Technology Research on Gas Turbine Combustor Utilizing Melt-Growth Composite Ceramics

  • Konoshita, Yasuhiro (Gas Turbine Research and Development Center Kawasaki Heavy Industries, Ltd.) ;
  • Hagari, Tomoko (Gas Turbine Research and Development Center Kawasaki Heavy Industries, Ltd) ;
  • Matsumotoi, Kiyoshi (Gas Turbine Research and Development Center Kawasaki Heavy Industries, Ltd) ;
  • Ogata, Hideki (Gas Turbine Research and Development Center Kawasaki Heavy Industries, Ltd) ;
  • Ishida, Katsuhiko (Gas Turbine Research and Development Center Kawasaki Heavy Industries, Ltd.)
  • Published : 2004.03.01

Abstract

"Research and Development of Melt-Growth Composite (MGC) Ultra High Efficiency Gas Turbine System Technology" program has been started in JFY2001. The main objective of the program is to establish basic component technologies to apply MGC material to an efficient gas turbine system successfully. It is known that MGC material maintains its mechanical strength at room temperature up to about 2000 K, which is ideal for the high temperature gas turbine. The purposes of the present study are to develop the cooling structure of the gas turbine combustor liner where MGC material is applied as the heat shield panel, also to develop the low NOx combustion system for a 1970 K (1700 deg.C) class gas turbine combustor. To start with, basic heat transfer characteristics were investigated by one-dimensional calculation and heat transfer experiment for the cooling structure. Axially staged configuration and fuel preparation were investigated by CFD calculation and experiments for the low NOx combustor.

Keywords