Remotely operated aerial vehicle with reduced cross-section area during forward flight
The present invention extends to methods, systems, devices, and apparatus for remotely operated aerial vehicle with reduced cross-section area during forward flight. In one aspect, a remotely operated aerial vehicle is a rotor based Unmanned Aerial Vehicle (UAV) having a plurality of rotors. A remotely operated aerial vehicle includes a frame, a power source, a plurality of motors, and a corresponding plurality of fixed rotors. The frame includes a top surface. Each fixed rotor in the plurality of fixed rotors is mounted to a corresponding motor from among the plurality of motors. The corresponding motor controls the rotation of the fixed rotor. Each of the plurality of fixed rotors is mounted at a specified angle relative to the top surface. Mounting the fixed rotors at the specified angle minimizes the cross-sectional area of the frame when the remotely operated aerial vehicle flies in a specified direction.
1. A remotely operated aerial vehicle comprising:
a frame including a top surface;
a power source contained within the frame;
a plurality of motors mounted to the frame, the motors powered by the power source; and
a plurality of fixed rotors, each fixed rotor included in the plurality of fixed rotors mounted to a corresponding motor from among the plurality of motors, the corresponding motor controlling the rotation of the fixed rotor, each of the plurality of fixed rotors mounted at a specified angle relative to the top surface; and
wherein, based on the specified angle, the remotely operated aerial vehicle has a first cross-sectional area when hovering and the remotely operated area vehicle has a second cross-sectional area when moving in a specified direction, the second cross-sectional area being smaller than the first cross-sectional area.
2. The remotely operated aerial vehicle of claim 1 , wherein the remotely operated aerial vehicle is a quad-rotor Unmanned Aerial Vehicle (UAV).
3. The remotely operated aerial vehicle of claim 1 , wherein the plurality of fixed rotors comprises six rotors.
4. The remotely operated aerial vehicle of claim 1 , wherein the plurality of fixed rotors comprises a plurality of open rotors.
5. The remotely operated aerial vehicle of claim 1 , wherein the frame includes a plurality rotor housings; and
wherein the plurality of fixed rotors are enclosed within the plurality of rotor housings.
6. The remotely operated aerial vehicle of claim 1 , wherein the power source includes one or more of: a battery or an engine that consumes liquid fuel.