A multi-axis amphibious copter for flying and cruising at high speeds. The multi-axis amphibious copter includes six propulsion points i.e., four propellors oriented vertically, a coaxial rotor oriented vertically, and a mini turbine thruster on the rear of the aircraft body and configured to propel the multi-axis amphibious copter forward. The multi-axis amphibious copter can land and take off vertically from congested places and can fly at cruising speeds.

An unmanned aerial device having cleaning function includes a fuselage, a washing assembly and two propulsion assemblies. The washing assembly is disposed at a head of the fuselage. The propulsion assemblies are connected to two opposite sides of the fuselage. The two opposite sides are connected to the head. The propulsion assemblies each have an axial direction, and the axial direction is parallel to a direction from a bottom of the fuselage to a top of the fuselage.

A first embodiment includes a circuit based aerial vehicle including an enclosed air duct circuit with a plurality of fans within respective fan tunnels and a plurality of rotating archway assemblies. The rotating archway assemblies may include respective cylinder casings with medial archways, actuating collars at opposing ends of the cylinder casing, and a rotational cylinder rotatable along its longitudinal axis. The actuating collars may be structured to spin their respective cylinder casings along the cylinder casing longitudinal axes thereby orienting the rotational cylinders in different positions along their medial axes.

A second embodiment includes rounded cylinder assemblies with respective bulbous cylinder casings including medial actuating collars that rotate rather than the entire cylinder casing. The actuating collars themselves are structured to spin their respective rotational cylinders along the rotational cylinder longitudinal axes to orient the rotational cylinders in different positions along their medial axes.

A firefighting aerial vessel that can coordinate with other firefighting aerial vessels to extinguish fires. The vessel has a body with a bottom container providing a volume for extinguishing substances that are fluidly coupled to spray units supported by the exterior of the body. The plurality of propulsion units of each vessel may be rotatably to the body of the vessel so that the vessel can move and rotate about the x, y, and/or z-axis. The vessel can form specific formation with other vessels in a coordinated manner by way of communication and positioning systems, so that the formation can surround and thwart fires.

An aerial vehicle platform, which may be unmanned, includes an engine rotatable along multiple axes to provide various modes of flight and movement. The platform may be scaled for different purposes. The purposes may range from defense, to reconnaissance, and to civilian or commercial applications. Other applications may also benefit from the embodiments disclosed. Embodiments may include a gimbal hub to control the orientation of the engine along different axes.

Systems, methods, and apparatuses for an aerial vehicle (AV). The AV can include a frame structure comprising an upper frame, a lower frame, and bridges connecting the upper frame and the lower frame. The upper frame can include a housing for electrical components. The AV can include a duct extending from the upper frame to the lower frame. The AV can include a motor to rotate the propeller. The AV can include guides located between the bridges and the duct. A portion of the guides can include a non-linear path. The AV can include actuators. The AV can include flaps, coupled to the guides and the actuators, configured to protrude from the lower frame or retract into the frame structure. The flaps can curve along at least one of a horizontal axis or a vertical axis of the flaps. The flaps can overlap with each other when protruded.

The aircraft thrust control system comprises a central power unit and peripheral power units. The central power unit comprises upper and lower propellers arranged one above the other and adapted to rotate in opposite directions, while propellers of the peripheral power units are located outside the aerodynamic operating range of the central power unit propellers.

The aircraft thrust control system comprises a central power unit and peripheral power units. The central power unit comprises upper and lower propellers arranged one above the other and adapted to rotate in opposite directions, while propellers of the peripheral power units are located outside the aerodynamic operating range of the central power unit propellers.

This disclosure describes an aerial vehicle, such as an unmanned aerial vehicle (“UAV”), which includes a plurality of maneuverability propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll). The aerial vehicle may also include a lifting propulsion mechanism that operates to generate a force sufficient to maintain the aerial vehicle at an altitude.

This disclosure describes an aerial vehicle, such as an unmanned aerial vehicle (“UAV”), which includes a plurality of maneuverability propulsion mechanisms that enable the aerial vehicle to move in any of the six degrees of freedom (surge, sway, heave, pitch, yaw, and roll). The aerial vehicle may also include a lifting propulsion mechanism that operates to generate a force sufficient to maintain the aerial vehicle at an altitude.