A frame assembly for an aerial system including a fuselage body and first and second rotor assemblies is described herein. The first and second rotor assemblies are coupled to the fuselage body by respective positioning assemblies. Each positioning assembly including a hinge assembly to enable the first and second rotor assemblies to pivot between a deployed position and a stowed position. A first positioning assembly including tapered positioning shaft. A second positioning assembly including a positioning sleeve having a tapered inner surface defining a cavity that is configure to receive the positioning shaft therein. The first positioning assembly being coupled to the second positioning assembly such that the first positioning assembly is rotatable about the rotor assembly rotational axis independent of the second rotor assembly.

An inflatable package enclosure for use on an aerial vehicle including an inflatable exterior chamber, a first inner cavity positioned within the inflatable exterior chamber, an inflation valve positioned on the inflatable exterior chamber, and a handle on the inflatable exterior chamber for securing the inflatable package enclosure to the aerial vehicle, wherein when the inflatable exterior chamber is inflated and when a package is positioned in the first inner cavity, inner surfaces of the inflatable exterior chamber conform to outer surfaces of the package to secure the package within the inflatable exterior chamber.

Disclosed is an apparatus (100) for an aerial transportation of a payload. The apparatus (100) includes a propeller unit (10) to provide a primary thrust whereas a plurality of propellers (50) is fitted around a body of the apparatus (100) to help in maneuvering and orientation control. The apparatus (100) employs gasoline as a primary source of energy that has a higher energy density than lithium polymer batteries. The apparatus (100) facilitates longer flight times. The apparatus (100) is useful for safe transportation of higher payloads and has vertical takeoff and land capability.

An electric unmanned aerial vehicle includes a position sensor configured to obtain first coordinate information of a present position of the electric unmanned aerial vehicle in real-time, a memory configured to store second coordinate information of a preset position of the electric unmanned aerial vehicle, and a controller in communication with the position sensor and the memory. The controller is configured to calculate, based on the first coordinate information and the second coordinate information, safety electricity amount information of the electric unmanned aerial vehicle; select, based on the safety electricity amount information and a present remaining electricity amount of the electric unmanned aerial vehicle, a safety protection command from a plurality of safety protection commands; and control the electric unmanned aerial vehicle to perform the selected safety protection command.

An aircraft includes; a plurality of rotor units each of which includes a propeller and a motor which drives the propeller, and generates thrust for flight of the aircraft; a controller which controls rotation of the propellers included in the plurality of rotor units; a balloon which laterally covers the plurality of rotor units; and a detector which detects a state of the aircraft, wherein the controller decreases a rotational speed of the propeller included in at least one rotor unit among the plurality of rotor units, according to a result of detection by the detector.

Combination fuel cell stack and electrochemical battery system provides stable and redundant electrical power to one or more traction motors. The electrochemical battery packs comprise modules that are switched between a low-voltage parallel configuration connecting to the fuel cell stack and a high-voltage series configuration connecting to the traction motors, thereby harvesting low-voltage energy from the fuel cells and deploying that energy as high-voltage power to the motor. The plurality of electrochemical battery packs can be switched such that at least one is always connected to the traction motor for continuity of power.

An apparatus in which electric power is generated for an electrical load from differentials in electric field strengths within a vicinity of powerlines includes: a plurality of electrodes separated and electrically insulated from one another for enabling differentials in voltage resulting from differentials in electric field strength experienced there at; and electrical components electrically connected therewith and configurable to establish one or more electric circuits whereby voltage differentials cause a current to flow through the established electric circuit for powering the electrical load. Preferably, the apparatus includes a control assembly having one or more voltage-detector components configured to detect relative voltages of the electrodes; and a processor enabled to configure—based on the detected voltages and based on voltage and electric current specifications for powering the electrical load—one or more of the electrical components to establish an electric circuit for powering the electrical load.

The present disclosure describes a signal relay node that is physically displaceable by a delivery system to move the signal relay node to a different location, to enable the signal relay node to overcome physical obstructions to signal propagation. A delivery system, such as a launching system, can launch the signal relay node encased within a housing unit, such as a projectile cap. Upon launch into the air, an additional aloft package may provide an aerostat, parachute, and/or a propeller and motor system to keep the signal relay node aloft in the air for a longer period of time.

An unmanned aerial vehicle (UAV) includes a central body, a plurality of arms extending out from the central body and in fluid communication with the central body, and a plurality of propulsion units. The plurality of arms are configured to route fluid away from the central body of the UAV. Each propulsion unit attached to a corresponding arm of the plurality of arms.

An aerial device includes a body, an optical system having gimbal supporting a camera, a lift mechanism coupled to the body, a haptic sensor coupled to the body and configured to generate haptic data, and a processing system disposed in the body and in data communication with the haptic sensor. The processing system is configured to process the haptic data to understand an intended position of the aerial device and/or an intended orientation of the gimbal and convert the intended position to a target position of the aerial device and/or the intended orientation to a target orientation of the gimbal utilizing said processed data irrespective of an initial position of said aerial device and an initial orientation of said gimbal. Also disclosed is a method for controlling the aerial device.