| 摘要 |
PROBLEM TO BE SOLVED: To provide a stator vane segment and tip shroud segment assembly. SOLUTION: The stator vane segment and tip shroud segment assembly 10 comprises: two or more vanes 12, each having an airfoil portion 16 and a radially inner tip 20, each tip being formed with at least one radially inwardly projecting tenon 18; and a tip shroud segment 26 extending over the radially inner tips of the vanes. In this case, the tip shroud segment 26 is formed with two or more holes 28, and each hole is fitted with a bushing 34 that receives one of the tenons 18, respectively. COPYRIGHT: (C)2007,JPO&INPIT
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