An unmanned aerial vehicle according to certain embodiments generally includes a chassis, a power supply mounted to the chassis, a control system operable to receive power from the power supply, at least one rotor operable to generate lift under control of the control system, and a motor operable to lower a free end of a line. The free end of the line is operable to engage a parcel to be delivered by the unmanned aerial vehicle. The control system is configured to operate the motor to cause the free end of the line to accelerate toward a delivery surface as the free end of the line passes through a first portion of a distance between the unmanned aerial vehicle and the delivery surface, and to decelerate as the free end of the line passes through a lower portion of the distance.

An aircraft ground support unit, which is mobile, for supplying a service to an aircraft on the ground according to a specific servicing program is provided that includes a GPS to identify an instantaneous position of the ground support unit, a receiver suitable for identifying an aircraft by receiving information emitted by a transponder of said aircraft including one or more of: an instantaneous GPS coordinates of an aircraft position, an identity of the aircraft, a type of aircraft, a company of the aircraft, or aircraft status data, and a microprocessor configured for calculating a distance, d, of the aircraft from the ground support unit, selecting a predefined specific servicing program stored in a database corresponding to the type and company of the thus identified aircraft, controlling the ground support unit to implement the thus selected specific servicing program, and logging aircraft and ground unit data for airlines optimization.

A base apparatus for docking of at least one flying apparatus includes a controller. The controller outputs information of a location to which the base apparatus is to be moved, the location being determined based on a predetermined condition including a condition related to the battery level of the at least one flying apparatus.

A self-insulating air delivery and recirculation system maintains a desired air temperature of the conditioned air supplied thereinto for delivery to an aircraft. The system uses insulating airflow layers; a parallel layer and a counterflow layer. A starting section connects to a PCA unit and delivers conditioned air therefrom to an interior supply hose. The starting section supplies conditioned insulating air to an interior insulating hose that is annularly outward of the supply hose and in which air flows parallel to airflow in the supply hose. A reversing connector indirectly connects the supply hose to the aircraft and reverses the flow of air from the interior insulating hose to flow back toward the PCA unit in an exterior counterflow hose that is annularly outward of the interior insulating hose and connects at its far end to provide intake airflow to the PCA unit.

An UAV controller device is provided. In some embodiments, the device may include a control panel having one or more user control inputs, and a processing unit may be in communication with the control inputs. A display screen may also be in communication with the processing unit. Optionally, the display screen may be movable between an open and a closed position. A side wall may be coupled to a proximal wall and to a distal wall, the side wall, proximal wall, and distal wall forming a storage compartment. The storage compartment may have a storage cavity for removably receiving a UAV, and the UAV may be in wireless communication with the processing unit. A camera, for recording video, may be coupled to the UAV. Video recorded by the camera may be displayed on the display screen, and one or more of the control inputs may govern movement of the UAV.

A drone equipped with piezoelectric structures and/or a self-energizing capability has increased functionality. The piezoelectric structures can act as a variety of sensors and/or can implement or perform a variety of tasks, especially those associated with assisting a vehicle. The self-energizing capability can extend operations and/or permit a drone low on power to sufficiently recharge to fly home.

A system performs a control method to launch an unmanned aerial vehicle, UAV. The control method includes calculating a selected altitude, relative to a reference level, for launching the UAV, operating a lifting arrangement to vertically elevate the UAV to the selected altitude, and causing the UAV to be launched from the selected altitude. Elevating the UAV may improve the performance of the UAV in terms of range, power consumption, ability to carry payload, transit time to destination, etc. The selected altitude may be calculated as a function of parameter data representing any of the UAV, the lifting arrangement, or surrounding conditions. An apparatus is further provided to determine an optimal location of the system in relation to a plurality of destinations of UAVs to be elevated by the system.

A system is provided for multi-engine coordination of gas turbine engine motoring in an aircraft. The system includes a controller operable to determine a motoring mode as a selection between a single engine dry motoring mode and a multi-engine dry motoring mode based on at least one temperature of a plurality of gas turbine engines and initiate dry motoring based on the motoring mode.

A docking assembly for unmanned aerial vehicles (UAVs). The docking assembly includes a dock having a shaft. The present invention further includes UAVs. Each of the UAVs include a slot sized such that the shaft may slidably engage the slot. The shaft of the dock inserts through the slot of the UAVs, thereby docking the UAVs on the dock.

Example implementations may relate to self-deployment of operational infrastructure by an unmanned aerial vehicle (UAV). Specifically, a control system may determine operational location(s) from which a group of UAVs is to provide aerial transport services in a geographic area. For at least a first of the operational location(s), the system may cause a first UAV from the group to perform an infrastructure deployment task that includes (i) a flight from a source location to the first operational location and (ii) installation of operational infrastructure at the first operational location by the first UAV. In turn, this may enable the first UAV to operate from the first operational location, as the first UAV can charge a battery of the first UAV using the operational infrastructure installed at the first operational location and/or can carry out item transport task(s) at location(s) that are in the vicinity of the first operational location.