发明名称 VARIABLE GEOMETRY TURBOCHARGER HAVING INTERNAL BYPASS EXHAUST GAS FLOW.
摘要 <p>Variable geometry turbochargers (10) comprise a turbine housing (12) having an exhaust gas inlet (14) and outlet (16), a volute connected to the inlet, and a nozzle wall (24) adjacent the volute. A turbine wheel (17) is carried within the turbine housing and is attached to a shaft (18). A plurality of movable vanes (22) are disposed within the turbine housing adjacent the nozzle wall, and are positioned between the exhaust gas inlet and turbine wheel. The turbine housing includes a bypass exhaust gas flow port (102) disposed internally therein having an inlet opening (110) positioned upstream from the turbine wheel, and a outlet opening (112) positioned downstream from the turbine wheel. The vanes are positioned adjacent respective bypass ports with inlet openings covered by a respective vane when the vane is place in a closed position. The inlet opening is exposed for facilitating bypass exhaust gas flow through the turbocharger when the respective vane is actuated or moved into an open position. The turbine housing may also comprise a specially configured nozzle wall terminal edge designed to work with vanes having a recessed underside surface to permit additional bypass exhaust gas flow within the turbocharger when the vanes are actuated in an open position.</p>
申请公布号 MXPA05000037(A) 申请公布日期 2005.04.08
申请号 MX2005PA00037 申请日期 2003.06.24
申请人 HONEYWELL INTERNATIONAL, INC. 发明人 ARNOLD, STEVEN, DON
分类号 F01D9/02;F01D5/14;F01D5/18;F01D17/10;F01D17/16;F02B37/18;F02B37/24;F02C6/12;(IPC1-7):F01D17/10 主分类号 F01D9/02
代理机构 代理人
主权项
地址