Assembly of engine and aircraft pylon

• Main Authors: MI, BRASS WILLIAM, BERJOT MICHAEL, LANCIO, R
• Format: Patent
• Language: Chinese; English
• Published: 29.03.2022
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The invention relates to an assembly of an engine and an aircraft pylon, comprising a force reaction assembly having a connection device secured to the pylon and two rods, the connection device comprising: a boot; a dilator having a central portion connected to the boot by a main connection, the main connection comprising a main rotation pin and a main axis of rotation, which are contained in a plane of symmetry of the connection means; two fittings, each fitting having two arms, the dilator being positioned between the two arms; a first rod and a second rod respectively comprising a front end fastened to the engine and a rear end respectively fastened to a first end and a second end of the dilator and fastened to the first and second fittings by a secondary connection, the dilator comprising two extensions, one at each end, each extension is associated with a pair of resilient stops sandwiching the extension, respectively for the first and second ends of the dilator, each stop being positioned between the ar