| 摘要 |
The invention relates to an engine suspension pylon for an aircraft including a rigid structure provided with a box ( 24 ), this pylon also including an engine aft attachment ( 8 ) provided with an attachment body ( 38 ), and a thrust resistance device ( 9 ) generated by the engine. The rigid structure according to the invention includes an offset rib ( 35 ) for the attachment body ( 38 ), this rib ( 35 ) being mounted fixed on the box ( 24 ) between the box and the engine ( 2 ) and carrying the attachment body. Furthermore, the device ( 9 ) includes a thrust resistance spar ( 9 b) of which the forward end is mounted fixed on the rib ( 35 ), and the aft end is mounted fixed on the box.
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