Low speed high pressure ratio turbocharger

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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F02C 6/12 (2006.01) F04D 25/04 (2006.01) F04D 29/28 (2006.01)

Patent

CA 2337790

A low speed high pressure ratio turbocharger incorporates a compressor impeller having impeller blades for a first stage of compression mounted on a first side of the wheel and impeller blades for a second stage of compression mounted on a second side of the wheel. Driving the dual sided compressor impeller on a common shaft from the turbine wheel allows reduction in rotational speeds while increasing compression ratio of the turbine. The scroll inlet and outlet volute for the second stage inducer are integrated with the compressor housing or other portions of the turbocharger case for compact packaging.

L'invention concerne un turbocompresseur à faible vitesse et à rapport de pression élevé, qui comprend une roue à aubes avec aubage monté sur un premier côté de la roue pour une première étape de compression et aubage monté sur un second côté de la roue pour une seconde étape de compression. En entraînant cette roue à double aubage sur un arbre commun de la roue de turbine, on peut réduire les vitesses de rotation tout en augmentant le rapport de compression de la turbine. Afin d'assurer une configuration compacte, on intègre au carter de compresseur ou à d'autres parties du carter du turbocompresseur l'entrée hélicoïdale et la volute de sortie pour l'aubage d'alimentation de la seconde étape.

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