公开(公告)号：US20150337717A1

公开(公告)日：2015-11-26

申请号：US14814832

申请日：2015-07-31

申请人： Cummins Turbo Technologies Limited

发明人： Lee J. Robinson ,  Daniel M. Acker

IPC分类号： F02B37/00 ,  F02B37/18 ,  F02B37/013

CPC分类号： F02B37/004 ,  F02B37/013 ,  F02B37/16 ,  F02B37/18 ,  F02B37/183 ,  F02D9/06 ,  F02D9/16 ,  F02M26/08 ,  Y02T10/144

摘要： A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger and a second relatively large low pressure (LP) turbocharger. The turbine of the LP turbocharger is connected in series downstream of the turbine of the HP turbocharger. A first exhaust bypass flow passage provides a bypass flow path around the HP turbine. A second exhaust bypass flow passage provides a bypass flow path around the LP turbine. A rotary valve is located at a junction of the first and second bypass flow passages and a first exhaust gas flow passage. The rotary valve comprises a valve rotor which is rotatable selectively to permit or block flow to the LP turbine and to permit or block flow to the first and second bypass paths.

公开(公告)号：US20170101925A1

公开(公告)日：2017-04-13

申请号：US15387895

申请日：2016-12-22

申请人： Cummins Turbo Technologies Limited

发明人： Lee J. Robinson ,  Daniel M. Acker ,  Akram Ghassan Khatib ,  Nandha Kumar Manoharan ,  Simon James Davis

IPC分类号： F02B37/18 ,  F02B37/013 ,  F16K11/06 ,  F02B37/00

CPC分类号： F02B37/183 ,  F02B37/004 ,  F02B37/013 ,  F02B37/16 ,  F02B37/18 ,  F02D9/06 ,  F02D9/16 ,  F02M26/08 ,  F16K11/06 ,  Y02T10/144

摘要： A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger and a second relatively large low pressure (LP) turbocharger. The turbine of the LP turbocharger is connected in series downstream of the turbine of the HP turbocharger. A first exhaust bypass flow passage provides a bypass flow path around the HP turbine. A second exhaust bypass flow passage provides a bypass flow path around the LP turbine. A rotary valve is located at a junction of the first and second bypass flow passages and a first exhaust gas flow passage. The rotary valve comprises a valve rotor which is rotatable selectively to permit or block flow to the LP turbine and to permit or block flow to the first and second bypass paths.

公开(公告)号：US10054037B2

公开(公告)日：2018-08-21

申请号：US14814832

申请日：2015-07-31

申请人： Cummins Turbo Technologies Limited

发明人： Lee J. Robinson ,  Daniel M. Acker

IPC分类号： F02B37/18 ,  F02D9/16 ,  F02B37/00 ,  F02B37/013 ,  F02B37/16 ,  F02D9/06 ,  F02M26/08

CPC分类号： F02B37/004 ,  F02B37/013 ,  F02B37/16 ,  F02B37/18 ,  F02B37/183 ,  F02D9/06 ,  F02D9/16 ,  F02M26/08 ,  Y02T10/144

摘要： A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger and a second relatively large low pressure (LP) turbocharger. The turbine of the LP turbocharger is connected in series downstream of the turbine of the HP turbocharger. A first exhaust bypass flow passage provides a bypass flow path around the HP turbine. A second exhaust bypass flow passage provides a bypass flow path around the LP turbine. A rotary valve is located at a junction of the first and second bypass flow passages and a first exhaust gas flow passage. The rotary valve comprises a valve rotor which is rotatable selectively to permit or block flow to the LP turbine and to permit or block flow to the first and second bypass paths.

公开(公告)号：US09995207B2

公开(公告)日：2018-06-12

申请号：US15387895

申请日：2016-12-22

申请人： Cummins Turbo Technologies Limited

发明人： Lee J. Robinson ,  Daniel M. Acker ,  Akram Ghassan Khatib ,  Nandha Kumar Manoharan ,  Simon James Davis

IPC分类号： F02D23/00 ,  F02B37/18 ,  F02B37/00 ,  F02B37/013 ,  F16K11/06

CPC分类号： F02B37/183 ,  F02B37/004 ,  F02B37/013 ,  F02B37/16 ,  F02B37/18 ,  F02D9/06 ,  F02D9/16 ,  F02M26/08 ,  F16K11/06 ,  Y02T10/144

摘要： A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger and a second relatively large low pressure (LP) turbocharger. The turbine of the LP turbocharger is connected in series downstream of the turbine of the HP turbocharger. A first exhaust bypass flow passage provides a bypass flow path around the HP turbine. A second exhaust bypass flow passage provides a bypass flow path around the LP turbine. A rotary valve is located at a junction of the first and second bypass flow passages and a first exhaust gas flow passage. The rotary valve comprises a valve rotor which is rotatable selectively to permit or block flow to the LP turbine and to permit or block flow to the first and second bypass paths.