| 摘要 |
FIELD: aircraft engineering. ^ SUBSTANCE: invention relates to VTOL flight vehicles heavier than air. Flying wing of vertical take-off and landing incorporates adaptive wind and power plant comprising engines and centrifugal compressors that allow changing thrust vector and boundary layer control. Round- or oval-shape wing features surface coordinates located on 2nd-order lines. Plane wherein every line lies is perpendicular to that of the wing lengthwise profile shape. Power plant comprises air jet engine integrated, via pto-device and air duct, with pneumatic drive of centrifugal compressor. The latter is furnished with motor-generator or super flywheel and nozzle with flaps to change thrust vector from vertical to horizontal one. FWVTL upper part split wing features slits to make air intakes of centrifugal compressors and to control boundary layer. ^ EFFECT: expanded performaces. ^ 10 dwg |
