| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide gas turbine engine nozzles (26, 28, 30). <P>SOLUTION: The gas turbine engine nozzles (26, 28, 30) include respectively at least one-nozzle blades (54, 56, 58 60) including the first end part and the second end part, the first end part is coupled to inner sidewalls (32, 70), the second end part is coupled to outer sidewalls (34, 72), at least one of stress removing pockets (110, 120) is defined in an inside of at least one of the inner sidewall and the outer sidewall, to be adjacent to the at least one nozzle blade, and the at least one stress removing pocket reduces easily the stress generated in the nozzle blade. <P>COPYRIGHT: (C)2010,JPO&INPIT</p> |
