Patent classifications
B64F3/00
Wind harvesting systems and methods
Various embodiments of the present disclosure provide wind harvesting systems and methods using crosswind power kites and methods for launching crosswind power kites into wing-borne flight, for generating electricity through such flights, and for landing or retrieving such crosswind power kites.
Wind harvesting systems and methods
Various embodiments of the present disclosure provide wind harvesting systems and methods using crosswind power kites and methods for launching crosswind power kites into wing-borne flight, for generating electricity through such flights, and for landing or retrieving such crosswind power kites.
METHOD AND APPARATUS FOR SURFACE ATTACHMENT OF MODULAR UNMANNED AERIAL VEHICLE FOR INSPECTION
A modular aerial vehicle for inspection of enclosed and open space environments. The aerial vehicle is employed for inspection of various environments in remotely controlled and autonomous fashions. The aerial vehicle is capable of carrying different sensory modules depending on the specific application including surface inspection. Aerial vehicle may be connected to a tether cable for electrical power delivery and transmission of control commands. The aerial vehicle may utilize a landing structure which allows landing on any angled metallic or non-metallic surface.
HIGH ALTITUDE ATMOSPHERIC ENERGY STORING APPARATUS
The present invention relates to a high altitude atmospheric energy storing apparatus having a new structure, which is conceived to store the energy of low-temperature air located at high altitude in the sky and utilize it as needed. The high altitude atmospheric energy storing apparatus includes an air tank adapted to store air, an air supply pipe provided such that it extends in a vertical direction and its lower end is connected to the air tank, and a compression means provided in the sky, connected to the upper end of the air supply pipe, and configured to compress air using the wind and supply the compressed air to the air tank through the air supply pipe, thereby enabling air to be compressed by the wind blowing at high altitude and to be then stored in the air tank (10).
SYSTEMS, METHODS, AND DEVICES FOR VEHICLE INTEGRATION OF UNMANNED AIRCRAFT SYSTEMS
Systems and methods are disclosed for vehicle integration of unmanned aircraft systems (UASs). Example methods may include coupling a landing dish of a vehicle integrated UAS to a ground station assembly; positioning the landing dish and the ground station assembly into a portion of a vehicle and a capping member of the vehicle integrated UAS; and coupling the landing dish to the capping member of the vehicle integrated UAS. In various embodiments, the vehicle integrated UAS may be configured to send and receive information (e.g., route information, power information, status information, etc.) between unmanned aerial vehicles (UAV) associated with the UAS to device(s) of a vehicle.
SPOOLER FOR UNMANNED AERIAL VEHICLE SYSTEM
In an aspect, in general, a spooling apparatus includes a filament feeding mechanism for deploying and retracting filament from the spooling apparatus to an aerial vehicle, an exit geometry sensor for sensing an exit geometry of the filament from the spooling apparatus, and a controller for controlling the feeding mechanism to feed and retract the filament based on the exit geometry.
SPOOLER FOR UNMANNED AERIAL VEHICLE SYSTEM
In an aspect, in general, a spooling apparatus includes a filament feeding mechanism for deploying and retracting filament from the spooling apparatus to an aerial vehicle, an exit geometry sensor for sensing an exit geometry of the filament from the spooling apparatus, and a controller for controlling the feeding mechanism to feed and retract the filament based on the exit geometry.
METHOD AND SYSTEM FOR DETECTING, POSITIONING AND CAPTURING AN INTRUDER IN-FLIGHT USING A LASER DETECTION AND RANGING DEVICE
A method and a system for detecting and positioning an intruder within a specified volume are provided herein. The method may include the following steps: periodically scanning using a laser detection and ranging (LADAR) device directing a laser beam, within the specified volume; collecting reflections of the laser beam arriving from objects within the volume; converting the reflections to LADAR signal indicative of spatiotemporal presence of objects within the volume; applying signal processing algorithms to the LADAR signals, to determine a presence of an intruder and respective orientation parameters, based on predefined criteria; directing a camera based on the orientation parameters associated with the intruder for continuously capturing images of the intruder; and analyzing the images by a computer processor and instructing the camera to track the intruder based on the analysis, to yield real-time tracking parameters of the intruder.
METHOD AND SYSTEM FOR DETECTING, POSITIONING AND CAPTURING AN INTRUDER IN-FLIGHT USING A LASER DETECTION AND RANGING DEVICE
A method and a system for detecting and positioning an intruder within a specified volume are provided herein. The method may include the following steps: periodically scanning using a laser detection and ranging (LADAR) device directing a laser beam, within the specified volume; collecting reflections of the laser beam arriving from objects within the volume; converting the reflections to LADAR signal indicative of spatiotemporal presence of objects within the volume; applying signal processing algorithms to the LADAR signals, to determine a presence of an intruder and respective orientation parameters, based on predefined criteria; directing a camera based on the orientation parameters associated with the intruder for continuously capturing images of the intruder; and analyzing the images by a computer processor and instructing the camera to track the intruder based on the analysis, to yield real-time tracking parameters of the intruder.
SYSTEMS, METHODS, AND DEVICES FOR PACKAGE DELIVERY USING UNMANNED AERIAL VEHICLES
Systems and methods are disclosed for package delivery using unmanned aerial vehicles. Example methods may include positioning a first component at a first elevation, and operatively connecting the first component to a winch; positioning a second component at a second elevation higher than the first elevation; and configuring cable of a lifting component to: operatively connect to the first component and the second component, connect to and disconnect from a vehicle, and lift the vehicle from the first component towards the second component using the winch.