Described herein is an elevated unmanned aerial vehicle (UAV) station. The elevated UAV station includes an elevated platform and a conveyance device configured to raise a payload to the elevated platform. The elevated unmanned UAV station may further include a launch device configured to cause a takeoff of a UAV from the elevated platform. The elevated UAV station may further include a recovery device configured to cause a controlled landing of the UAV at the elevated platform. The elevated UAV station may be associated with a payload housing structure to establish a system for payload storage and launch.

An unmanned aerial vehicle includes a fuselage having a first side and a second side, a first arm disposed on a first side of the fuselage, wherein the first arm is coupled to one or more first propellers, wherein the first arm is adapted to move between a first folded position in which the first arm is in a folded state inside the fuselage and a first extended position in which a first section of the first arm and the one or more first propellers are outside the fuselage, and a second arm disposed on the second side of the fuselage, wherein the second arm is coupled to one or more second propellers, wherein the second arm is adapted to move between a second folded position in which the second arm is in a folded state inside the fuselage and a second extended position in which a second section of the second arm and the one or more second propellers are outside the fuselage.

A base module may be used to receive and house one or more unmanned aerial vehicles (UAVs) via one or more cavities. The base module receives commands from a manager device and identifies a flight plan that allows a UAV to execute the received commands. The base module transfers the flight plan to the UAV and frees the UAV. Once the UAV returns, the base module once again receives it. The base module then receives sensor data from the UAV from one or more sensors onboard the UAV, and optionally receives additional information describing its flight and identifying success or failure of the flight plan. The base module transmits the sensor data and optionally the additional information to a storage medium locally or remotely accessible by the manager device.

There is provided a landing platform for mounting on a luminaire, where the landing platform provides an interface to a drone. For example, there is provided a landing platform for a drone, the landing platform being adaptable to mount on a luminaire. The landing platform includes two electrically active portions and an elevated portion. The elevated portion is configured to secure the drone on the landing platform and provide electrical contact between the two electrically active portions and electrical connectors of the drone.

According to an aspect, a distributed package transport system includes unmanned aerial vehicles (UAVs), each of which is configured to transport packages within a geographic area and along a travel route. The system also includes UAV enclosures dispersed within the geographic area. The UAV enclosures include a number of cells, each of which provides a receptacle to temporarily house a UAV. At least one of the UAV enclosures is dynamically assigned to a location within the geographic area. Each of the UAV enclosures includes a computer processor and communication network interface and, for each of the UAVs in transit, the UAV enclosures communicate information specifying an origination point, drop off point, and return point amongst each other and coordinate to define, based on locations of the UAV enclosures and capacities of the UAV enclosures, a refined travel route including a subset of the UAV enclosures to serve as hops.

A multi-rotor aircraft with multi-shaft dislocation layout including a frame, a plurality of upper-layer power sources, a plurality of lower-layer power sources, a plurality of upper-layer propeller blades and a plurality of lower-layer propeller blades. The plurality of upper-layer propeller blades are disposed at intervals, and are connected to the upper side of the frame through the plurality of upper-layer power sources. The plurality of lower-layer propeller blades are disposed at intervals, and are connected to the lower side of the frame through the plurality of lower-layer power sources. The plurality of upper-layer propeller blades and the plurality of lower-layer propeller blades are staggered along a projection direction of the frame. The centers of the plurality of upper-layer propeller blades and the centers of the plurality of lower-layer propeller blades are located on the same flat geometric figure along the projection direction of the frame.

One embodiment is an aircraft including a main body, a plurality of propulsion assemblies, and a plurality of hinges, wherein each of the plurality of propulsion assemblies is rotatably coupled to the main body using a hinge from the plurality of hinges. In an example, the aircraft includes four motor support arms and each motor support arm rotatably couples a specific propulsion assembly to a specific corresponding hinge on the main body of the aircraft and increases a span of the aircraft when the aircraft is in the flight configuration and reduces the footprint of the aircraft when the aircraft is in a storage configuration.

Embodiments of the present invention discloses a wing detachment assembly and an aerial vehicle. The wing detachment assembly includes a first connecting portion and a second connecting portion. The first connecting portion includes a fixing base, a press-fitting member and a fastening member, one of the fixing base and the second connecting portion being fixed on a wing and the other being fixed on a vehicle body. A mounting groove is provided on the second connecting portion, a notch of the mounting groove being provided far away from the first connecting portion. The press-fitting member is rotatably connected to the fixing base, the fastening member is rotatably connected to the press-fitting member, an end of the fastening member is fastened in the mounting groove.

A system for a wind park including: a control system in communication with a plurality of unmanned air vehicles, wherein the control system is configured to deploy one or more unmanned air vehicles during a triggering condition; and wherein the deployed unmanned air vehicles are guided towards an assigned wind turbine and to interact with a blade of that wind turbine in order to control oscillation of the blade. The invention also embraces a method for reducing blade oscillations of a wind turbine, comprising: monitoring for a triggering condition associated with the wind turbine; on detecting the triggering condition, deploying unmanned air vehicles towards a wind turbine and interacting with a blade of the wind turbine using the unmanned air to control oscillation of the blade. The invention therefore provides an efficient approach to controlling blade oscillations with minimal human operator involvement. Drones may be deployed automatically once suitable conditions are detected and may automatically engage with the blades, either by contacting those blades physically, or by interacting with the blades in close proximity, in order to disrupt airflow around the blades thereby reducing oscillations.

An unmanned aerial vehicle (UAV), a stand for launching, landing, testing, refueling and recharging a UAV, and methods for testing, landing and launching the UAV are disclosed. Further, embodiments may include transferring a payload onto or off of the UAV, and loading flight planning and diagnostic maintenance information to the UAV.