INVESTIGATION OF AN INDEPENDENT COOLING SYSTEM FOR A GAS TURBINE,

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Abstract:

The necessity for experimental study on an autonomous cooling system for gas turbine rotor blades is examined. The design and technological peculiarities of a test facility for investigating a high-temperature turbine with an independent cooling system are described, and investigation problems are presented. Author

Author(s):
Manushin, E. A. ; Pugin, G. A.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited machine trans. of Izvestiya Vysshikh Uchebnykh Zavedenii. Mashinostroenie (USSR) n12 p135-140 1967.
Annotation:
Investigation of an independent cooling system for a gas turbine--Translation.
Pagination:
0014

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-MT-24-114-69
 Subject Terms
Modernization Areas:
Autonomy
Communities of Interest:
Autonomy
Descriptor(s):
(*GAS TURBINES, *COOLING), GAS TURBINE BLADES, HEAT TRANSFER, COOLANTS, USSR
Field(s)/Group(s):
Thermodynamics, Jet and Gas Turbine Engines
Keyword(s):
TRANSLATIONS
Report Date:
1969 May 22