Systems and methods for dedicated exhaust gas recirculation and control
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F02D-041/00
F02M-025/07
출원번호
US-0744928
(2013-01-18)
등록번호
US-9032940
(2015-05-19)
발명자
/ 주소
Dane, Marten H.
Geckler, Samuel C.
Talwar, Sudhanshu
출원인 / 주소
Cummins Inc.
대리인 / 주소
Krieg DeVault LLP
인용정보
피인용 횟수 :
2인용 특허 :
7
초록▼
Systems and methods for exhaust gas recirculation are provided. The system includes a dedicated exhaust gas recirculation loop for recirculating exhaust gas flow from at least one dedicated cylinder of an engine into an intake system prior to combustion. The system further includes a low pressure ex
Systems and methods for exhaust gas recirculation are provided. The system includes a dedicated exhaust gas recirculation loop for recirculating exhaust gas flow from at least one dedicated cylinder of an engine into an intake system prior to combustion. The system further includes a low pressure exhaust gas recirculation loop for increasing the exhaust gas recirculation amount above that provided by the dedicated exhaust gas recirculation loop.
대표청구항▼
1. A method, comprising: operating an internal combustion engine including a plurality of cylinders, an exhaust system, and an intake system, at least one of the plurality of cylinders being operably connected to only provide exhaust flow to a dedicated exhaust gas recirculation system and a remaini
1. A method, comprising: operating an internal combustion engine including a plurality of cylinders, an exhaust system, and an intake system, at least one of the plurality of cylinders being operably connected to only provide exhaust flow to a dedicated exhaust gas recirculation system and a remaining portion of the plurality of cylinders being operably connected to provide exhaust flow to the exhaust system;determining an amount of recirculated exhaust gas to include in a charge flow to the internal combustion engine during operation;providing a first portion of the amount of recirculated exhaust gas with exhaust flow from the dedicated exhaust gas recirculation system; and providing a remaining portion of the amount of recirculated exhaust gas from exhaust flow in the exhaust system through a low pressure exhaust gas recirculation loop connecting the exhaust system to the intake system, wherein the low pressure exhaust gas recirculation loop is connected to the intake system upstream of a compressor in the intake system and downstream of a turbine in the exhaust system. 2. The method of claim 1, wherein the dedicated exhaust gas recirculation system is connected to the intake system downstream of the compressor. 3. The method of claim 1, wherein the dedicated exhaust gas recirculation system includes a flow control valve operable to control the first portion of the amount of recirculated exhaust gas. 4. The method of claim 1, wherein the low pressure exhaust gas recirculation system includes a flow control valve operable to control the remaining portion of the amount of recirculated exhaust gas. 5. A method, comprising: operating an engine having a plurality of cylinders and a turbocharger including a turbine and a compressor;directing a charge flow into the plurality of cylinders from an intake system, the compressor being connected to the intake system;combusting a mixture of the charge flow and fuel within the plurality of cylinders to generate a power output and a flow of exhaust;directing a first portion of the flow of exhaust to a dedicated exhaust gas recirculation system to mix with the charge flow in the intake system prior to combustion, wherein the first portion of the flow of exhaust is created by combustion in at least one of the plurality of cylinders dedicated to providing only the first portion of the flow of exhaust;directing a first part of a second portion of the flow of exhaust to the intake system to mix with the charge flow, wherein the turbine receives the second portion of the flow of exhaust; anddirecting a second part of the second portion of the flow of exhaust to an exhaust outlet, wherein the second portion of the flow of exhaust is created by combustion in a plurality of cylinders not dedicated to exhaust gas recirculation, wherein:the first part of the second portion of the flow of exhaust is recirculated in a low pressure exhaust gas recirculation system; andthe low pressure exhaust gas recirculation system is connected downstream of the turbine and upstream of the compressor. 6. The method of claim 5, further comprising controlling the first part of the second portion of the flow of exhaust with a flow control valve. 7. The method of claim 6, further comprising controlling the first portion of the flow of exhaust with a second flow control valve. 8. The method of claim 5, wherein directing the first part of the second portion of the flow of exhaust to the intake system to mix with the charge flow includes determining that a target exhaust gas recirculation fraction of the charge flow exceeds the amount of recirculated exhaust gas that can be provided from the dedicated exhaust gas recirculation system. 9. A system, comprising: an engine including a plurality of cylinders;an intake system configured to direct a charge flow to all of the plurality of cylinders;an exhaust system configured to receive exhaust from a first portion of the plurality of cylinders and selectively direct a portion of the exhaust from the first portion of the plurality of cylinders to a low pressure exhaust gas recirculation system connected to the intake passage; anda dedicated exhaust gas recirculation system configured to receive exhaust only from a second portion of the plurality of cylinders and direct the exhaust from the second portion of the plurality of cylinders to the intake passage, wherein the first portion of the plurality of cylinders is dedicated entirely to providing exhaust to a turbocharger system. 10. The system of claim 9, wherein the second portion of the plurality of cylinders is dedicated entirely to providing exhaust to the intake passage. 11. The system of claim 9, wherein the low pressure exhaust gas recirculation system is connected downstream of a turbine of the turbocharger system and upstream of a compressor of the turbocharger system. 12. The system of claim 9, wherein the second portion of the plurality of cylinders consists of no more than one third of the plurality of cylinders. 13. The system of claim 12, wherein the first portion of the plurality of cylinders includes at least two cylinders. 14. The system of claim 9, further including: a first control valve between the low pressure exhaust gas recirculation system to the intake system; anda second control valve configured to regulate exhaust flow through the dedicated exhaust gas recirculation system. 15. A system, comprising: an engine including a plurality of cylinders;an intake system configured to direct a charge flow to all of the plurality of cylinders;an exhaust system configured to receive exhaust from a first portion of the plurality of cylinders and selectively direct a portion of the exhaust from the first portion of the plurality of cylinders to a low pressure exhaust gas recirculation system connected to the intake passage;a dedicated exhaust gas recirculation system configured to receive exhaust only from a second portion of the plurality of cylinders and direct the exhaust from the second portion of the plurality of cylinders to the intake passage;a first control valve between the low pressure exhaust gas recirculation system to the intake system; anda second control valve configured to regulate exhaust flow through the dedicated exhaust gas recirculation system, wherein the first control valve is connected to the exhaust passage downstream of a turbocharger in the exhaust passage.
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