FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the design of devices for placing the payload on unmanned aerial vehicles (UAV). Suspension device (SD) consists of a housing, a base made in the form of a container, the upper surface of which has holes configured for the size of the ammunition. In the cavity between the lower and upper surfaces of the container there is a locking mechanism is installed consisting of a servo drive with a cam and a pusher, connected by means of a bracket to the lower surface of the container. Cam and pusher are installed on side surface of housing. SD contains electronic unit for connection and control of ammunition safety mechanism, connected to servo drive of locking mechanism. On the housing there are bends and protruding elements that are interfaced with the surface of the UAV, as well as providing the required arrangement of the ammunition in the suspension device.
EFFECT: convenience and safety of handling a loaded release device, increasing the efficiency of using ammunition.
1 cl, 4 dwg
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Authors
Dates
2024-07-09—Published
2023-12-18—Filed