TURBOJET NACELLE AIR INTAKE Russian patent published in 2013 - IPC B64D29/06 

FIELD: transport.

SUBSTANCE: invention relates to aircraft engineering, namely, to turbojet aircraft nacelle 4. Air intake comprises outer panel 40, inner panel 41 and air intake edge 4a furnished with inner wall 70 to get in contact with airflow flowing into turbojet, and baffle 45 to separate said edge 4a from the other part of nacelle 1. Air intake edge 4a incorporates extra segment to be attached to inner panel 41 to extend, in fact, along inner wall 79 to air intake downstream section through length I approximating to maximum distance a between baffle 45 and air intake edge.

EFFECT: improved aerodynamics of aircraft.

9 cl, 6 dwg