Spigot fastener comprising means for measuring the loads generated by an aircraft engine.

摘要

The fastener (1) has a part (2) whose end is secured to another part (14) i.e. single piece. An end (9) of the latter part is separated from the former part by a distance. An opposite end (10) of the latter part fits into a recess (4) of a third part (3) via a protrusion (11) such that force along two axes is transmitted by the former part to the third part by using the latter part. A measuring unit measures the force and is mounted on one of the three parts. A shaft (15) is positioned in parallel to a third axis. A flange (8) is a part connected to the shaft. An independent claim is also included for an assembly for an aircraft, comprising multiple engine mounts.