FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft power plant attachment. Aircraft power plant 110 comprises two-stage jet engine arranged in nacelle confining secondary flow passage and engine suspension 132 including pylon 134, in fact, parallel with engine axis 135, and means to attach engine to pylon. Said pylon is arranged at an angle to vertical plane 150 extending through engine lengthwise axis and nacelle top and located outside said secondary flow. Attachments of engine to pylon comprises two crosswise horizontal and parallel beams to engage said pylon with joint atop engine housing parts.
EFFECT: simplified design of engine suspension, improved aerodynamics.
12 cl, 8 dwg
