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Investigation on NOx of a low emission combustor design with multihole premixer-prevaporizer

  • Yuzhen Lin*
  • , Yunhui Peng
  • , Gaoen Liu
  • *Corresponding author for this work

Research output: Contribution to conferencePaperpeer-review

Abstract

A low NOX emission combustor design was presented in this paper. The design features the premixer-prevaporizer tube with multihole and two stages arranged radially hi line, with the outer stage being pilot stage and inner stage being main stage. The multihole premixer and prevaporizer is a part of main stage. The results of NOX emission were provided and also compared with the baseline design that the premixer and prevaporizer tube without multihole. The double swirler prefilming airblast atomizer was installed in the premixed prevaporized duct entrance. The mean drop size and radial fuel flux distribution were measured to determine proper configurations of the multihole premixer-prevaporizer. NOX emission investigations were carried out using a test combustor with one pilot stage and one main stage under the operating condition of high inlet temperature (800K) and inlet air pressure was atmospheric pressure. The experiment results demonstrated large NOX emissions reduction of the multihole premixer-prevaporizer compared with the baseline design. The more even fuel-air mixing, which was gained by the multiple jets, intensified the fuel and air mixing within the premixer-prevaporizer, resulted in the large reduction of NOX emission. The configurations of multihole premixerprevaporizer had great influence on NOX emissions reduction.

Original languageEnglish
Pages73-80
Number of pages8
DOIs
StatePublished - 2004
Event2004 ASME Turbo Expo - Vienna, Austria
Duration: 14 Jun 200417 Jun 2004

Conference

Conference2004 ASME Turbo Expo
Country/TerritoryAustria
CityVienna
Period14/06/0417/06/04

Keywords

  • Aircraft engine
  • Combustion
  • Gas turbine engine
  • Low emission
  • NO

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