The disclosure concerns a drone trailer system. The drone trailer system includes a rear door hingedly coupled to a distal end of a trailer. A first track system is disposed on the trailer at a floor thereof. A second track system is disposed on the rear door at an inner surface thereof. A movable platform is slidably engaged with the first track system, the second track system, or both. A drone is configured to sit on top of the moveable platform to allow for fast deployment.

Example UAV landing systems and methods are described. In one implementation, a landing platform includes a conveyor belt capable of supporting an unmanned aerial vehicle (UAV). The conveyor belt can move in a first direction and a second direction that is opposite the first direction. The landing platform also includes a first positioning bumper and a second positioning bumper, where the first positioning bumper and the second positioning bumper are capable of repositioning the UAV on the conveyor belt. The landing platform further includes a cradle that can receive and secure the UAV.

Methods are provided for enabling network operators to play a key role in allowing Cellular Unmanned Aerial Vehicles (UAVs) to recharge batteries based on RF parameters and/or a class of service the UAVs provide to users/customers. For example, a particular mobile network operator (MNO) has a UAV charging station deployed in it leased towers where it has base stations (eNB/gNB) deployed. The MNO can provide charging as a service to the UAVs. When more than one drone is requesting a charge, the MNO can prioritize which UAV has the highest priority. In some aspects, the MNO can prioritize the UAVs for charging based on a Quality of Service identifier. Additionally or alternatively, the MNO can prioritize the UAVs for charging based on a Network Slice Selection Assistance Information indicator.

A technique for determining the number of appropriate work entities is implemented. A simulator includes: a transport capacity acquisition portion for acquiring the transport capacity of work entities; a load information acquisition portion; a map information acquisition portion; a work entity situation acquisition portion; and a number-of-work entities determination portion for determining the number of work entities.

Disclosed is a take-off and landing station (1) for a flying vehicle (2) for transporting people and/or loads, which flying vehicle takes off and lands vertically and comprises a flight module (3), having a plurality of drive units (17) arranged on a supporting framework structure (16) of the flight module (3), and a transportation module (4), which can be coupled to the flight module (3). The take-off and landing station (1) comprises a holding apparatus (21) having a plurality of gripper elements and support elements (11) for supporting, fixing and/or orienting the supporting framework structure (16) during take-off and landing of the flying vehicle (2) or the flight module (3).

Systems and methods are described herein for providing wireless power to a mobile device, such as an aerial mobile device like an unmanned aerial vehicle (UAV). A navigational constraint model may prescribe a navigation path along which a wireless power transmission system can provide wireless power to the mobile device. Deviations from the prescribed path may require the mobile device to self-power. The prescription of a navigation path allows for the use of reduced-complexity wireless power transmitters that are fully capable of servicing the prescribed path. Multiple embodiments of prescribed paths with various limitations and features are set forth herein, along with multiple embodiments of wireless power transmission systems of reduced complexity and functionality to fully service the various embodiments of prescribed paths.

In a hybrid flight vehicle, having four rotors attached to a frame and configured to produce propelling force to propel the frame, a gas turbine engine attached to the frame and configured to rotate when fuel is supplied, a generator connected to an output shaft of the engine and configured to generate electric power when driven by the engine, a battery configured to store the electrical power generated by the generator, and four first electric motors each connected to the rotors to drive associated one of the rotors when the electric power is supplied from the battery, and an electronic control unit configured to control flight by regulating driving of the four rotors by the first electric motors. In the vehicle, the output shaft of the engine is attached parallel to at least one among yaw axis, pitch axis and roll axis of the frame.

A charging and recharging drone assembly system and apparatus are provided. The system has a unique charging pad having a plurality of cones which direct the legs of a charging drone into a specific location on the charging pad for charging/re-charging. A QR code may be located in the middle of a cover of a charging pad so that the charging drone may detect the charging pad from the air and may direct the charging drone to land on a specific spot on the landing pad for charging. The movable cover may cover the charging pad when the charging pad is not in use to protect the charging pad.

Disclosed herein is a system comprising: a hydrogen fuel cell; a fuel storage tank; a regulator coupled to the storage tank and the fuel cell; an electronic auto pilot; a rechargeable battery; a power electronics module for delivering power from the fuel cell to the autopilot and the battery; and a heat exchanger coupled to the fuel cell. The fuel cell is characterized by: a minimum continuous power output of no more than 25 W; a maximum continuous power output of no less than 5000 W; a specific power of at least 200 W/kg based on the mass of the fuel cell and any control electronics, cooling components, air delivery components, and water management components; an ability to operate at least 2 psig of hydrogen at an inlet; and an ability to operate at temperatures up to 90° C.

A drone-based product delivery mechanism in which power is transferred between the drone's battery and a product's battery while the product is in transit to its destination. For a short distance delivery, the drone battery may be used to charge the product battery so that the product is delivered with a fully-charged battery. On the other hand, for long distance deliveries, the power from a fully-charged product battery may be used to charge the drone's battery to extend the flight time/radius of the drone or to supplement the drone battery to conserve its power. The power transfer may be carried out using a wireless connection or a wired connection. The wireless connection may be a Qi interface, whereas the wired connection may be a Universal Serial Bus (USB) connection. The product packaging may be re-designed to allow the desired power transfer between the drone and the product inside the packaging.