| 摘要 |
This invention relates to a mounting structure ( 1 ) for mounting an engine ( 2 ) under an aircraft wing ( 4 ), the structure comprising a rigid structure ( 8 ) and means ( 10 ) of fastening this rigid structure under the wing, the mounting means comprising a forward fastener ( 14 ), an intermediate fastener ( 15 ) and an aft fastener ( 16 ). According to the invention, the forward fastener has at least one triangular shackle on each side of a vertical plane passing through a longitudinal axis ( 5 ) of the engine ( 2 ), placed in a vertical plane oriented along a longitudinal direction (X) of the aircraft. Furthermore, the intermediate fastener comprises a connecting rod capable of transferring forces applied in a direction (Y) transverse to the aircraft, and the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.
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