发明名称 Multi-stage turbocharger system
摘要 <p>A turbocharger system comprises a first relatively small high-pressure (HP) turbocharger (1) and a second relatively large low pressure (LP) turbocharger (2). The turbine (6) of the LP turbocharger (2) is connected in series downstream of the turbine (4) of the HP turbocharger (1) in a first exhaust gas passage (11). An exhaust bypass flow passage (12) provides a bypass flow path around the HP turbine (4). A rotary valve (8) is located at a junction of the bypass flow passage (12) and a first exhaust gas flow passage (11). The rotary valve (8) comprises a valve rotor (19) which is rotatable to selectively permit or block flow to the LP turbine (6) from either the first exhaust gas passage (11) or the bypass gas passage (12).</p>
申请公布号 GB0615143(D0) 申请公布日期 2006.09.06
申请号 GB20060015143 申请日期 2006.07.29
申请人 CUMMINS TURBO TECHNOLOGIES LIMITED 发明人
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