Experimental Study on High Loading Combustor for Lift Jet Engine PUBLIC ACCESS

[+] Author Affiliations
Kuniyasu Yamanaka

Heavy Industries Co., Ltd., Tokyo, Japan

Paper No. 72-GT-99, pp. V001T01A097; 14 pages
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show
  • San Francisco, California, USA, March 26–30, 1972
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7981-8
  • Copyright © 1972 by ASME


This paper deals with the parameters to specify a performance of a spray-type combustor which is a high loading combustor for a lift jet engine. The mixing parameter to control a combustion efficiency was obtained analytically by means of simplifying a primary zone, and its effectiveness was confirmed experimentally. The combustor geometry used for the test was 90-deg sector model of an annular type, the 42 combinations of different seven swirlers and six deflectors were tested systematically. The maximum combustion loading of 2.0 × 107 Btu/hr/cu ft combustion volume per atmosphere was obtained.

Copyright © 1972 by ASME
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