Title:
多段ターボ機械
Document Type and Number:
Japanese Patent JP7394830
Kind Code:
B2
Abstract:
This multi-stage turbomachine comprises:a central part (2) having at least two bearings (6) from which part there extends at least on one side a shaft (4) guided by said bearings (6) and on which shaft there are mounted, in cantilever fashion, two radial wheels (22, 34), the two radial wheels (22, 34) are separated from one another by a leak-tight partition (32), andeach of the two radial wheels (22, 34) is mounted in its casing (24, 32, 40), each casing having a dedicated fluid inlet (24a, 42) and a dedicated fluid outlet (24b, 44).
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Inventors:
Bogey, Jack
Application Number:
JP2021504241A
Publication Date:
December 08, 2023
Filing Date:
July 10, 2019
Export Citation:
Assignee:
Cryostar Societe Pearl Axion Saint Prifier
International Classes:
F04D29/42; F04D17/12
Domestic Patent References:
| JP2012251528A | ||||
| JP2007177695A |
Foreign References:
| US20170335756 | ||||
| US20170175754 | ||||
| WO2016193002A1 |
Attorney, Agent or Firm:
Patent Attorney Corporation Asamura Patent Office