| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide an airfoil part profile for a manufactured article, i.e., a compressor. <P>SOLUTION: The manufactured article has a reference contour substantially following the values of the Cartesian coordinates of X, Y, Z in table 1 (not shown). In table 1 (not shown), X and Y indicate distances in inches forming airfoil part profile sections at every distance Z in inches when connected with a smooth continuous circular arc. The profile sections at the distance Z are smoothly connected to one another to form a complete airfoil part profile 22 or 23. <P>COPYRIGHT: (C)2008,JPO&INPIT</p> |
