FIELD: aviation.
SUBSTANCE: aircraft cargo compartment is a niche formed in the fuselage strakes joint area with wing panel (3). In the cargo compartment niche, an inferential trigger (4) of load (5) is fixed. At the bottom, the cargo compartment niche is provided with a recess fairing (6) comprising at least one flap (7). Inferential starting device (4) is a lever mechanism for load (5) cleaning and release in a plane lying at an acute angle α ranging from 20 to 70 degrees to the aircraft plane of symmetry, so that in the released position, the head part of load (5) is located in front of front edge (10), wing panel (3) to reduce the load "shadowing" area from forward fuselage (11 ) and front edge (12) of fuselage strake and the longitudinal axis of load (5) is removed from the entrance to air intake (13), forming the so-called stagger.
EFFECT: invention reduces aerodynamic drag and radar signature.
4 dwg
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Authors
Dates
2017-03-30—Published
2015-06-24—Filed