A description is given of an atomizer for gas turbines. It is a modification of existing liquid fuel atomizers incorporating a plug with tangential swirl grooves. To retain the quality of the spray under various loads the grooved plug is made of an elastic material. The plug compresses under an increased fuel pressure and forms an opening through which fuel also passes to the nozzle.

  • Supplemental Notes:
    • Edited Translation of Patent (USSR) 249 533 p-12 1969 by V. Mesenzeff
  • Corporate Authors:

    Foreign Technology Division

    Wright-Patterson Air Force Base
    Dayton, OH  United States  45433
  • Authors:
    • Belokrylov, A A
  • Publication Date: 1972-2-25


  • Russian

Media Info

  • Pagination: 6 p.

Subject/Index Terms

Filing Info

  • Accession Number: 00035595
  • Record Type: Publication
  • Source Agency: National Technical Information Service
  • Report/Paper Numbers: FID-HT-23-1425-71
  • Files: TRIS
  • Created Date: Oct 27 1973 12:00AM