The invention relates to a control system for an air cushion vehicle (400) for the purpose of improving maneuverability of the air cushion vehicle. The system includes four propeller towers (401-404), propellers installed at the propeller towers, and mounting seats for mounting the propeller towers to the air cushion vehicle. In the system, an edge portion (442) located closest to a side wall N of the air cushion vehicle in the mounting seat is located closer to the ground than an opposite edge portion (446) in relation to a pivot point in the mounting seat, providing a tilt (450) of the propeller in response to rotation of the mounting seat at the pivot point, and in response to the rotation of the mounting seat, the propeller tower directs an air flow (452) produced with the propeller over the side wall of the air cushion vehicle and, due to the tilt of the propeller, partly downwardly relative to a horizontal plane defined by the ground, the air flow exerting a force (462) that lifts the side wall of the air cushion vehicle upwardly from the ground.

The invention relates to a control system for an air cushion vehicle (400) for the purpose of improving maneuverability of the air cushion vehicle. The system includes four propeller towers (401-404), propellers installed at the propeller towers, and mounting seats for mounting the propeller towers to the air cushion vehicle. In the system, an edge portion (442) located closest to a side wall N of the air cushion vehicle in the mounting seat is located closer to the ground than an opposite edge portion (446) in relation to a pivot point in the mounting seat, providing a tilt (450) of the propeller in response to rotation of the mounting seat at the pivot point, and in response to the rotation of the mounting seat, the propeller tower directs an air flow (452) produced with the propeller over the side wall of the air cushion vehicle and, due to the tilt of the propeller, partly downwardly relative to a horizontal plane defined by the ground, the air flow exerting a force (462) that lifts the side wall of the air cushion vehicle upwardly from the ground.

The purpose of the present invention is to provide a moving object comprising a configuration suitable for miniaturization in a view from at least one direction, and to provide a method for using the same. Provided is a moving object comprising: two or more rotors positioned at the front side and at the rear side in the traveling direction; and a driving device that drives the two or more rotors and rotates at least two of the two or more rotors in mutually different directions.

The purpose of the present invention is to provide a moving object comprising a configuration suitable for miniaturization in a view from at least one direction, and to provide a method for using the same. Provided is a moving object comprising: two or more rotors positioned at the front side and at the rear side in the traveling direction; and a driving device that drives the two or more rotors and rotates at least two of the two or more rotors in mutually different directions.

A modular wing in ground effect vehicle has a fuselage which receives interchangeable cockpit and component modules and may accept a variety of snap-on wing styles and control surfaces for various flying conditions and pilot skill levels. When depleted or due for repairs, modules containing stored energy components or machinery subject to wear or periodic maintenance may be exchanged for fresh units so that a vehicle requiring such an exchange may be returned to service quickly and conveniently.

The invention relates to a control system for an air cushion vehicle (400) for the purpose of improving maneuverability of the air cushion vehicle. The system includes four propeller towers (401-404), propellers installed at the propeller towers, and mounting seats for mounting the propeller towers to the air cushion vehicle. In the system, an edge portion (442) located closest to a side wall N of the air cushion vehicle in the mounting seat is located closer to the ground than an opposite edge portion (446) in relation to a pivot point in the mounting seat, providing a tilt (450) of the propeller in response to rotation of the mounting seat at the pivot point, and in response to the rotation of the mounting seat, the propeller tower directs an air flow (452) produced with the propeller over the side wall of the air cushion vehicle and, due to the tilt of the propeller, partly downwardly relative to a horizontal plane defined by the ground, the air flow exerting a force (462) that lifts the side wall of the air cushion vehicle upwardly from the ground.

The invention relates to a control system for an air cushion vehicle (400) for the purpose of improving maneuverability of the air cushion vehicle. The system includes four propeller towers (401-404), propellers installed at the propeller towers, and mounting seats for mounting the propeller towers to the air cushion vehicle. In the system, an edge portion (442) located closest to a side wall N of the air cushion vehicle in the mounting seat is located closer to the ground than an opposite edge portion (446) in relation to a pivot point in the mounting seat, providing a tilt (450) of the propeller in response to rotation of the mounting seat at the pivot point, and in response to the rotation of the mounting seat, the propeller tower directs an air flow (452) produced with the propeller over the side wall of the air cushion vehicle and, due to the tilt of the propeller, partly downwardly relative to a horizontal plane defined by the ground, the air flow exerting a force (462) that lifts the side wall of the air cushion vehicle upwardly from the ground.

The present invention relates to flying scooter comprising a base made of fibreglass, 20 fans with 20 motors connected to a power system with components comprising capacitors, batteries, photovoltaic solar cells, an oxygen generator, a regulator, electronic sensors, and electronic chips. The scooter has a circular front part that includes a display that gives operational levels of the components, and the base has a cavity for the passenger's legs, and a rubber strap for securing the passenger. Manual controls are provided as well as a grip for the controls. The controls are connected to the sensors and electronic chips wirelessly.

The present invention relates to flying scooter comprising a base made of fibreglass, 20 fans with 20 motors connected to a power system with components comprising capacitors, batteries, photovoltaic solar cells, an oxygen generator, a regulator, electronic sensors, and electronic chips. The scooter has a circular front part that includes a display that gives operational levels of the components, and the base has a cavity for the passenger's legs, and a rubber strap for securing the passenger. Manual controls are provided as well as a grip for the controls. The controls are connected to the sensors and electronic chips wirelessly.

An amphibious air cushion vehicle includes an air cushion supported hull configured for travel on water and smooth land; a deck supported by the hull; and a dual-rail cargo system having tracks arranged longitudinally on along the hull cargo deck from an aft end. The tracks include (1) guide rails and rollers providing for guided sliding movement of palletized cargo along the tracks, and (2) locks for locking pallets in position during transport, The track is configured at the aft end for an unloading operation in which the locks are disengaged and the palletized cargo slides off the aft end onto underlying land as the vehicle is moving forward thereon. The track may be the one track of a single-track variant, or one of a pair of tracks in a two-track variant.