| 摘要 |
This invention relates to a structure ( 1 ) for mounting a turboprop ( 2 ) under an aircraft wing ( 4 ), comprising a rigid structure and means ( 10 ) of fastening the turboprop on the rigid structure. According to the invention, the rigid structure is composed of a box ( 8 ), and the mounting means comprise at least two lateral connecting rods ( 26 ) resisting the engine torque generated by the turboprop, the connecting rods ( 26 ) being arranged on each side of the box and each having a forward end ( 26 a) connected to a gear box ( 24 ) of the turboprop ( 2 ), and an aft end ( 26 b) connected to said box.
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