FIELD: engine devices and pumps.
SUBSTANCE: pylon (31) for mounting the engine (10) on the aircraft structure comprises a first fastening means (32) which is mountable on the pylon and a second fastening means (33). The second fastening means is made to be fixed to the structure of the aircraft. The pylon also comprises a connection means (35) connecting the first fastening means (32) to the second fastening means (33). The connection means (35) is configured to allow the first fastening means to move relative to the second fastening means between the first and second positions by force that is a resultant traction force and the weight of the engine (10).
EFFECT: invention improves aerodynamics of the engine during the lifting phase of the aircraft.
7 cl, 2 dwg
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Authors
Dates
2017-11-08—Published
2013-09-12—Filed