Valve actuator for turbocharger systems

Details Valve actuator for turbocharger systems Valve actuator for turbocharger systems

F - Mech Eng,Light,Heat,Weapons

02

B

F02B 37/18 (2006.01) F02B 37/013 (2006.01) F02B 37/16 (2006.01) F02M 25/07 (2006.01) F16K 31/124 (2006.01) F16K 31/163 (2006.01) F16K 31/54 (2006.01)

Patent

CA 2730087

A turbocharger system for an engine is provided. The turbocharger system includes a low pressure turbocharger that has a low pressure compressor and a low pressure turbine and a high pressure turbocharger that has a high pressure compressor and a high pressure turbine. The turbocharger system further includes a bypass valve for controlling a gas stream hi the turbocharger system. The bypass valve includes an actuator operable to control the bypass valve, and the actuator is an electronic solenoid controlled hydraulic actuator with a position feedback sensor to detect the position of the bypass valve.

L'invention concerne un système turbocompresseur destiné à un moteur. Le système turbocompresseur comprend un turbocompresseur à basse pression qui comporte un compresseur basse pression et une turbine basse pression, et un turbocompresseur haute pression qui comporte un compresseur haute pression et une turbine haute pression. Ce système turbocompresseur comprend de plus une vanne de dérivation pour réguler un écoulement gazeux dans le système turbocompresseur. La vanne de dérivation comprend un actionneur destiné à commander la vanne de dérivation, cet actionneur étant un solénoïde électronique commandé par un actionneur hydraulique et pourvu d'un capteur de rétroaction de position pour détecter la position de la vanne de dérivation.

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