| 摘要 |
<p><P>PROBLEM TO BE SOLVED: To provide a method of easily, satisfactorily and economically solving a problem that components including a vane, flanges and shelves of a diffuser/guide vane assembly are highly expensive, and supply problems. <P>SOLUTION: The diffuser/guide vane assembly 10 for an aircraft turbojet or a turboprop engine comprises the diffuser 12 including annular flanges 22, 24 joined to each other by a blade 26, and a guide vane assembly 14 including cylindrical shelves 28, 30 joined to each other by a vane 32, the annular flanges and the cylindrical shelves formed of metal plates on which the vanes 26, 32 are assembled by brazing. <P>COPYRIGHT: (C)2008,JPO&INPIT</p> |
