| 摘要 |
This invention relates to a structure ( 1 ) for mounting an engine ( 2 ) under an aircraft wing ( 4 ), comprising a rigid structure ( 8 ) and means ( 10 ) of mounting this rigid structure under the wing, the mounting means ( 10 ) comprising a forward fastener ( 14 ) 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, placed in a vertical plane oriented along a direction inclined with respect to a longitudinal direction (X) and a transverse direction (Y) of the aircraft, and located in a horizontal plane defined by these directions (X) and (Y). Furthermore, the aft fastener comprises at least one shackle oriented along a vertical direction (Z) of the aircraft.
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