A drone delivery system provides to send or to receive the package conveniently and safely without going out of the building by using the platform installed at the vicinity of the window. The drone delivery system includes the drone having a first docking device, a standard box having a second docking device corresponding to the first docking device and a third docking device and a platform having a fourth docking device corresponding to the third docking device.

The disclosure relates to a lighting apparatus of a helicopter deck, which is meant especially while being installed in connection with an identification marking, such as an H, triangle, cross figure or the like, and/or a touchdown and positioning mark ring on a landing and takeoff area of the helicopter deck for illuminating the safety marking/markings in question in order to make more efficient observing thereof from the air. The lighting apparatus includes of light units formed of one or more lamps and being operable by power supply transmitted from a power source in connection with the helicopter deck, wherein the light units are coupled essentially immovably in connection with an upper surface of the helicopter deck. Light units of the lighting apparatus are coupled in connection with the upper surface of the helicopter deck by means of a horizontal fastening arrangement in order to keep the light units in place by means of fastening means, being in connection therewith in a manner transmitting power essentially in a direction parallel with a plane of the helicopter deck.

The disclosure relates to a lighting apparatus of a helicopter deck, which is meant especially while being installed in connection with an identification marking, such as an H, triangle, cross figure or the like, and/or a touchdown and positioning mark ring on a landing and takeoff area of the helicopter deck for illuminating the safety marking/markings in question in order to make more efficient observing thereof from the air. The lighting apparatus includes of light units formed of one or more lamps and being operable by power supply transmitted from a power source in connection with the helicopter deck, wherein the light units are coupled essentially immovably in connection with an upper surface of the helicopter deck. Light units of the lighting apparatus are coupled in connection with the upper surface of the helicopter deck by means of a horizontal fastening arrangement in order to keep the light units in place by means of fastening means, being in connection therewith in a manner transmitting power essentially in a direction parallel with a plane of the helicopter deck.

A port for electric vehicles includes an off-loading zone for off-loading one or more passengers from an electric vehicle; a loading zone for loading one or more passengers onto the electric vehicle; and a charging zone for charging the electric vehicle while the electric vehicle is moving from the off-loading zone to the loading zone.

A port for electric vehicles includes an off-loading zone for off-loading one or more passengers from an electric vehicle; a loading zone for loading one or more passengers onto the electric vehicle; and a charging zone for charging the electric vehicle while the electric vehicle is moving from the off-loading zone to the loading zone.

Described are systems and methods for adjusting a takeoff platform for a vertical takeoff and landing (VTOL) aerial vehicle. The described systems and methods allow a VTOL aerial vehicle to be oriented prior to takeoff to reduce the effects that a VTOL aerial vehicle may experience due to weather conditions at takeoff. In view of the aerodynamic characteristics of a VTOL aerial vehicle and certain weather conditions, a heading, pitch, and/or roll of the VTOL can be provided to counteract the effects the VTOL may experience from the weather conditions at takeoff.

Described are systems and methods for adjusting a takeoff platform for a vertical takeoff and landing (VTOL) aerial vehicle. The described systems and methods allow a VTOL aerial vehicle to be oriented prior to takeoff to reduce the effects that a VTOL aerial vehicle may experience due to weather conditions at takeoff. In view of the aerodynamic characteristics of a VTOL aerial vehicle and certain weather conditions, a heading, pitch, and/or roll of the VTOL can be provided to counteract the effects the VTOL may experience from the weather conditions at takeoff.

A helicopter take-off and landing pad (helipad) includes a drain conduit embedded within a surface, a bed of crushed aggregate within a portion of the surface graded to be inclined toward the drain conduit, and a plurality of pavers supported by the aggregate bed and defining a substantially level top surface to serve as a landing surface for a helicopter. The plurality of pavers are permeable to liquid on the top surface to communicate the liquid to the aggregate bed. A pump connected to the drain conduit is operable to discharge liquid directed from the aggregate bed through the drain conduit to a water separator that is operable to separate water from other liquid components of the discharged liquid. At least one collection tank is fluidly connected to the water separator to receive the other liquid components discharged by the water separator.

An air-taxi pod system floats on a lake, river, sea, etc. and has a spoke connected between a base and an air pod. The pod is configured as a landing region for air taxi within larger metropolitan cities. Each of the spoke, base, and pod use a hull section to provide the buoyancy necessary for each of these components to float. In some versions, two or more, such as six spokes sit around a base connected to the base with connections that can withstand heavy storms. An air pod or separately an air-ship pod connect to some of the spokes at second ends of the spokes with a similar connection. The system can also have terminals or terminal buildings to facilitate travel or commuting.

An air-taxi pod system floats on a lake, river, sea, etc. and has a spoke connected between a base and an air pod. The pod is configured as a landing region for air taxi within larger metropolitan cities. Each of the spoke, base, and pod use a hull section to provide the buoyancy necessary for each of these components to float. In some versions, two or more, such as six spokes sit around a base connected to the base with connections that can withstand heavy storms. An air pod or separately an air-ship pod connect to some of the spokes at second ends of the spokes with a similar connection. The system can also have terminals or terminal buildings to facilitate travel or commuting.