FIELD: heavier-than-air flying vehicles.
SUBSTANCE: proposed flying vehicle has landing gear with wheel drive and crank mechanism for performing flapping motion of wing. Landing gear is taken from ground transport facility which is equipped with bracket turnable in horizontal direction and having varying extent of cantilever; it is also provided with L-shaped lever whose one end is articulated on end of bracket cantilever; it carries wing. Crank mechanism set in rotation by drive of transport facility is connected with lever and wing by means of rope or rigid coupling. Maneuvering in flight is performed by turning the bracket and changing the extent of cantilever by means of steering gear of transport facility and additional unit for changing the extent of bracket cantilever.
EFFECT: enhanced reliability.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ELASTICALLY FLEXING ORNITHOPTER WING AND ORNITHOPTER | 2015 |
|
RU2615030C2 |
| AIRCRAFT | 2011 |
|
RU2480378C1 |
| ORNITHOPTER | 2010 |
|
RU2451623C1 |
| 0 |
|
SU131618A1 | |
| METHOD OF DRIVING ORNITHOPTER WINGS AND ORNITHOPTER | 2010 |
|
RU2450954C1 |
| ORNITHOPTER | 2017 |
|
RU2655582C1 |
| FLYING VEHICLE WITH ENGINE IN FORM OF FLAPPING WINGS | 2002 |
|
RU2217355C1 |
| BIOAERODYNAMIC AIRCRAFT WITH OSCILLATING WINGS | 2009 |
|
RU2392189C1 |
| METHOD TO CONTROL MOVEMENT OF VEHICLE CONVERTIBLE INTO AIRCRAFT AND DESIGN OF SUCH VEHICLE | 1999 |
|
RU2169085C1 |
| ORNITHOPTER | 2012 |
|
RU2488525C1 |
