A secure terminal for the aerial transport of passengers whose technical and operational infrastructure makes it possible to ensure the physical security of the building, of the aircraft, of the goods, of the passengers and of the flight, technical and administrative personnel and the confidentiality of the passengers and of their goods, noteworthy in that it comprises at least one building having a globally V-shaped horizontal section and comprising two branches extending from a mid-zone, constituting parking hangars for aircraft and determining between them an uncovered central zone.

An apparatus (1) for changing a power source of a drone, the apparatus (1) comprises an adaptor (2) for securing a power source (3) to a drone and comprising a first energy connection for supplying energy from the power source (3) and a second energy connection for supplying energy to a drone, wherein one of the first and second energy connections comprises a pair of energy links (20, 21) which are movable between a first position (FIG. 5) to facilitate energy supply and secure the power source (3) to the drone and a second position (FIG. 4) to interrupt energy supply and enable the power source (3) to be removed from the drone.

A hybrid aerial vehicle (HAV) comprising: a fuselage of the HAV; a first mechanism within the fuselage for accepting a plurality of wings of the HAV, the first mechanism allowing coordinated contraction of the plurality of wings essentially into the fuselage such that tips of the wings are position in proximity of the fuselage and coordinated extension of the wings such that tips of each wing are positioned away from the fuselage; a first wing extending from the port side of the fuselage and connected to the first mechanism; a second wing extending from the starboard side of the fuselage and connected to the first mechanism; a second mechanism placed within the fuselage in proximity to its front end, the second mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain; a first set of propellers affixed at the port side of the fuselage to the second mechanism; a second set of propellers affixed at the starboard side of the fuselage to the second mechanism; a third mechanism placed within the fuselage in proximity to its rear end, the third mechanism allowing motion of propellers of the HAV affixed there to between a first plain and a second plain, and further placing the propellers affixed thereto to be at a vertical displacement with respect to the propellers affixed to the second mechanism; a third set of propellers affixed at the port side of the fuselage to the third mechanism; and a fourth set of propellers affixed at the starboard side of the fuselage to the third mechanism.

A landing platform control system and methods used for refuel or recharge purposes by a fleet of unmanned aerial vehicles (UAVs) performing aerial surveys are disclosed. The system can include a plurality of landing platforms positioned at predetermined locations within the area of interest, each landing platform comprising a mount connecting the landing platform to a surface, a mount component for coupling a floor, a floor to support a UAV while docked at the landing platform, a cover enclosing the floor; a battery charger; and a communications interface. The floor can be rotated to clear any accumulated debris. The cover can be coupled to the floor. The cover can alternate between open and closed position via rotating along the same axis as the floor.

A landing platform control system and methods used for refuel or recharge purposes by a fleet of unmanned aerial vehicles (UAVs) performing aerial surveys are disclosed. The system can include a plurality of landing platforms positioned at predetermined locations within the area of interest, each landing platform comprising a mount connecting the landing platform to a surface, a mount component for coupling a floor, a floor to support a UAV while docked at the landing platform, a cover enclosing the floor; a battery charger; and a communications interface. The floor can be rotated to clear any accumulated debris. The cover can be coupled to the floor. The cover can alternate between open and closed position via rotating along the same axis as the floor.

An aircraft tug apparatus for tugging an aircraft by an aircraft tire includes a turntable on a main base portion of the tug, capable of rotational movement relative to the main base portion. A tire cradle assembly on the turntable releasably holds the aircraft tire, and a latch mechanism holds the tire cradle assembly in a position that confines the aircraft tire. A pivoting arm coupled to the main base portion extends under the turntable. The pivoting arm includes a first plunger and a second plunger extending therefrom, with the first plunger coupled to the pivoting arm using a spring assembly allowing it to move up and down relative to the pivoting arm. The spring assembly is configured such that the pivoting arm may move the second plunger to engage the latch mechanism while the first plunger is impinged by the turntable.

An aircraft tug apparatus for tugging an aircraft by an aircraft tire includes a turntable on a main base portion of the tug, capable of rotational movement relative to the main base portion. A tire cradle assembly on the turntable releasably holds the aircraft tire, and a latch mechanism holds the tire cradle assembly in a position that confines the aircraft tire. A pivoting arm coupled to the main base portion extends under the turntable. The pivoting arm includes a first plunger and a second plunger extending therefrom, with the first plunger coupled to the pivoting arm using a spring assembly allowing it to move up and down relative to the pivoting arm. The spring assembly is configured such that the pivoting arm may move the second plunger to engage the latch mechanism while the first plunger is impinged by the turntable.

A docking station for an aircraft includes a base portion and an alignment system disposed on the base portion configured to orient the aircraft relative to the base portion. The alignment system can include a plurality of outer protrusions extending away from the base portion in a vertical direction.

A docking station for an aircraft includes a base portion and an alignment system disposed on the base portion configured to orient the aircraft relative to the base portion. The alignment system can include a plurality of outer protrusions extending away from the base portion in a vertical direction.

An apparatus for storing airplanes includes a first airplane parking floor at a first elevation, a second airplane floor at a second elevation, and an elevator. The first airplane parking floor defines a vacant region within a notional circle circumscribing the first airplane parking floor and defining a notional circumcenter. The first floor is rotatable about the circumcenter for selective angular alignment of one of several first airplane parking floor regions or the vacant region with a fixed sector of the circle. The second airplane parking floor is rotatable, at the second elevation, about the circumcenter for selective angular alignment of one of several second airplane parking floor region with the vacant region. When so aligned, the second airplane parking floor region may be vertically translated by the elevator between the second elevation and the vacant region at the first elevation.