Aircraft engine mounting arrangement on an engine pylon

摘要

The system comprises main fastening system (18,24) which allows effort transmission in two directions: parallel to motor axi (OX') and perpendicular (OY') to it. It comprises also additional safety fastening system, which has part (10) in common with ma system. There are two distinct parts (10a, 10b) able to transmit stress in favorite directions and pin (42) which contacts motor housing (C) and allows transmission of stress in direction (OZ) if main fastening system is out of use.