FIELD: aviation.
SUBSTANCE: quadrocopter comprises a body with stationary useful equipment mounted therein, four traction means with four lifting propellers, each of which is located on a frame mounted on the respective remote beam of the body. Traction means are mounted with possibility of rotation in frames to an angle of not less than 180°both mutual and independent from each other, and frames with possibility of rotation around the axis of beams to an angle of 360°both mutual and independent, in this case the propellers are installed with possibility of changing the thrust force and direction both mutual or independent from each other.
EFFECT: possibility to change the spatial orientation of quadrocopter body regardless of trajectory and mode of motion, increase of efficiency in case of horizontal flight.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
AIRCRAFT | 2016 |
|
RU2656932C2 |
GYROPLANE | 2018 |
|
RU2673933C1 |
METHOD OF LANDING UNMANNED AERODYNAMIC FLYING VEHICLE | 2005 |
|
RU2278801C1 |
AIRCRAFT OF HORIZONTAL FLIGHT WITH VERTICAL TAKE-OFF AND LANDING AND BEARING PLATFORM FOR AIRCRAFT OF HORIZONTAL FLIGHT WITH VERTICAL TAKE-OFF AND LANDING | 2018 |
|
RU2693362C1 |
TETHERED AIR HELICOPTER SIMULATOR | 2016 |
|
RU2622583C1 |
MULTICOPTER WITH COMBINED PROPELLERS AND HYBRID PROPELLER OF POWER PLANTS | 2022 |
|
RU2803214C1 |
CONVERTIPLANE | 2019 |
|
RU2723516C1 |
GROUND SITUATION OBSERVATION SYSTEM | 2004 |
|
RU2248307C1 |
VERTICAL TAKEOFF AND LANDING AIRCRAFT | 2016 |
|
RU2627220C1 |
AIRCRAFT | 2012 |
|
RU2507122C1 |
Authors
Dates
2015-04-10—Published
2013-12-19—Filed