Title:
A compact multistage type turbine pump
Document Type and Number:
Japanese Patent JP5918396
Kind Code:
B2
Abstract:
A turbo pump has a common axis of rotation for a plurality of compressor and turbine wheels. One or more of the turbine and compressor wheels defines a gas passage axially therethrough, said gas passage being associated with another of the turbine and compressor wheels. The arrangement provides a compact multi-stage turbocharger.
Inventors:
Olivier location
Application Number:
JP2014561378A
Publication Date:
May 18, 2016
Filing Date:
March 08, 2013
Export Citation:
Assignee:
JAGUAR LAND ROVER LIMITED
International Classes:
F04D17/12; F04D25/04
Domestic Patent References:
| JP62064828U |
Foreign References:
| US2595505 | ||||
| US5105616 | ||||
| US2611241 |
Attorney, Agent or Firm:
Axis International Patent Business Corporation
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