| 摘要 |
PROBLEM TO BE SOLVED: To provide a fastener of a gas turbine engine for attaching members made of different materials. SOLUTION: A fastener assembly for joining members made of different materials includes a fastener 13, a spacer 138, and a mechanism fastening the assembly. The spacer absorbs difference of thermal expansion between the members while providing firm joint between a non-metal member 38 and a metal member 40. An opening part 64 is an oblong hole shape slot provided in the metal member 40 and stores a main body part 148 of the fastener 134 penetrating the opening part 64 and the spacer 138, and enables relative movement between the non-metal member 38 and the metal member 40. COPYRIGHT: (C)2006,JPO&NCIPI |
