Study on Stage of Centrifugal Compressor with Air Turbine,

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Abstract:

Discussed briefly in this article is the scheme of a centrifugal compressor with an air turbine, which replaces the bladed diffuser. A brief description is given of the experimental device and the experimental characteristics of this stage. Investigated is the problem of optimizing parameters in the given compressor. Author

Author(s):
Yanson, R. A.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Mashinostroyeniye (USSR) n7 p91-95 1966, by Marilyn Olaechea.
Annotation:
Study on Stage of Centrifugal Compressor with Air Turbine--Translation.
Pagination:
0016

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-ID(RS)I-0759-77
 Subject Terms
Joint Capability Areas:
JCA_3.2_Engagement; JCA_3_Force Application
Communities of Interest:
Energy and Power Technologies
Descriptor(s):
*GAS TURBINES, *CENTRIFUGAL COMPRESSORS, USSR, COMPUTATIONS, AIR FLOW, EFFICIENCY, GAS DYNAMICS, TURBINE BLADES, FLOW RATE, POWER SUPPLIES, HIGH PRESSURE COMPRESSORS, TRANSLATIONS, STAGING, DIFFUSERS, COMPRESSION RATIO, IMPELLERS
Field(s)/Group(s):
Hydraulic and Pneumatic Equipment, Jet and Gas Turbine Engines
Report Date:
1977 May 04