FIELD: aviation. SUBSTANCE: flapping wing aeroplane has rigid casing, two flapping wings, their drive, power plant and pilot seat. Each flapping wing is rotatably secured on crank pin of crankshaft ensuring planetary rotation at halved frequency in opposite direction relative to crankshaft. EFFECT: enhanced reliability. 4 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLAPPING WING AEROPLANE | 1993 |
|
RU2063367C1 |
| ORNITHOPTER | 2010 |
|
RU2452660C2 |
| ORNITHOPTER | 2010 |
|
RU2451623C1 |
| INTERNAL COMBUSTION ENGINE | 2001 |
|
RU2200858C2 |
| DYNAMIC INERTIAL ORNITHOPTER (DIMa) | 2021 |
|
RU2779547C1 |
| FLAPPING-WING FLYING VEHICLE | 2003 |
|
RU2255026C2 |
| METHOD OF DRIVING ORNITHOPTER WINGS AND ORNITHOPTER | 2010 |
|
RU2450954C1 |
| FLAPPING VEHICLE | 1996 |
|
RU2129076C1 |
| INTERNAL COMBUSTION ENGINE | 1989 |
|
RU2008476C1 |
| AIRCRAFT | 2011 |
|
RU2480378C1 |
