FIELD: flying vehicles.
SUBSTANCE: proposed aero electrically lifting flying vehicle has fuselage, electric motors whose shafts are connected with propellers and with electric power source located on ground or on transport facility by means of electric cables. Secured on fuselage above flying vehicle CG is line connected with length regulator found on ground or on transport facility. Flying vehicle is provided with at least one wing stabilizer mounted on fuselage. Said line is secured on fuselage through swivel truss mounted on fuselage by means of articulated joint.
EFFECT: reduced dimensions and mass of flying vehicle at low power requirements.
3 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
ELECTRICALLY DRIVEN FLYING VEHICLE | 2008 |
|
RU2371355C1 |
AERIAL ELECTROLIFTING AIRCRAFT | 2018 |
|
RU2696051C1 |
HIGH-RISE BUILDING FIRE EXTINGUISHING DEVICE (EMBODIMENTS) | 2023 |
|
RU2802658C1 |
HYDRODYNAMIC STARTER-GENERATOR DRIVE | 2014 |
|
RU2571895C1 |
PROPELLER BLADE | 2018 |
|
RU2705373C1 |
VERTICAL TAKE-OFF AND LANDING SEAPLANE WITH A MAIN ROTOR WITH FOLDING RETRACTABLE BLADES | 2021 |
|
RU2781817C1 |
AMPHIBIA | 1999 |
|
RU2174080C2 |
VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
HYDRODYNAMIC DRIVE-GENERATOR | 2018 |
|
RU2690120C1 |
AEROSTATIC LIFTER | 2007 |
|
RU2374168C2 |
Authors
Dates
2006-06-20—Published
2005-07-08—Filed