FIELD: aviation.
SUBSTANCE: invention relates to devices for suspension of engines to aircraft wing. Device for engine suspension to aircraft wing includes power beam (1) of pylon, comprising front assembly (3) of engine suspension (50), rear assembly (5) of engine suspension (50) and central assembly (4) of engine suspension (50), assembly (47) of engine suspension (50) on pylon and front assembly (48) of engine suspension (50) on pylon, arranged on lower surface in front part of power beam (1). Pylon power beam (1) is connected to the wing using four suspension links formed by: suspension shackles on brackets located symmetrically relative to the pylon axis, shackles on the bracket and central suspension unit (4) consisting of bracket of outer and inner kingpin connected to spherical bearing installed in power beam (1) of pylon.
EFFECT: higher strength and reliability of design.
3 cl, 9 dwg
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