发明名称 |
Internal combustion engine with two-stage exhaust turbocharger and power output turbine |
摘要 |
In an internal combustion engine (1) with two-stage exhaust turbocharger (7 and 16; 9 and 11) and power output turbine (20), which can be coupled to the engine crankshaft (2) and driven by a portion of the engine exhaust gases, the outlet of the power output turbine (20) can be conductively connected by way of an exhaust gas recirculation line (28) to the inlet of the low pressure turbine (9) and the outlet of the high pressure compressor (16) can be connected to the high pressure exhaust line (5) upstream of the high pressure turbine (7) by way of a bypass line (36) in order to improve the partial load performance of the engine (1). The inflows of exhaust gas to the low pressure turbine (9) and of high pressure charge air to the high pressure turbine (7) by way of the exhaust gas lines (21, 28) and the bypass line (36) respectively are shut off or released by shut-off elements (22, 29, 37), which can be automatically controlled by known means as a function of the operating condition of the engine (1). <IMAGE>
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申请公布号 |
DE3807372(A1) |
申请公布日期 |
1989.09.21 |
申请号 |
DE19883807372 |
申请日期 |
1988.03.07 |
申请人 |
ASEA BROWN BOVERI AG, BADEN, AARGAU, CH |
发明人 |
MATHEY, CHRISTOPH, DIPL.-ING., WETTINGEN, CH |
分类号 |
F02B37/013;F02B37/16;F02B37/18;F02B41/10 |
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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