AIRCRAFT POWER PLANT COMPRISING ENGINE SUSPENSION ASSEMBLIES SHIFTED DOWNWARD AT BLOWER HOUSING Russian patent published in 2013 - IPC B64D27/26 

FIELD: aircraft engineering.

SUBSTANCE: power plant comprises means to secure turbojet 2 at attachment prop stiff structure 10. Said means of attachment comprises 1^st, 2^nd and 3^rd engine suspension front assemblies 6a, 6b, 8 to take up traction forces arranged at blower housing 12 so that said 3^rd assembly extends in turbojet first center plane P1. Suspension 1^st and 2^nd are arranged on both sides of said center plane P1. Suspension assemblies 6a, 6b are mounted at blower housing 12 at points 6'a, 6'b outside of turbojet second center plane P2 perpendicular to first plane P1 with respect to suspension 3^rd assembly.

EFFECT: ruled our deformation of blower housing.

9 cl, 16 dwg