FUEL-AIR BURNER

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

• TRT Terms: Burners; Fuel system components; Gas turbines; Nozzles
• Old TRIS Terms: Fuel atomization; Fuel spray nozzles
• Subject Areas: Marine Transportation; Vehicles and Equipment;

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