FIELD: aviation.
SUBSTANCE: invention relates to aircraft and rocket engineering, mainly to devices for mounting an unmanned aerial vehicle (UAV) with a launching device. UAV attachment assembly includes a separate yoke of two symmetrical yokes, which are fixed on rotation axes arranged in parallel in the cavity of the bearing structure power element. Axes of rotation of symmetrical yokes are equipped with torsion springs connected by synchronizer. Cover made of two interconnected equal parts is fixed to the outer surface of each of the symmetrical yokes. End surfaces of the cover on the side of hinged joints of the cover attachment are equipped with support surfaces. Attachment unit is equipped with a collet fixture of the symmetrical yoke docking position connected by a flexible link to the launching device. On the side surface of each of the symmetrical yoke bodies there is a seat for a collet fixture. Invention can be used in the field of aviation and rocket engineering, mainly to devices for communication of UAVs with a launching device.
EFFECT: invention provides improved aerodynamic characteristics and reduced effective dispersion area of UAV.
1 cl, 6 dwg
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Authors
Dates
2024-10-16—Published
2024-04-08—Filed