FIELD: aircraft engineering.
SUBSTANCE: proposed device comprises front and rear attachments composed of hydraulic cylinders secured at aircraft, their head ends being communicated with gas generators intended for compressed air feed. Outer ends of the rods are furnished with threaded joints for connection of brackets. Note here that said cargo has contact surfaces to thrust against aircraft structure on tightening thread joints. One of connection brackets allows compensation for temperature change in cargo length. Front and rear assemblies provide for equal force pulse at rear assy rod stroke. Front assy rod length is larger than that of rear assy rod. Recesses to house cargo in aircraft fuselage are equipped with closable flaps or covers. Gas cylinders of front and rear assemblies have exhaust openings in piston outlets.
EFFECT: higher safety of cargo separation.
4 cl, 4 dwg
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