FIELD: aviation. SUBSTANCE: flying vehicle cabin has sides, fuselage floor and module mounted on floor. This module is articulated in its upper portion to fuselage sides by means of special units. This unit is made in form of parallel link mechanism by means of two double-arm levers, ropes and rods. Levers are mounted in upper portion of module on fuselage sides. Ropes are used for connecting the double- arm levers in parallel link mechanism. At one end, rods are connected to double-arm levers over parallelogram diagonal; other ends of rods are connected to fuselage sides. EFFECT: increased mass of payload; reduced mass of flying vehicle at retained strength characteristics. 3 dwg
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