FIELD: aircraft engineering.
SUBSTANCE: electric hybrid two aircraft comprises bearing fuselage low and high sweepforward and sweepback wings. Ends of said wings are connected by end plate. Front horizontal tail unit comprises keels, and all-moving keels stabilizer. Four electrically driven blowers in circular channels and tandem nacelles of large propellers, front pull and rear push propellers, run in opposite directions to work at different angles of deflection in vertical plane. Large sweepforward wing is arranged under rear sweepback small wing.
EFFECT: decreased stall, lower aerodynamic and inductive resistance.
1 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| HYBRID SHORT TAKEOFF AND LANDING ELECTRIC AIRCRAFT | 2014 |
|
RU2554043C1 |
| HYBRID SHORT TAKEOFF AND LANDING AIRCRAFT | 2015 |
|
RU2577931C1 |
| VTOL AIRCRAFT WITH HYBRID POWER PLANT | 2013 |
|
RU2542805C1 |
| MULTIROTOR CONVERTIBLE HIGH-SPEED HELICOPTER | 2014 |
|
RU2548304C1 |
| CRYOGENIC TURBO-ELECTRIC STOL AIRCRAFT | 2013 |
|
RU2534676C1 |
| MULTIROTOR CONVERTIBLE PILOTLESS HELICOPTER | 2014 |
|
RU2550909C1 |
| CRYOGENIC ELECTRICAL CONVERTIPLANE | 2013 |
|
RU2529568C1 |
| MULTIROTOR CONVERTIBLE HIGH-SPEED HELICOPTER (MCSH) | 2014 |
|
RU2568517C1 |
| AIR-TRANSFORMER, CONVERTED INTO THE CAR | 2016 |
|
RU2650257C1 |
| HEAVY CONVERTIBLE ELECTRIC DRONE | 2013 |
|
RU2532672C1 |
