Invention Grant
US07748218B2 System and method for achieving engine back-pressure set-point by selectively bypassing a stage of a two-stage turbocharger 有权
通过选择性地旁路两级涡轮增压器的级来实现发动机背压设定点的系统和方法

System and method for achieving engine back-pressure set-point by selectively bypassing a stage of a two-stage turbocharger
Abstract:
A control system for operating vanes of a turbocharger turbine (16T) and for operating a turbine-shunting bypass valve (22) according to a strategy wherein a processor executes an algorithm for selectively unenabling the control system to operate the bypass valve when the control system is operating the vanes to adjust exhaust back-pressure on the engine within a range of effectiveness for the vanes to control the exhaust back-pressure and enabling the control system to operate the bypass valve when the control system has operated the mechanism to a limit of the range of effectiveness.
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