FIELD: transportation.
SUBSTANCE: invention relates to aviation, in particular to aircraft engine assemblies. The aircraft engine assembly contains the first and the second rings and the first and the second connecting flanges. The first connecting flange contains the section forming the flat surface passing in radial direction with reference to the first ring. The connection zone between the first ring and the first connecting flange is displaced from the named flat surface to the distance providing damping of the shift-inducing bending moment created by the flows of forces passing through the named first ring.
EFFECT: increase of mechanical strength of internal wall of the air inlet is achieved.
8 cl, 5 dwg
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Authors
Dates
2015-12-10—Published
2011-05-09—Filed