发明名称 |
TWO-STAGE TURBOCHARGED ENGINE |
摘要 |
A turbocharged internal combustion engine (1) is disclosed that may comprise an engine block (10) with a first end side (18L) opposing a second end side (18H) and a two-stage turbocharged system (12). The two-stage turbocharged system (12) may comprise a low-pressure turbocharger (26) with a first turbine (T L ) and a first compressor (C L ) and a high-pressure turbocharger (28) with a second turbine (T H ) and a second compressor (C H ). A turbine connection (35) may fluidly connect the first turbine (T L ) and the second turbine (T H ) and a compressor connection (34) fluidly connects the first compressor (C L ) and the second compressor (C H ). The low-pressure turbocharger (26) is mounted at the first end side (18L) of the engine block (10) and the high-pressure turbocharger (28) is mounted at a second end side (18H) of the engine block (10). |
申请公布号 |
KR20130096263(A) |
申请公布日期 |
2013.08.29 |
申请号 |
KR20137005671 |
申请日期 |
2011.08.05 |
申请人 |
CATERPILLAR MOTOREN GMBH & CO. KG |
发明人 |
SCHLEMMER KELLING UDO |
分类号 |
F02B37/013;F01N3/20;F02B37/02;F02B37/18 |
主分类号 |
F02B37/013 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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