FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, namely, to in-flight refuelling cone assembly. Proposed assembly comprises intake component provided with intake axial hole, mating docking device and drogue parachute. Said drogue parachute is arranged around said component and comprises set of levers arranged along circumference to carry first canopy and second canopy arranged around said first canopy. Second canopy may be reconfigured by air pressure to allow second canopy to be folded inside first canopy to reduce effective surface of second canopy.
EFFECT: possibility for use in wide ranges of flight speeds.
9 cl, 6 dwg
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