FIELD: aircraft engineering.
SUBSTANCE: proposed drone comprises lengthwise airframe equipped with X-like folding airfoils with the part turning about axle arranged along the airframe at fixed root section of airfoil at a distance from the drone vertical mirror plane, drives of airfoil turning parts, assemblies for suspension under carrier aircraft arranged at airframe top part, and control system. X-like airfoil turning parts as-folded adjoin the airframe surface sidewalls. X-like airfoil turning parts adjoin the airframe surface bottom wall, airframe being provided with lengthwise ledges arranged opposite end edges of top airfoils.
EFFECT: lower probability of end tip damage in operation.
2 cl, 2 dwg
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