FIELD: arrangement of jet engines on flying vehicles.
SUBSTANCE: proposed air intake has outer fairing 3, leading edge 4 and inner narrowing fairing 5 made from layers of composite material. Each layer of composite material is equidistant relative to working surfaces of leading edge 4 and fairings 3 and 5. Narrowing part 8 of inner fairing 5 is provided with circular layers 10 in zone of leading edge 9. Circular layers 10 are provided with thermo-shrinkable fibers.
EFFECT: enhanced operational reliability.
3 cl, 4 dwg
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