FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to device intended for cargo mounting and transportation by aircraft. Proposed device comprises two flexible links, stabilising tie rod and locking device. Locking device represents two clamps arranged on stabilising tie rod at a certain distance one from another to fix said tie rod to each flexible link connected to aircraft electric (hydraulic) lock. Free end of stabilising tie rod can slide in the frame pivoted to cantilever arranged on aircraft. Two additional clamps are arranged on said flexible links. Ring is secured to one additional clamp to accommodate tie rod of aerodynamic stabilisation sliding relative said ring, while another additional clamp is rigidly connected with aforesaid tie rod with aerodynamic fin secured to its end. Said fin is made up of two plates arranged at the angle to each other. Said angle can be adjusted. There are hooks on the ends of two flexible links for cargo to be suspended thereon.
EFFECT: expanded performances and cargo stabilisation.
4 dwg
