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
| Title | Year | Author | Number |
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