Fuel-Air Burner,

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Abstract:

The fuel-air burner for a combustion chamber of gas turbine engine, consisting of a centrifugal atomizer and a swirler located between it and the housing is different in that to broaden the range of stable operation and to reduce the length and brightness of the flame a second swirler with a perforated nozzle, for example, converging nozzle with a perforation on the outlet part, is placed in the cup beyond the first swirler. Author

Author(s):
Markushin, N. A. ; Epeikin, L. F.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Patent (USSR) 230 557 p1-2 1969, by V. Mesenzeff.
Annotation:
Fuel-Air Burner--Translation.
Pagination:
0006

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-1426-71
 Subject Terms
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*COMBUSTION CHAMBERS, ENGINE FUEL SYSTEMS COMPONENTS), (*PATENTS, USSR), GAS TURBINES, FLAME PROPAGATION, NOZZLES, ATOMIZATION
Field(s)/Group(s):
Combustion and Ignition
Keyword(s):
TRANSLATIONS
Report Date:
1972 Feb 25