Patent classifications
B64U70/90
ENERGY SUPPLY SYSTEM
An energy supply system, which is a system constituting a regional power system in a target region, includes a power transmission system including a first power generation facility and a second power generation facility, a power transmission and distribution system that supplies power to each consumer, a management system, and an unmanned flying object. The unmanned flying object has a transport function of transporting a cargo and a power supply function of supplying power to an outside. When the amount of power supplied by the power transmission system is less than the amount of power required by the power transmission and distribution system, the management system performs a power adjustment process of supplying power from the unmanned flying object to the power transmission and distribution system by using the power supply function of the unmanned flying object.
DRONE SYSTEM WITH DISTRIBUTED BASING
A system for basing drones is described. A network of geographically diverse hangars provides storage and charging locations as well as backhaul communications infrastructure and video monitoring. As drones are needed, a central command point tasks an available drone, which may or may not already be located in proximity to a target. If additional drones are needed, drones can be flown to the area of interest and continuous coverage provided by charging drones while an active drone is conducting the mission, then rotating charged drones into the active mission. Structures for the hangars, the overall system, and methods of operation are described.
BATTERY ARM SENSOR ASSEMBLY
The present disclosure is directed toward a system for autonomously landing an unmanned aerial vehicle (UAV) within an unmanned aerial vehicle ground station (UAVGS) and removing a battery assembly from within the UAV while landed. In particular, systems described herein enable a battery arm to engage a battery assembly and remove the battery assembly from within the UAV. Additionally, the battery arm can include one or more sensors that detect a pattern of sensor contacts arranged on an end of the battery assembly. In particular, the sensors on the battery arm can detect and identify the battery assembly based on the particular pattern of sensor contacts on the end of the battery assembly.
AERIAL VEHICLE WITH ENHANCED PITCH CONTROL AND INTERCHANGEABLE COMPONENTS
An aircraft capable of vertical take-off and landing comprises a fuselage, at least one processor carried by the fuselage and a pair of aerodynamic, lift-generating wings extending from the fuselage. A plurality of vectoring rotors are rotatably carried by the fuselage so as to be rotatable between a substantially vertical configuration relative to the fuselage for vertical take-off and landing and a substantially horizontal configuration relative to the fuselage for horizontal flight. The vectoring rotors are unsupported by the first pair of wings. The wings may be modular and removably connected to the fuselage and configured to be interchangeable with an alternate pair of wings. A cargo container may be secured to the underside of the fuselage, and the cargo container may be modular and interchangeable with an alternate cargo container.
ANTENNA FOR CHARGING AND MEASURMENT, AND METHOD AND APPARATUS FOR MEASURING RADIO WAVES AND WIRELESS CHARGING USING THE SAME
An antenna for charging and measurement may comprise: a telescopic support installed at a lower portion of an aerial vehicle and configured to contract when the aerial vehicle lands on a wireless station and extend when the aerial vehicle takes off from the wireless station; and an antenna coil part deformed into a spiral shape when the telescopic support is contracted so that the wireless station receives wireless power and deformed into a conical shape when the telescopic support is extended to measure a radio signal.
ANTENNA FOR CHARGING AND MEASURMENT, AND METHOD AND APPARATUS FOR MEASURING RADIO WAVES AND WIRELESS CHARGING USING THE SAME
An antenna for charging and measurement may comprise: a telescopic support installed at a lower portion of an aerial vehicle and configured to contract when the aerial vehicle lands on a wireless station and extend when the aerial vehicle takes off from the wireless station; and an antenna coil part deformed into a spiral shape when the telescopic support is contracted so that the wireless station receives wireless power and deformed into a conical shape when the telescopic support is extended to measure a radio signal.
Construction Machine
A construction machine system that can shorten a work period is described. A construction machine system includes a main body that is revolvable by revolving of a revolving device, a first working device including a plurality of actuators and connected to the main body, and a second working device including a plurality of actuators and connected to the main body.
Construction Machine
A construction machine system that can shorten a work period is described. A construction machine system includes a main body that is revolvable by revolving of a revolving device, a first working device including a plurality of actuators and connected to the main body, and a second working device including a plurality of actuators and connected to the main body.
Access management system
An access management system includes a mobile device with a processor and a memory and a software platform including at least a processor and a memory. The software platform is configured to analyze data obtained from the mobile device and other devices connected to the software platform. Specifically, the software platform is operable to determine if an access key received, read, or captured by a mobile device matches an access key for an authorized account, object, device, or space for the mobile device, and to provide access to the mobile device if the access key received, read, or captured by the mobile device matches the authorized access key.
Self-centering landing platform
Example landing platform systems and methods are described. In one implementation, a landing platform includes a top plate configured to support an unmanned aerial vehicle (UAV), where the top plate has a plurality of slots therethrough. A rotating plate is located adjacent the top plate and includes multiple centering pins extending therefrom and extending through the plurality of slots in the top plate. A motor is capable of rotating the rotating plate, which causes the multiple centering pins to center the UAV on the top plate.