NOZZLE ASSEMBLY FOR A SMALL GAS TURBINE,

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Abstract:

An Author Certificate has been issued for a nozzle assembly for a small gas turbine with nozzles having an annular cross section whose leading or trailing edges are intersected by the corresponding edges of the preceding nozzle. To secure a uniform supply of the working fluid to the inlet section of the rotor blades, the nozzles are arranged in two or several rows. Author

Author(s):
Dumov, V. I. ; Arinushkin, L. S. ; Vainbaum, I. F. ; Mikhailov, Yu. N. ; Emin, O. N.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Patent (USSR) 205 466 p1-2, 28 May 66, by J. Sechovicz.
Annotation:
Nozzle assembly for a small gas turbine--Translation.
Pagination:
0006

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-1494-68
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
*GAS TURBINES, *ANNULAR NOZZLES, GAS TURBINE NOZZLES, PATENTS, NOZZLE GAS FLOW, OPTIMIZATION, USSR
Field(s)/Group(s):
Jet and Gas Turbine Engines
Keyword(s):
TRANSLATIONS
Report Date:
1969 Apr 29