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
Descriptors:
Subject Categories:
- Combustion and Ignition