Small turbo compressor

F - Mech Eng,Light,Heat,Weapons – 04 – D

Patent

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Details

F04D 25/16 (2006.01) F01D 15/08 (2006.01) F01D 15/12 (2006.01) F04D 25/04 (2006.01)

Patent

CA 2325048

A multi-stage turbo compressor including a turbine driven by a high-pressure gas from a low-stage compressor's outlet; and a high-stage compressor driven by a power transmitted through an axis directly connected to the turbine. The gas that passed the turbine is returned to a first-stage compressor's inlet.

L'invention se rapporte à un turbocompresseur multi-étage comportant une turbine commandée par un gaz sous haute pression en provenance d'une sortie de compresseur d'étage inférieur, et un compresseur d'étage supérieur commandé par l'énergie transmise par un axe directement relié à la turbine. Le gaz qui a traversé la turbine est renvoyé vers une entrée de compresseur de premier étage.

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