Patent ID: 9169892
Filing Date: 2015-10-27
Classification: B64D,F16F

Abstract:
1. An aircraft comprising at least one mechanical connection device including a body that extends along a longitudinal axis, the body comprising: two opposite end portions disposed along the longitudinal axis and adapted to receive external axial loads in compression and in tension; at least one spring member adapted to be compressed axially; a mechanism which, in the event of external axial loads in compression or in tension on the end portions, is configured to transmit to said at least one spring member compression forces oriented in opposite directions according to whether the external axial loads are in a compression condition or in a tension condition; two mobile parts aligned axially with each other and between which is axially arranged said at least one spring member, a first end portion of the body which is axially mobile when acted on by external axial loads in compression and in tension and including a central piston axially mobile inside the body and a peripheral contact area around the piston, the first end portion transmitting: