A modular aircraft includes a plurality of structural elements. The structural elements include a pod module assembly, a wing assembly, and a chassis module. The pod module assembly is configured to be selectively attached to and detached from at least one of the chassis module and the wing module when the aircraft is not in flight. The pod module assembly is configured to transport at least one of a passenger and cargo.

The present disclosure provides a modular and scalable platform for the development of land and/or flying multi-purpose manned and unmanned vehicles. The platform including a plurality of parts is provided for structural support, wherein the parts include beams, joints and panels interconnected for forming the platform, a plurality of components is connected to the platform for providing propulsion, a plurality of equipment is connected to the platform for generating mobility in air and land, and navigating the vehicle, wherein the equipment include wings, wheels, landing gears, telemetry equipment, sensors, receivers, transmitters, battery systems, fuel tank, onboard computers, servos, actuators, engines, avionics, direction controls and a case provided for enclosing the platform.

The invention discloses a vertical take-off and landing triphibian flight vehicle that can travel on land, water and air. These three traveling modes are realized by changing the position of the propeller module. The vehicle has retractable and foldable wings and has the accommodate space in the vehicle body to store the wings. When the vehicle is in land mode, the wings are stowed in the accommodate space to reduce the size of the vehicle and the air resistance. When the vehicle is in flight mode, the wings can be extended out of the accommodate space through the control system, so that the vehicle can use the wings to obtain aerodynamic force to counter gravity, thereby reducing the energy consumption required for countering gravity during flight and increasing the flight mileage.

The invention discloses a vertical take-off and landing triphibian flight vehicle that can travel on land, water and air. These three traveling modes are realized by changing the position of the propeller module. The vehicle has retractable and foldable wings and has the accommodate space in the vehicle body to store the wings. When the vehicle is in land mode, the wings are stowed in the accommodate space to reduce the size of the vehicle and the air resistance. When the vehicle is in flight mode, the wings can be extended out of the accommodate space through the control system, so that the vehicle can use the wings to obtain aerodynamic force to counter gravity, thereby reducing the energy consumption required for countering gravity during flight and increasing the flight mileage.

An air, sea and underwater tilt tri-rotor UAV capable of performing vertical take-off and landing. By the method for controlling a submerged floating device and a tilt tri-rotor device, the UAV is switched among the vertical take-off and landing mode, fixed wing mode, water surface sailing mode and underwater submerging mode.

Disclosed herein is a schematic of a transportation system for hybrid vehicles, in accordance with some embodiments. Accordingly, the transportation system may include pillars and a raised pathway. Further, the pillars configured to be vertically mounted on the ground. Further, a first pillar of the pillars may include a first lower portion and a first upper portion. Further, a second pillar of the pillars may include a second lower portion and a second upper portion. Further, the raised pathway supported by the pillars. Further, a raised pathway of the raised pathway may include a first end and a second end. Further, the first end may be supported by the first upper portion of the first pillar. Further, the second end may be supported by the second upper portion of the second pillar. Further, the raised pathway may include a raised transportation surface configured to facilitate transportation of a hybrid vehicle.

A rotor includes a rotor axis, two elongate blades, a hub on the rotor axis, and a rotational drive system on the rotor axis. The hub supports the blades for pivotation relative thereto, including folding one blade over the hub between radial opposition with the other blade about the rotor axis and alongside the other blade. The rotational drive system supports the blades on the hub for rotation about the rotor axis, and supports the blades on the hub for teetering.

A rotor includes a rotor axis, two elongate blades, a hub on the rotor axis, and a rotational drive system on the rotor axis. The hub supports the blades for pivotation relative thereto, including folding one blade over the hub between radial opposition with the other blade about the rotor axis and alongside the other blade. The rotational drive system supports the blades on the hub for rotation about the rotor axis, and supports the blades on the hub for teetering.

A mobility vehicle hub configured to function as a terminal for an air mobility vehicle, a ground mobility vehicle, or a water mobility vehicle, includes a plurality of layers through a combination of: a water layer connected to the surface of water and having an entrance for a water mobility vehicle; a port layer having a take-off and landing pad for an air mobility vehicle; or a ground layer configured to be connected to a ground and having an entrance for a ground mobility vehicle, wherein an elevation passage is provided between the layers, the elevation passage has an internal space extending in an up-down direction of the mobility vehicle hub, the internal space is connected to each of the water, port and ground layers, and the air mobility vehicle, the ground mobility vehicle, or the water mobility vehicle is lifted or lowered through the internal space.

A mobility vehicle hub configured to function as a terminal for an air mobility vehicle, a ground mobility vehicle, or a water mobility vehicle, includes a plurality of layers through a combination of: a water layer connected to the surface of water and having an entrance for a water mobility vehicle; a port layer having a take-off and landing pad for an air mobility vehicle; or a ground layer configured to be connected to a ground and having an entrance for a ground mobility vehicle, wherein an elevation passage is provided between the layers, the elevation passage has an internal space extending in an up-down direction of the mobility vehicle hub, the internal space is connected to each of the water, port and ground layers, and the air mobility vehicle, the ground mobility vehicle, or the water mobility vehicle is lifted or lowered through the internal space.