A battery connector for connecting a replaceable battery to an aerial vehicle, comprising a housing configured for fixing to one of the replaceable battery and the aerial vehicle. The connector element includes a first connection portion for releasable connection to an external connection element of the other one of the replaceable battery and the aerial vehicle and a second connection portion for fixed connection to the replaceable battery or the aerial vehicle. The connector element is supported in a horizontal direction in the housing by at least one flexible element positioned at least partly between the connector element and the housing and in a vertical direction in the housing by an upper flexible element positioned between an upper part of the connector element and the housing and a lower flexible element positioned between a lower part of the connector element and the housing.

Systems and methods involving dynamic recharge features and functionality for electric vehicles and other applications are disclosed. In one example, an illustrative electro-mechanical power system may comprise an electric vehicle (EV) motor that drives a shaft, an EV battery module coupled to the EV motor, and a dynamic recharge system coupled to the EV battery module, wherein the DRS includes an ambient air intake, a turbo coupled to the air intake and configured to create power that is used to charge the EV battery module, and a generator assembly. Further, the generator assembly may include a generator and a generator control module, wherein the generator includes a rotor coupled to the turbo, and the generator control module includes control electronics that manage and provide the electrical energy as an output to the EV battery module and/or the EV motor. Other embodiments for differing applications are also disclosed.

Systems and methods involving dynamic recharge features and functionality for electric vehicles and other applications are disclosed. In one example, an illustrative electro-mechanical power system may comprise an electric vehicle (EV) motor that drives a shaft, an EV battery module coupled to the EV motor, and a dynamic recharge system coupled to the EV battery module, wherein the DRS includes an ambient air intake, a turbo coupled to the air intake and configured to create power that is used to charge the EV battery module, and a generator assembly. Further, the generator assembly may include a generator and a generator control module, wherein the generator includes a rotor coupled to the turbo, and the generator control module includes control electronics that manage and provide the electrical energy as an output to the EV battery module and/or the EV motor. Other embodiments for differing applications are also disclosed.

A drone fishing system mountable on a fishing vessel having an aft portion includes a landing pad mounted having a drone station mounted on the aft portion of the fishing vessel, an unmanned aerial vehicle (UAV), and tether line and tether reel for maintaining an electrical connection between the drone station and the UAV. The UAV including a computing module for determining optimal positioning of the UAV with respect to the fishing vessel during operation. The UAV tether line spools about the tether reel and has an abrasion resistant cable jacket for enabling a selective engagement of a clip on the tether line. A first altimeter mounted on the fishing vessel. A second altimeter mounted on the UAV. The first and second altimeters communicate with the computing module of the UAV. The electrical connection communicates power and data between the landing pad and the UAV.

A drone fishing system mountable on a fishing vessel having an aft portion includes a landing pad mounted having a drone station mounted on the aft portion of the fishing vessel, an unmanned aerial vehicle (UAV), and tether line and tether reel for maintaining an electrical connection between the drone station and the UAV. The UAV including a computing module for determining optimal positioning of the UAV with respect to the fishing vessel during operation. The UAV tether line spools about the tether reel and has an abrasion resistant cable jacket for enabling a selective engagement of a clip on the tether line. A first altimeter mounted on the fishing vessel. A second altimeter mounted on the UAV. The first and second altimeters communicate with the computing module of the UAV. The electrical connection communicates power and data between the landing pad and the UAV.

A modular autonomous aerial passenger vehicle is provided to automatically transport any person or luggage or capable of being used by the defense organizations for monitoring without any interference or need of human pilot. The autonomous aerial vehicle is comprising of an aerodynamic main body having 4 fixed arms each and 2 foldable arms each of which further having a pair of propellers coupled at the edge of each foldable arm, one at the top and one at the bottom. Further, the autonomous aerial vehicle further includes a power management system; safety system; interior cockpit having a HMI and seating arrangement, where the HMI is a brain computer interface that acquires signals from the brain and analyses them to convert it into commands. It includes a display unit and manual control unit; primary and auxiliary battery modules, flight control unit, plurality of sensors and cameras and other safety equipment for safe functioning of the present autonomous aerial vehicle.

In an aspect, a system for a guidance interface for a vertical take-off and landing (VTOL) aircraft comprises a plurality of flight components that are mechanically coupled to the VTOL aircraft. The VTOL aircraft also comprises an output device that is configured to present a display of the outside environment. The output device may overlay the display with a datum, a focal point, and a guidance symbol. The datum may be associated with the flight components of the VTOL aircraft. The focal point may be indicative of a desired landing location for the VTOL aircraft. The focal point may be determined by at least a predetermined flight plan. The guidance symbol may be a symbol that includes an optimal flight path to the focal point.

Recently, jobs involving transporting goods, tasks involving surveying a wide area, etc. using multicopters have increased, and it has become necessary for multicopters to fly for long periods of time, In the present invention, wings that are separate from the main body are provided all the way around or at individual locations around it to connect neighboring pairs of the multiple arms extending radially from it, in order to increase the multicopter’s lift and extend its flight time.

Systems, devices, and techniques for active thermal control of energy storage units are described. In some embodiments, an unmanned aerial vehicle (UAV) includes a battery pack. The battery pack includes a plurality of battery cells and an enclosure coupled with the plurality of battery cells to physically retain the plurality of battery cells in an arrangement. The arrangement defines a void space between the plurality of battery cells. The UAV also includes a cooling system configured to cool the battery cells. The cooling system includes a source of forced convection fluidically coupled with the battery pack to drive a cooling fluid through the void space. The cooling system also includes a cooling controller electrically coupled with the source of forced convection to controllably activate the source of forced convection.

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.