Device for controlling a variable inlet nozzle of a turbine

摘要

A variable geometry turbine (1), particularly for a supercharger turbocompressor (2) of an internal combustion engine, comprising an outer housing (3) forming a spiral inlet channel (6) for an operating fluid, a rotor (4) supported in a rotary manner in the housing (3), and an annular vaned nozzle (10) of variable geometry interposed radially between the channel (6) and the rotor (4) and comprising a control member (14) moving axially in order to control of the flow of the operating fluid from the channel (6) to the rotor (4), the control member (14) being formed as an annular piston of a fluid actuator (20) actuated directly by means of a control pressure. <IMAGE>