Accession Number:

AD0742695

Title:

Fuel-Air Burner,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1972-02-25

Pagination or Media Count:

6.0

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

Subject Categories:

  • Combustion and Ignition

Distribution Statement:

APPROVED FOR PUBLIC RELEASE