Accession Number : AD0742695

Title :   Fuel-Air Burner,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Markushin,N. A. ; Epeikin,L. F.

Report Date : 25 FEB 1972

Pagination or Media Count : 6

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)

Descriptors :   (*COMBUSTION CHAMBERS, ENGINE FUEL SYSTEMS COMPONENTS), (*PATENTS, USSR), GAS TURBINES, FLAME PROPAGATION, NOZZLES, ATOMIZATION

Subject Categories : Combustion and Ignition

Distribution Statement : APPROVED FOR PUBLIC RELEASE