FIELD: aviation.
SUBSTANCE: proposed aircraft has fuselage, two hulls, power plant, mid-mounted wing of low aspect ratio provided with control surfaces and main wing on pylons which is used for connecting the fuselage and hulls in such way that connecting members work in compression; aircraft is also provided with horizontal tail mounted in its nose section, quick-detachable coupling units and parachute systems. Hulls and fuselage are provided with pylons. Main wing is provided with triple-slotted flaps and systems of two-mode control jets at tips of its outer panels; it is articulated on pylons. Horizontal tail is mounted in nose section between fuselage and hulls. Main wing and mid-mounted wing are of low aspect ratio and are spaced apart relative to each other along aircraft axis in such way that aircraft center of mass is located between centers of pressure of main wing and mid-mounted wing.
EFFECT: reduction of mass; improved aerodynamic efficiency; enhanced seaworthiness and afloat maneuverability.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT | 2008 |
|
RU2408501C2 |
| AMPHIBIOUS AIRCRAFT OF "FLYING WING" SCHEME | 2017 |
|
RU2668000C1 |
| FLOAT-TYPE SEAPLANE OF CATAMARAN CONFIGURATION-SEA-GOING SALVAGE VESSEL | 2004 |
|
RU2270137C2 |
| VTOL HYDROPLANE AND ENGINE THRUST VECTOR DEFLECTOR | 2013 |
|
RU2549588C2 |
| HEAVY TRANSPORT FLOAT-TYPE SEA PLANE-AMPHIBIAN OF CATAMARAN CONFIGURATION | 2004 |
|
RU2314231C2 |
| AMPHIBIOUS AIRCRAFT | 2011 |
|
RU2471677C1 |
| VERTICAL TAKEOFF AND LANDING SEAPLANE AND PNEUMATIC TAKEOFF AND LANDING APPARATUS | 2020 |
|
RU2755561C1 |
| AMPHIBIOUS WITH INCREASED CARRYING CAPACITY | 2020 |
|
RU2739451C1 |
| MULTI-MODE GROUND-EFFECT VEHICLE - AIRPLANE | 2019 |
|
RU2719993C1 |
| MULTIFUNCTIONAL SMALL-SCALE TRANSFORMABLE REUSABLE UNMANNED AERIAL VEHICLE IN TRANSPORT-LAUNCH CONTAINER AND STARTING METHODS | 2022 |
|
RU2778177C1 |
