Patent ID: 9527599
Filing Date: 2016-12-27
CPC Classification: B64D

Claim Text:
1. An aircraft engine fastener, intended to fix an engine to a nacelle stub for suspension of this engine, the engine fastener comprising an elongate fastener body formed of two joined fittings, the fastener body being provided at a first end with a fixing assembly, the engine fastener comprising two connecting rods connected by a crossbar to the fastener body at a second end thereof opposite the first end, the fixing assembly comprising a connection element provided with a shaft and configured to hold two tubular pins arranged one in each of the two fitting parts of the two fittings, the two fitting parts being joined at a junction zone, and the two tubular pins surrounding the shaft by being arranged one at each of the two axial ends of the shaft, the fixing assembly comprising a tubular shear pin surrounding the shaft of the connection element with a clearance, the shear pin being arranged between the two pins and being in contact with the two fitting parts on either side of the junction zone, the shaft of the connection element also being mounted with clearances relative to the two pins and to the two fitting parts.