| 摘要 |
<P>PROBLEM TO BE SOLVED: To provide a gas turbine rotor blade optimized in weight, without losing efficiency in a process. <P>SOLUTION: The problem is solved by forming respective dimensions of individual parts 16, 17 and 18 extremely smaller than assembled rotor blades 10 and 20. <P>COPYRIGHT: (C)2010,JPO&INPIT |
