B64U20/60

AUXILIARY SYSTEM FOR TAKE-OFF, LANDING, AND CARRYING OF MULTI-ROTOR UNMANNED AIRCRAFT ON MOBILE PLATFORM
20200247558 · 2020-08-06 ·

Some embodiments provide an auxiliary system for take-off, landing, and carrying of a multi-rotor unmanned aircraft on a mobile platform. One system includes a base and a sleeve rod. The base is fixed on the mobile platform. The sleeve rod is inserted into an opening of the base and fixed on the mobile platform. An airframe is provided with a circular hole at a center portion, through which the sleeve rod is configured to pass. The cone sleeve on the lower side has a circular opening at a top portion fixedly connected to the circular hole. The cone sleeve on the upper side has a circular opening at a top portion. A sleeve is provided downward along the circular opening.

DRONE APPARATUS USED IN HEALTHCARE APPLICATIONS
20200242984 · 2020-07-30 · ·

A rechargeable drone apparatus or arrangement is provided. The rechargeable drone device includes a series of sensors configured to receive information about a user and transmit the information to a computing system configured to assess the information collected from the drone device and a set of securable compartments configured to maintain samples or medications, wherein the series of securable compartments are configured to be openable by an approved individual.

POWER GENERATING WINDBAGS AND WATERBAGS
20200232443 · 2020-07-23 ·

A method of using a bagged power generation system comprising windbags and waterbags integrated with drones and adapting drone technologies for harnessing wind and water power to produce electricity. An extremely scalable and environmentally friendly method, system, apparatus, equipment, techniques and ecosystem configured to produce renewable green energy with high productivity and efficiency.

UAV having hermetically sealed modularized compartments and fluid drain ports

In one possible embodiment, an amphibious unmanned aerial vehicle is provided, which includes a fuselage comprised of a buoyant material. Separators within the fuselage form separate compartments within the fuselage. Mounts associated with the compartments for securing waterproof aircraft components within the fuselage. The compartments each have drainage openings in the fuselage extending from the interior of the fuselage to the exterior of the fuselage.

VERSATILE FLEXIBLE AND RECONFIGURABLE VEHICLE SYSTEMS
20200130795 · 2020-04-30 ·

Various embodiments are directed to interconnectable tiles configured for operation in an aquatic environment or a near-zero/zero gravity environment. The interconnectable tiles are configured to interconnect relative to one another to form interconnected surfaces, and individual interconnectable tiles provide thrust, ballast, and/or buoyancy to the overall interconnected surface so as to move the interconnected surface in a desired configuration.

TRAFFIC CONTROL SYSTEM, CONTROLLER AND METHOD FOR DIRECTING VEHICLE BEHAVIOR AT A DEFINED SPATIAL LOCATION
20200130826 · 2020-04-30 · ·

A traffic control system, a controller and an associated method are provided to direct a vehicle to slow or, in some instances, stop at a defined spatial location along the roadway. In the context of a controller, the controller includes at least one processor and memory including computer program code with the memory and the computer program code configured to, with the at least one processor, cause the controller to receive information indicative of at least one characteristic of the behavior of the vehicle as the vehicle approaches a defined location. Based on the information, the controller is caused to compare the behavior of the vehicle to a defined criterion and, in response, to cause an unmanned air vehicle (UAV) to maintain a hovering position in which the UAV hovers above the roadway so as to be within the path of travel of the vehicle on the roadway.

SYSTEM AND METHOD OF MANAGING A PROJECTILE MODULE ON A FLYING DEVICE

A flying vehicle is disclosed with a projectile module or component that contains a projectile for projecting at another flying device. The flying vehicle receives an identification of a target flying device and applies a projectile model which generates a determination that indicates whether a projectile, if fired from the projectile component, the projectile will hit the target flying device. The projectile model taking into account one or more of a wind modeling in an area around the flying vehicle based on an inference of wind due to a tilt of the flying vehicle, a projected path of the target device based on its identification and a drag on the projectile as it deploys from the projectile component. When the determination indicates that the projectile will hit the targeted device according to a threshold value, the flying vehicle fires the projectile at the targeted flying device.

Power generating windbags and waterbags
10619625 · 2020-04-14 ·

A method of using a bagged power generation system comprising windbags and waterbags integrated with drones and adapting drone technologies for harnessing wind and water power to produce electricity. An extremely scalable and environmentally friendly method, system, apparatus, equipment, techniques and ecosystem configured to produce renewable green energy with high productivity and efficiency.

AERIAL VEHICLE WITH DEPLOYABLE COMPONENTS

An unmanned aerial vehicle with deployable components (UAVDC) is disclosed. The UAVDC may comprise a fuselage, at least one wing, and at least one control surface. In some embodiments, the UAVDC may further comprise a propulsion means and/or a modular payload. The UAVDC may be configured in a plurality of arrangements. For example, in a compact arrangement, the UAVDC may comprise the at least one wing stowed against the fuselage and the at least one control surface stowed against the fuselage. In a deployed arrangement, the UAVDC may comprise the at least one wing deployed from the fuselage and the least one control surface deployed from the fuselage. In an expanded arrangement, the UAVDC may comprise the at least one wing telescoped to increase a wingspan of the deployed arrangement.

SYSTEM AND METHOD FOR OBSTACLE AVOIDANCE IN AERIAL SYSTEMS
20200090530 · 2020-03-19 ·

An aerial system includes a body, a lift mechanism coupled to the body, a processing system, and at least one camera. The aerial system also includes a first motor configured to rotate the at least one camera about a first axis and a second motor configured to rotate the at least one camera about a second axis. The processing system is configured to determine a direction of travel of the aerial system and to cause the first motor and the second motor to automatically orient the at least one camera about the first axis and the second axis such that the at least one camera automatically faces the direction of travel of the aerial system.