An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

A flying machine includes a flying machine body including a rotor blade; a frame including a frame body supporting the flying machine body, and a pressing section that is pressed against a target object at least at two locations separated along a direction orthogonal to a width direction of the frame body; and a detector fixed to the frame, and having a detection direction that is a direction orthogonal to a direction joining the two locations together and facing toward the target object.

An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

The present invention provides a drone-passing multiple detection sensor gate comprising: a gate having a ring-like structure through which a drone can pass during flight; a first sensor, disposed on the front or the inner front of the gate, for detecting whether the drone approaches the gate or passes through the front side of the gate; a second sensor, disposed on the inner rear of the gate, for detecting whether the drone sensed by the first sensor passes through the rear side of the gate; a detection signal transmitter, disposed inside or on a surface of the gate, for receiving, from the first sensor and the second sensor, the detection signal indicating whether the drone approaches or passes through the gate, and wirelessly transmitting the detection signal. In addition, the present invention provides a drone game system using a multiple detection sensor gate.

A flying machine frame structural body including: a frame that surrounds a flying machine body including a rotating blade, and to which the flying machine body is fixed; and plural wheels that are rotatably supported by the frame.

A self-stabilizing spherical unmanned aerial vehicle (UAV) camera assembly, including: a stabilizer assembly; a plurality of motors coupled to the stabilizer assembly; a spherical camera mounting cage assembly disposed about and coupled to the stabilizer assembly; and a plurality of cameras coupled to the spherical camera mounting cage assembly. Preferably, the plurality of cameras include a plurality of stereoscopic cameras coupled to an exterior of the spherical camera mounting cage assembly. The self-stabilizing spherical UAV camera assembly is capable of taking/recording 360 degree180 degree stereoscopic photo/video content. The self-stabilizing spherical UAV camera assembly can also be used with various real-time visualization and control technologies.

An aeronautical vehicle that rights itself from an inverted state to an upright state has a self-righting frame assembly has a protrusion extending upwardly from a central vertical axis. The protrusion provides an initial instability to begin a self-righting process when the aeronautical vehicle is inverted on a surface. A propulsion system, such as rotor driven by a motor can be mounted in a central void of the self-righting frame assembly and oriented to provide a lifting force. A power supply is mounted in the central void of the self-righting frame assembly and operationally connected to the at least one rotor for rotatably powering the rotor. An electronics assembly is also mounted in the central void of the self-righting frame for receiving remote control commands and is communicatively interconnected to the power supply for remotely controlling the aeronautical vehicle to take off, to fly, and to land on a surface.

An Unmanned Aerial Vehicle includes a body, a boom, a rotor, and a nozzle. The rotor is connected to the body and rotates about an axis of rotation. The axis of rotation of the rotor is disposed at a fixed locations relative to the body. The boom is connected to the body. The nozzle is disposed at a distal end of the boom and is configured to controllably apply a liquid to a surface disposed proximate to the nozzle. The rotor, boom, and nozzle are arranged such that the nozzle is disposed further away from the body than the axis of rotation of the rotor.

A robot includes a housing including a first shell and a second shell and having a first configuration and a second configuration, a rack disposed in an inner cavity of the housing, a telescopic assembly disposed on the rack and connected between the first shell and the second shell, and a rotary wing assembly disposed on the rack and having a folded configuration and a flight configuration. The rotary wing assembly includes: a folding arm with one end rotatably connected to the rack, a rotary wing, and a tilting arm connected between the rotary wing and the folding arm, the tilting arm and the rotary wing are extended to an outside of the housing to be adapted to drive the robot to fly in the flight configuration, and the tilting arm is rotatable relative to the folding arm to adjust a rotation direction of the rotary wing.

A self-stabilizing spherical unmanned aerial vehicle (UAV) camera assembly, including: a stabilizer assembly; a plurality of motors coupled to the stabilizer assembly; a spherical camera mounting cage assembly disposed about and coupled to the stabilizer assembly; and a plurality of cameras coupled to the spherical camera mounting cage assembly. Preferably, the plurality of cameras include a plurality of stereoscopic cameras coupled to an exterior of the spherical camera mounting cage assembly. The self-stabilizing spherical UAV camera assembly is capable of taking/recording 360 degree?180 degree stereoscopic photo/video content. The self-stabilizing spherical UAV camera assembly can also be used with various real-time visualization and control technologies.