FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to turbojet nacelles. Claimed nacelle internal structure comprises active and passive moving elements. Active elements drive the adjacent passive elements. Internal structure has three positions. At the first nominal position, an aerodynamic continuity exists between active moving elements and passive moving elements. At second position, the active moving elements extend beyond the passive moving elements outward from the internal structure. At third position, the active moving elements extend beyond the passive moving elements inside the internal structure.
EFFECT: simplified design.
13 cl, 22 dwg
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