FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed device comprises stiff structure and attachment to secure engine on said stiff structure wherein said attachment comprises engine rear attachment 8 and thrust take-up device 9. Note here that said rear attachment 8 is secured to stiff structure by two transverse connection elements. Device 9 comprises two connections bars 26a, 26b jointed to cross-arm 28 by mechanical fastener, connection element 49 secured to rear attachment 8 and fastened with stiff structure by pin 60. Transverse connection elements of device 9 comprises means to limit turn of cross-arm 28 in failure of bars 26a, 26b and to transfer traction forces to stiff structure 10.
EFFECT: simplified design.
10 cl, 9 dwg
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