Turbo compressor

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Plural rigidly related blade sets

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Details

4152083, 4152112, F01D 102

Patent

active

050627660

ABSTRACT:
A single-shaft multi-staged turbo compressor capable of compressing a gas at a large flow rate and with a high pressure ratio has a first impeller group composed of at least one oblique-flow impeller and a second impeller group composed of at least one centrifugal impeller. The impellers of the first and second groups are mounted on a common impeller shaft in a back-to-back relation.

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patent: 4844695 (1989-07-01), Banks et al.
patent: 4887940 (1989-12-01), Todoroki et al.

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