发明名称 |
Two-stage turbocharged engine system |
摘要 |
A two-stage turbocharged engine system is provided. The two-stage turbocharged engine system includes an internal combustion engine, a high-pressure turbocharger having a high-pressure turbine for rotating a high-pressure compressor through a connecting shaft, and a low-pressure turbocharger having a low-pressure turbine for rotating a low-pressure compressor by a connecting shaft. The two-stage turbocharged engine system also includes a low-pressure intake line for fluidly connecting the outlet of low-pressure compressor to the inlet of high-pressure compressor, a high-pressure intake line for fluidly connecting the outlet of high-pressure compressor to an air cooler, and a bypass device for selectively fluidly connecting a first branching point located in low-pressure intake line to a second branching point located in high-pressure intake line to thereby bypass the high-pressure compressor. The bypass device is located closer to the low-pressure compressor than to the high-pressure compressor.
|
申请公布号 |
US8534066(B2) |
申请公布日期 |
2013.09.17 |
申请号 |
US20100860264 |
申请日期 |
2010.08.20 |
申请人 |
CAVALLO ROBERTO;GOLISANO ROBERTO;BORETTO GIANMARCO;MANTA EUGENIO;GM GLOBAL TECHNOLOGY OPERATIONS LLC |
发明人 |
CAVALLO ROBERTO;GOLISANO ROBERTO;BORETTO GIANMARCO;MANTA EUGENIO |
分类号 |
F02B33/44;F01D5/10;F01D5/16;F01D17/10;F01D25/04;F02B33/00;F02B37/00;F02B37/013;F04D29/66 |
主分类号 |
F02B33/44 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|