Fuel-Air Burner,
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)
Document Details
- Document Type
- Technical Report
- Publication Date
- Feb 25, 1972
- Accession Number
- AD0742695
Entities
People
- L. F. Epeikin
- N. A. Markushin
Organizations
- National Air and Space Intelligence Center