| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: proposed system comprises gripping device with lock made up of anchor device wound on aircraft onboard winch by pickup halyard equipped with flexible element lock and aerodynamic carrier mounted on aircraft. Pickup halyard passes through guide element and coupler and has its one end connected with lock and aerodynamic carrier. Method of aircraft landing comprises guiding flight path on to flexible element stretched in vertical plane and suspended under tethered or independent aircraft. Method of aircraft takeoff comprises releasing halyard, hooking it by lock to flexible element, switching on the drive to lift, turning halyard around, lifting aircraft coupled with flexible element and halyard to launching height. ^ EFFECT: landing without runway, simplified guidance, takeoff without overloads. ^ 47 cl, 11 dwg |
