FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to engine support, and aircraft incorporating said power plant. Support 4 of aircraft engine 6 comprises rigid structure 8 and appliances to mount said engine on said structure. Mounting appliances comprise device 14 to take up thrust forces that comprises two lateral tie rods 26. Rear ends 26b of every said lateral tie rod are jointed with cross member 28 of said device 14 via mechanical joint 44. Every mechanical joint 44 consists of cantilever 48 arranged on cross member 28 to pass through hole 50 in rear end 26b of appropriate 26. Note here that said cantilever 48 is arranged across said support.
EFFECT: simplified design.
11 cl, 12 dwg
