| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to flying vehicle doors. Flight vehicle 1 can hover and comprises fuselage 2 with nose 3, tail 11 opposed said nose and cabin located between nose 3 and tail 11. Cabin 8 has loading opening 20 at the end opposite that nose 3 and first flap 26 to displace between closed position whereat it closed at least one segment 28 of loading opening and open position whereat it allows unobstructed access to segment 29 of loading opening 20. First flap 26 displaces from tail 11 to nose 3 to stay in open position at opposite side of said first edge 21 of loading opening 20 relative to second edge 22 of loading opening 20 located opposite said first edge 21.EFFECT: cleared loading site between loading opening, loading at running rotor.13 cl, 5 dwg |
