发明名称 SUPERCHARGED INTERNAL COMBUSTION ENGINE WITH EXHAUST-GAS TURBOCHARGER AND METHOD FOR OPERATING AN INTERNAL COMBUSTION ENGINE OF SAID TYPE
摘要 Embodiments for inducing swirl upstream of a compressor are provided. In one example, a method includes during a first condition, flowing exhaust gas from downstream of a turbine to upstream of a compressor via a tangential flow duct of an exhaust gas recirculation (EGR) injector circumferentially surrounding an intake passage upstream of the compressor, and during a second condition, flowing exhaust gas from downstream of the turbine to upstream of the compressor via a radial flow duct of the EGR injector.
申请公布号 US2016047324(A1) 申请公布日期 2016.02.18
申请号 US201514812837 申请日期 2015.07.29
申请人 Ford Global Technologies, LLC 发明人 Kemmerling Joerg;Kindl Helmut Matthias;Smiljanovski Vanco;Sommerhoff Franz Arnd;Kuske Andreas
分类号 F02D41/00;F02M25/07;F02B39/00 主分类号 F02D41/00
代理机构 代理人
主权项 1. A supercharged internal combustion engine having an intake system for supply of charge air, an exhaust-gas discharge system for discharge of exhaust gas, at least one exhaust-gas turbocharger which comprises a turbine arranged in the exhaust-gas discharge system and a compressor arranged in the intake system, the compressor being equipped with at least one impeller which is mounted on a rotatable shaft in a compressor housing, an exhaust-gas recirculation arrangement comprising a recirculation line system which branches off from the exhaust-gas discharge system downstream of the turbine of the at least one exhaust-gas turbocharger and which opens out into the intake system upstream of the at least one compressor impeller, and an additional exhaust-gas recirculation arrangement which comprises a line which branches off from the exhaust-gas discharge system upstream of the turbine and which opens out into the intake system again downstream of the compressor, wherein the recirculation line system comprises at least two annular ducts which surround the intake system in spiral form at least in sections upstream of the at least one compressor impeller, with multiple ducts extending from each annular duct, said ducts each being connected in terms of flow at an intake side, by way of an inlet opening, to the intake system, a first annular duct of the at least two annular ducts has ducts which, at least at the intake side, are oriented substantially radially with respect to the shaft of the compressor and thus, in a virtual elongation, intersect the shaft, and a second annular duct of the at least two annular ducts has ducts which, at least at the intake side, are oriented in the manner of a secant and thus, in a virtual elongation, run with a spacing to the shaft of the compressor.
地址 Dearborn MI US