FIELD: parachute systems.
SUBSTANCE: invention relates to controlled gliding parachute systems. Suspended undocked aircraft container has a body with internal lockable compartments for storing cargo and equipment, aircraft suspension assemblies and a parachute system. The contours of the outer surfaces of the aircraft container are made using geometry elements of the surfaces of the airframe unidirectional with them. The parachute and the pivotally folding rack located under it with the power plant located on it are placed in the compartment of the aircraft container, which is closed by hingedly folding consoles of the vertical tail. The hull has a cargo compartment, from which the instrument compartment is separated by a bulkhead, in which the pilot chute, main parachute, control system, radio beacon and batteries are located. On the upper edge of the side walls of the cargo compartment, the lower parts of the power lines of the parachute are fixed and laid, the upper part and steering lines of which are in the instrument compartment, protected from external influences by the consoles of the folding vertical tail. Under the main parachute there is a hinged strut with a power plant located on it.
EFFECT: invention is aimed at expanding the scope of functional use.
6 cl, 6 dwg
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Authors
Dates
2021-11-01—Published
2021-03-26—Filed