FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely to aircraft device comprising wing and suspension pylon. Aircraft device 1 comprises wing 2 and pylon 4 to suspend engine 10 above said wing. Besides device includes appliances 8 to attach pylon rigid structure 6 to wing 2. Note here that said appliances 8 comprise two front fasteners (29a, 29b), each being furnished with shackle (38) to take up vertical load acting along axis (Z) of engine suspension pylon. Said shackle (38) is pivoted by first pin (56) to first fastener (50) attached to front spar (34) that makes a part of wing (2) and arranged along direction (32) of said wing (2), and is articulated by second pin (46) with second fastener (42) secured to rigid structure (6). Shackles (38) of two front fasteners are located in one plane (P), which is parallel to pylon vertical direction.
EFFECT: reduced sizes of engine suspension.
15 cl, 10 dwg
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