| 摘要 |
PROBLEM TO BE SOLVED: To provide a method of joining titan-based metal parts to each other for solving problems in a joining method by a publicly known silicone elastomer and a gas turbine compressor nozzle ring formed by the method. SOLUTION: The titan-based metal parts 1 and 3 are brazed to each other by using, as a filler metal 7, an aluminum alloy containing magnesium but not substantially containing silicon. This method is used when a blade 3 is joined to the inner shroud 1 of the compressor nozzle ring of a gas turbine engine for aircraft. COPYRIGHT: (C)2005,JPO&NCIPI |
