while controlling the primary EGR control loop to satisfy the calculated quantity, but when the processing determines that the primary EGR control loop alone cannot satisfy the calculated quantity of exhaust gas, causing the secondary EGR control loop to be open concurrently with the primary EGR control loop and controlling both the primary EGR control loop and the secondary EGR control loop to cause the combined flow of exhaust gas through the primary EGR control loop and flow of exhaust gas through the secondary EGR control loop to satisfy the calculated quantity of exhaust gas, wherein the step of causing the secondary EGR control loop to be open concurrently with the primary EGR control loop and controlling both the primary EGR control loop and the secondary EGR control loop to cause the combined flow of exhaust gas through the primary EGR control loop and flow of exhaust gas through the secondary EGR control loop to satisfy the calculated quantity of exhaust gas comprises causing flow through the secondary EGR control loop to occur from a pierce point to the exhaust system that is upstream of the low-pressure turbine to a pierce point to the intake system that is downstream of the low-pressure compressor, causing both air that has entered the intake system and exhaust gas that has entered the intake system from the secondary EGR control loop to pass through a cooler that has an outlet to the high-pressure compressor, and selectively throttling air that has entered the intake system at a location upstream of the pierce point of the secondary EGR control loop to the intake system.

6. A method as set forth in claim 5 comprising controlling flow of exhaust gas through the primary EGR control loop by controlling a primary EGR valve in the primary EGR control loop and causing flow of exhaust gas through the primary EGR control loop to flow through a primary EGR cooler in the primary EGR control loop that is upstream of the primary EGR valve.

7. A method as set forth in claim 6 comprising introducing exhaust gas from the primary EGR control loop into the intake system downstream of a charge air cooler that is downstream of the high-pressure compressor.

8. A method as set forth in claim 7 comprising causing air from the low-pressure compressor to pass through an inter-stage cooler before entering the high-pressure compressor.

9. A method as set forth in claim 8 comprising selectively throttling air that has entered the intake system upstream of the pierce point of the secondary EGR control loop to the intake system.

10. A method as set forth in claim 8 comprising controlling flow of exhaust gas through the secondary EGR control loop by controlling a secondary EGR valve in the secondary EGR control loop.

Assignments (11)
RELEASE OF SECURITY INTEREST RECORDED AT REEL/FRAME 53545/443 Recorded Jul 15, 2021
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: NAVISTAR INTERNATIONAL CORPORATION; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC.
Reel/Frame 057441/0404 →
RELEASE OF SECURITY INTEREST Recorded Jul 2, 2021
From: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC. (F/KA/ INTERNATIONAL TRUCK AND ENGINE CORPORATION); INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC
Reel/Frame 056757/0136 →
CORRECTIVE ASSIGNMENT TO CORRECT THE CONVEYING PARTY DATA PREVIOUSLY RECORDED AT REEL: 052483 FRAME: 0742. ASSIGNOR(S) HEREBY CONFIRMS THE SECURITY INTEREST.. Recorded Apr 27, 2020
From: NAVISTAR INTERNATIONAL CORPORATION; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC. (F/K/A INTERNATIONAL TRUCK AND ENGINE CORPORATION)
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 053457/0001 →
SECURITY INTEREST Recorded Apr 27, 2020
From: NAVISTAR INTERNATIONAL CORPORATION; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC. (F/K/A INTERNATIONAL TRUCK AND ENGINE CORPORATION)
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 053545/0443 →
SECURITY INTEREST Recorded Apr 23, 2020
From: INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC. (F/K/A INTERNATIONAL TRUCK AND ENGINE CORPORATION)
To: JPMORGAN CHASE BANK, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 052483/0742 →
RELEASE OF SECURITY INTEREST Recorded Nov 10, 2017
From: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR, INC.; NAVISTAR INTERNATIONAL CORPORATION
Reel/Frame 044416/0867 →
SECURITY INTEREST Recorded Nov 10, 2017
From: NAVISTAR INTERNATIONAL CORPORATION; NAVISTAR, INC.
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 044418/0310 →
RELEASE OF SECURITY INTEREST Recorded Nov 10, 2017
From: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
To: NAVISTAR INTERNATIONAL CORPORATION; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC
Reel/Frame 044780/0456 →
SECURITY AGREEMENT Recorded Sep 15, 2015
From: NAVISTAR INTERNATIONAL CORPORATION; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC
To: JPMORGAN CHASE BANK N.A., AS COLLATERAL AGENT
Reel/Frame 036616/0243 →
SECURITY AGREEMENT Recorded Sep 12, 2012
From: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY, LLC; INTERNATIONAL TRUCK INTELLECTUAL PROPERTY COMPANY, LLC; NAVISTAR INTERNATIONAL CORPORATION; NAVISTAR, INC.
To: JPMORGAN CHASE BANK, N.A., AS COLLATERAL AGENT
Reel/Frame 028944/0730 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 4, 2009
From: LIU, ZHENGBAI; LEI, NING; ZHENG, JINCAI; ROWELLS, ROBERT L.
To: INTERNATIONAL ENGINE INTELLECTUAL PROPERTY COMPANY LLC
Reel/Frame 023469/0823 →