FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft nacelle air intake assembly. Aircraft nacelle air intake jacket 19 to be mounted at turbojet blower casing 15. Said jacket 19 features sizes that allow a peripheral clearance (J, J', J") between said jacket 19 and casing 15. Note here that means 27, 33 of point connection of said jacket 19 to said casing 15 are distributed over periphery of the former and separately from each other.
EFFECT: lower probability of deformation or breakage of air intake.
19 cl, 8 dwg
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