| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a structure that strikes a balance between a low NOx and high combustion stability in a gas turbine combustor. <P>SOLUTION: The combustor includes: a fuel nozzle 31 that ejects a fuel ; an air-hole plate including air-holes 34, 35 that eject the fuel and air ejected from the fuel nozzle 31; and a combustion chamber 7 for executing combined combustion of the fuel and air supplied from the air holes 34, 35, at least one of the air holes 35 having more exits than entrances. <P>COPYRIGHT: (C)2012,JPO&INPIT |
