FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely to engine attachment to be mounted between aircraft wing and its engine. Attachment 4 of engine 6 to be mounted between aircraft wing 2 and said engine 6, comprises rigid structure 8 and front aerodynamic structure 24 rigidly fixed thereon. Said aerodynamic structure 24 can support engine blower housings and be arranged between rigid structure and wing. Said attachment comprises at least one jointing adjustable-length link 32. Note here that one end of said link is jointed with rigid structure 8 while opposite end is jointed with front aerodynamic structure 24.
EFFECT: simplified design and more precise positioning of front aerodynamic structure.
9 cl, 3 dwg
