FIELD: aviation; designs of hydroplanes.
SUBSTANCE: amphibian aircraft contains a fuselage, floats, a wing with wingtips, a tail unit, a propulsion unit, a power unit, a landing gear, main hydrofoils, a rear water support, and a water rudder. The floats are connected to the fuselage, wing and tail in form of a profiled ring with the help of overlaps, cuffs, as well as longitudinal strakes along the bottom. The screw-type propeller is built into the profiled ring, and the profiled ring contains a high-positioned elevator with lateral profiled surfaces, as well as side rudders.
EFFECT: improved aerodynamic quality and efficiency, the possibility of short takeoff and landing, increased stability and controllability of amphibian aircraft.
17 cl, 8 dwg
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|---|---|---|---|
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|
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|
RU2668000C1 |
| LIGHTWEIGHT AMPHIBIAN AIRCRAFT | 2006 |
|
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|
RU2111150C1 |
| AIRCRAFT CONFIGURATION HAVING SPIN RESISTANCE | 2013 |
|
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| ELECTRIC AMPHIBIAN AIRFOIL BOAT | 2019 |
|
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| LONG DISTANCE SEARCH-AND-RESCUE FLOAT AMPHIBIAN SEA-PLANE OF TRIMARAN DESIGN "FREGAT" | 2006 |
|
RU2324627C2 |
| HOVERCRAFT AND ITS ALIGHTING GEAR | 2005 |
|
RU2337022C2 |
