| 摘要 |
FIELD: aviation. ^ SUBSTANCE: proposed amphibious aircraft has airframe including submersible hull and thick wing, power plant, device for fixation of flow shedding off trailing edge, gas-dynamic system for control of boundary layer and alighting gear. Proposed amphibious aircraft is provided with nozzles-elevons with yawing gas vane mounted inside them. Power plant includes lift-thrust engine with reactive thrust nozzles. Alighting gear includes wheel-ski landing gear of bicycle type. Mounted on submersible hull are center-wing section and engine. Mounted in tail section of wing are aero-gas vanes with slotted up section in front of engine nozzles. Landing gear is mounted under hull. Lock-catch for mooring rope is fitted on tail section of hull. ^ EFFECT: reduced takeoff and landing runs. ^ 12 cl, 8 dwg |
