Patent classifications
B64F1/00
Aeronautical light aid for vertical takeoff and landing
An aeronautical light aid for a vertical takeoff and landing (VTOL) flying object is provided. The aeronautical light aid includes a plurality of first lighting portions buried in a takeoff and landing port and configured to radiate light in a vertically upward direction, a plurality of second lighting portions provided on an outer side of the takeoff and lighting port and configured to radiate light in an externally upward direction, and a landing guide provided at the center of the takeoff and landing port.
Base Stations Including Integrated Systems For Servicing UAVs
A base station is disclosed for use with an unmanned aerial vehicle (UAV). The base station includes: an enclosure; a cradle that is configured to charge a power source of the UAV during docking with the base station; and a temperature control system that is connected to the cradle and which is configured to vary temperature of the power source of the UAV. The temperature control system includes: a thermoelectric conditioner (TEC); a first air circuit that is thermally connected to the TEC and which is configured to regulate temperature of the TEC; and a second air circuit that is thermally connected to the TEC such that the TEC is located between the first air circuit and the second air circuit. The second air circuit is configured to direct air across the cradle to thereby heat or cool the power source of the UAV when docked with the base station.
RUNWAY ARRANGEMENT FOR SIMULTANEOUS LANDING AND TAKE OFF
An airport runway arrangement for commercial aircraft comprises a first runway section, a second runway section extending substantially in prolongation of the first runway section and an intermediate section between the first and second runway sections.
RUNWAY ARRANGEMENT FOR SIMULTANEOUS LANDING AND TAKE OFF
An airport runway arrangement for commercial aircraft comprises a first runway section, a second runway section extending substantially in prolongation of the first runway section and an intermediate section between the first and second runway sections.
Device for the automated charging and discharging of a free-flying autonomously controlled drone
A device for the automated charging and discharging of an object on a free-flying autonomously controlled drone includes a landing platform for the drone, a storage device for storing objects, a robot where the robot is configured to remove an object from the storage apparatus in an automated manner and to provide the object on the landing platform to be picked up by the drone and is configured to pick up in an automated manner an object that is provided on the landing platform by the drone and to deposit the object in the storage apparatus, and a controller where the robot is controllable by the controller.
Protective cover for an aircraft comprising electromagnets
A protective cover for the protection of an aircraft having a fuselage and two wings, includes an anchoring system fixing the protective cover to the aircraft, a tarpaulin having a retracted position wherein it is gathered up and a deployed position wherein it is spread over the wing, a deployment device making the tarpaulin move from the retracted to the deployed position, an electromagnet fixed to the tarpaulin face against the wing, and having a deactivated state and an active state, a remote control, and a control system including a control unit in communication with the remote control. When the control unit receives activation information from the remote control, the control unit controls the deployment device, to make the tarpaulin move from the retracted position to the deployed position, and activates each electromagnet. When the control unit receives deactivation information from the remote control, the control unit deactivates each electromagnet.
GROUND SUPPORT STATION FOR AERIAL VEHICLES
A ground station for aerial vehicles including a protective casing, at least one charging mechanism, and an extendable landing pad. The extended landing pad is operable to transition between a closed configuration having dimensions suitable to be contained within said protective casing, and an open configuration having dimensions suitable to land the aerial vehicle.
METHODS FOR RECONFIGURABLE POWER EXCHANGE FOR MULTIPLE UAV TYPES
A reconfigurable system capable of autonomously exchanging material from unmanned vehicles of various types and sizes. The system comprises an environmental enclosure, a landing area, a universal mechanical system to load and unload material from the unmanned vehicle, and a central processor that manages the aforementioned tasks. The landing area may comprise a one or more visible or non-visible markers/emitters capable of generating composite images to assist in landing the unmanned vehicle upon the reconfigurable, autonomous system.
Systems and methods for UAV docking
An apparatus for housing an unmanned aerial vehicle (UAV) in or on a vehicle includes a landing connection component configured to form a connection between the UAV and the vehicle when the UAV is landed in or on the vehicle, and a cover movable between a plurality of positions to permit the UAV to take off and land in or on the vehicle. The cover includes an antenna or a satellite dish integrated thereto. An orientation of the antenna or the satellite dish is adjustable for tracking a motion of the UAV when the UAV is in flight.
Systems and methods for UAV docking
An apparatus for housing an unmanned aerial vehicle (UAV) in or on a vehicle includes a landing connection component configured to form a connection between the UAV and the vehicle when the UAV is landed in or on the vehicle, and a cover movable between a plurality of positions to permit the UAV to take off and land in or on the vehicle. The cover includes an antenna or a satellite dish integrated thereto. An orientation of the antenna or the satellite dish is adjustable for tracking a motion of the UAV when the UAV is in flight.