发明名称 Turbocharger control system
摘要 <p>An internal combustion engine is provided with at least one intake manifold and a turbocharger. The turbocharger includes a rotatable shaft; a turbine having a turbine wheel carried by the shaft; and a multi-stage compressor. The multi-stage compressor includes a first compressor wheel carried by the shaft, an axially extending first inlet associated with the first compressor wheel, a radially extending first outlet associated with the first compressor wheel, a second compressor wheel carried by the shaft, an axially extending second inlet associated with the second compressor wheel, a radially extending second outlet associated with the second compressor wheel, and an interstage duct fluidly interconnecting in series the first outlet associated with the first compressor wheel with the second inlet associated with the second compressor wheel. The second outlet is fluidly coupled with the intake manifold. One or more valves are each fluidly coupled with an ambient environment and the interstage duct or intake manifold. Each valve is adapted to open when a pressure of the ambient environment is less than a pressure within the interstage duct or intake manifold.</p>
申请公布号 EP1191229(A3) 申请公布日期 2003.05.02
申请号 EP20010117540 申请日期 2001.07.20
申请人 CATERPILLAR INC. 发明人 GLADDEN, JOHN R.
分类号 F02B33/44;F04D17/14;(IPC1-7):F04D27/00;F04D27/02;F04D25/04;F02B37/16 主分类号 F02B33/44
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