FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft (AC) with engines, and concerns protection of risk of impact action by part, separated from opposite engine in case of failure. AC comprises engine plant composed of two engines, installed on each its side. Fuselage rear part has vertical plane of symmetry and it is made of composite material. Wherein inner screen is installed in rear part of AC and it is located in vertical plane of symmetry. Inner screen extends in area covering possible paths of plurality of predefined fragments separated from one of engines in case of failure, which would have effect on critical elements of opposite engine. Wherein inner screen has flat shape and energy absorption capacity.
EFFECT: higher safety and strength are achieved.
16 cl, 8 dwg
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