A connector system for an aircraft, for connecting a hose line, includes a skin panel which has a clearance which extends between an external face and an internal face, a primary part which on the clearance is disposed on an internal side of the skin panel that is defined by the internal face, a cover mounted on the primary part and movable between a closing position in which the cover covers the clearance of the skin panel, and an opening position in which the cover releases the clearance of the skin panel, and a tubular connector port mounted on the primary part and movable between a storage position in which the connector port is disposed on the internal side of the skin panel, and a use position in which the connector port projects beyond the external face of the skin panel.

A package unloading and conveying system including a landing platform and one or more container aligning linear rails. The container aligning linear rails for aligning, on or above the landing platform and a hold of an aerial vehicle placed in front of one of multiple conveyor belts. One or more package extracting tools adapted to push or pull the package out of the aligned hold into a container aligned with one of the multiple conveyor belts. The multiple rail arrangements each adapted to convey the container to one of the multiple building windows from one of the multiple conveyors.

A charging system for mitigating charging failure for an electric aircraft, the system comprising a charger port located on the electric aircraft and configured to mate with a charging connector, a sensor communicatively connected to the charger port and configured to detect a charging datum, and a controller communicatively connected to the charger port and the sensor. The controller is configured to receive charging datum from the sensor, detect a charging failure as a function of a comparison between the charging datum to a pre-set charging datum threshold, and record the charging failure in a database.

Aspects relate to a charger for an electric aircraft with failure monitoring and method for its use. An exemplary charger for an electric aircraft with failure monitoring includes a charging circuit. Included within the charging circuit is a connector configured to mate with an electric aircraft port of an electric aircraft and at least a current conductor configured to conduct a current. At least a conductor comprises a direct current conductor configured to conduct a direct current. A charger may include a control circuit configured to command the charging circuit of an electric aircraft as a function of charging datum. A charger may also include a failure monitor circuit, the failure monitor circuit configured to initiate a failure mitigation procedure as a function of a failure of the charging circuit.

Aspects relate to a charging port of an electric aircraft and methods of use terminating a charging connection between a charger and the electric aircraft. A charging port includes a controller that is configured to receive a control signal from a remote device and terminate the charging connection in response to the control signal.

A system for regulating charging of an electric aircraft includes a charging connector and a controller communicatively connected to the charging connector. The charging connector includes a housing, at least a conductor, and at least a control signal conductor. The housing is configured to mate with an electric aircraft port of an electric aircraft. The at least a conductor is configured to conduct a current. The at least a control signal conductor is configured to conduct a control signal. The controller is configured to receive a voltage datum from the electric aircraft, and regulate a charging voltage, as a function of the voltage datum, to the electric aircraft. Regulation of the charging voltage includes charging at least a battery of the electric aircraft in a plurality of phases including a first charging phase at a constant current and a second charging phase at a constant voltage.

A system for a connector for charging an electric aircraft, wherein the system comprises a charging port located on an electric aircraft, wherein the charging port is configured to mate with a charger connector, receive at least an electrical current from current conductor, and detect a detection datum using at least a sensor. The system also includes a controller communicatively connected to the charging port, wherein the controller is configured to receive the detection datum from the at least a sensor and stop flow of the electrical current as a function of the detection datum.

A cell site with a landing zone for an Unmanned Aerial Vehicle (UAV) includes a cell tower including cell site components for wireless service; a cabinet or shelter with equipment for the wireless service; and one or more landing zones defined at the cell site for the UAV with associated structure for each of the one or more landing zones, equipment for one or more purposes associated with the UAV, and access privileges to the cell site for personnel associated with the UAV, wherein the one or more landing zones are located on one or more of the cell tower, the cabinet or shelter, and surrounding geography around the cell tower.

A system and method for a recharging station including a landing pad, a rechargeable component coupled to the landing pad, a power delivery unit configured to deliver powerfrom a power supply unit or power storage unit to the recharging component, and a support component coupled to the bottom of the landing pad.

Systems, methods, and other embodiments described herein relate to charging a battery of an electric vehicle while the electric vehicle is hovering. In one embodiment, a method includes, responsive to determining that an electric vehicle does not include a receiver pad, inserting the receiver pad into the electric vehicle that is hovering in the air at a charging station. The method includes determining a space above a transmitter pad for the electric vehicle to hover based, at least in part, on a location and a size of the transmitter pad. The method includes charging a battery to a threshold value through the receiver pad.