FIELD: aviation.
SUBSTANCE: node (10) for anchoring a sensor container (12) for anchoring a sensor container (12) to the fuselage (AF) of an aircraft (AC) comprises the front and rear pairs of the anchoring pylon nodes (14, 16). The front pair of the anchoring pylon nodes (14) includes pylon structures of the port side and starboard, and a transverse support base connected to the upper ends of the pylon structures of the port side and the starboard. The rear pair of the anchoring pylons (16) includes a spar node configured to be adjustable in the longitudinal direction.
EFFECT: invention improves aerodynamic characteristics, reduces weight and increases the strength of the aircraft.
20 cl, 9 dwg
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