发明名称 System to inhibit surge in the multi-stage compressor of a turbocharger
摘要 <p>A turbocharger (12) system for an internal combustion engine (10) is provided with at least one rotatable shaft (24) and a multi-stage compressor (20). The multi-stage compressor (20) includes a first compressor wheel (32) carried by a corresponding shaft (24), an axially extending first inlet (36) associated with the first compressor wheel (32), a radially extending first outlet (38) associated with the first compressor wheel (32), a second compressor wheel (34) carried by a corresponding shaft (24), an axially extending second inlet (40) associated with the second compressor wheel (34), and a radially extending second outlet (42) associated with the second compressor wheel (34). An interstage duct (44) fluidly interconnects in series the first outlet (38) associated with the first compressor wheel (32) with the second inlet (36) associated with the second compressor wheel (34). At least one bypass duct (46, 48, 50, 52, 54, 56, 58) is provided, with each bypass duct (46, 48, 50, 52, 54, 56, 58) fluidly interconnecting the first outlet (38) with the first inlet (36); the first outlet (38) with an ambient environment; and/or the second outlet (42) with the first outlet (38). At least one valve (60) is provided, each valve (60) being positioned within a corresponding bypass duct. A controller (14) is coupled with each valve (60) and selectively actuates each valve (60). &lt;IMAGE&gt;</p>
申请公布号 EP1191208(A2) 申请公布日期 2002.03.27
申请号 EP20010118590 申请日期 2001.08.02
申请人 CATERPILLAR INC. 发明人 GLADDEN, JOHN;WU, MIN
分类号 F02B37/013;F02B37/16;(IPC1-7):F02C9/18;F02C9/28 主分类号 F02B37/013
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