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.

  • Supplemental Notes:
    • Edited translation of Patent (USSR) 230 557 pages 1-2 1969 by V. Mesenzeff.
  • Corporate Authors:

    Foreign Technology Division

    Wright-Patterson Air Force Base
    Dayton, OH  United States  45433
  • Authors:
    • Markushin, N A
    • Epeikin, L F
  • Publication Date: 1972-2-25

Media Info

  • Pagination: 6 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00035608
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: FTD-HT-23-1426- 71
  • Files: TRIS
  • Created Date: Oct 27 1973 12:00AM