FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. In compliance with version, proposed suspension is furnished with balance weight fitted through guide secured sling fasteners to slide thereon. Control slings are secured to balance weight. In compliance with second version, suspension is furnished with suspension hook hinges and sling hinges. Tackle mechanism is arranged on suspension free end and coupled with rear free end to elongate central free end on pulling rear free end in tackle mechanism. In compliance with three versions, suspension comprises dog lead, linkage to transfer force from dog lead to suspension hooks, and accelerator tackle mechanism. Said linkage features rigidity and shape approximating to circle arc with centre located behind and atop payload centre of gravity. Guide with dog lead fastener is coupled with rigid linkage. Accelerator tackle sling ends are clamped at dog lead.
EFFECT: reduced forces of wing control.
3 cl, 6 dwg
