DEVELOPMENT OF THE FUEL ATOMIZING DEVICE UTILIZING HIGH ROTATIONAL SPEED

A device developed for a combustor of a small gas turbine engine is a rotary atomizer in which liquid fuel is supplied through a stationary nozzle onto a shaped disc rotating with a high tangential velocity (over 200 m/sec). This paper discusses its application in an automotive gas turbine engine.

  • Supplemental Notes:
    • From ASME Meeting held March 9-12, 1981.
  • Corporate Authors:

    American Society of Mechanical Engineers

    Two Park Avenue
    New York, NY  United States  10016-5990
  • Authors:
    • Morishita, T
  • Publication Date: 1981

Media Info

Subject/Index Terms

Filing Info

  • Accession Number: 00345170
  • Record Type: Publication
  • Source Agency: Engineering Index
  • Report/Paper Numbers: ASME 81-GT-180
  • Files: TRIS
  • Created Date: Jan 29 1982 12:00AM