Two-stage turbo compressor

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

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F04D 1/08 (2006.01) F01D 1/14 (2006.01) F04D 17/12 (2006.01) F04D 29/28 (2006.01)

Patent

CA 1150208

ABSTRACT A two stage compressor and the like which comprises concentric first and second stage impellers, an inlet to and an outlet from each impeller stage, cross-over passages from the first outlet to the second inlet located crossing the first inlet, adjustable guide vanes in the first inlet and fixed de-swirl vanes in the first outlet, the inlet to the second stage impeller being located radially inwardly to that of the first stage impeller.

356961

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