FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to aircraft air intake. Air intake 113 is to be engaged with aircraft fuselage 141 by means of pylon 134. Note here that local length of this air intake measured parallel with engine axis A between air intake leading edge 138 and transverse plane P located level with engine compressor inlet wheel is larger (Lmax) in air intake zone 142 jointed with pylon and smaller (Lmin) in air intake zone opposite the pylon.
EFFECT: simplified design.
11 cl, 6 dwg
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