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.

An assembly and inspection cart for precision equipment includes a frame that has three support portions to support the precision equipment at three points, air float devices attached to the frame at three positions, a rubber roller and a motor that are provided so as to be freely lifted and lowered with respect to the frame, and an air cylinder that lifts and lowers the rubber roller. The air float device floats the frame together with the precision equipment and forms an air layer between the frame and a floor surface. The rubber roller is arranged at a center of the three air float devices and is configured so as to press against the floor with a predetermined force when lowered by the air cylinder in a state where the frame is floated.

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.

A ground effect craft having a ground effect wing, a plurality of sponsons, and a control system is disclosed. The ground effect wing may include a fore ground effect wing and an aft ground effect wing. The ground effect wing may generate a stabilizing moment on at least one sponson to stabilize the ground effect craft. The plurality of sponsons may be dynamically coupled to the body. The plurality of sponsons may be dynamically coupled to each other. The dynamic coupling may permit the sponsons to move relatively independent of the body and each other, thereby stabilizing the ground effect craft. The ground effect craft may include a stabilizing wing.

A hovercraft including imaginary longitudinal, transverse and vertical axes; a propulsion system (12), configured to generate airflow; a base (50) and, a skirt (13) wherein the skirt (13) further including air permeable regions (130) and at least two set of outflow nozzles (220); wherein the air permeable regions (130) and the set of outflow nozzles (20, 21) are in fluid communication; wherein each set of nozzles (20, 21) comprises, at least, one outflow nozzle (22), said outflow nozzle (22) including two opposing ends, a first end (221) and a second end (222); the hovercraft further including actuating means (30) suitable to control the opening of at least one end (221 or 222) of the nozzles (22) managing the passage of airflow through the end (221 or 222). The technical features and functionalities described herein are applicable to the field of hovercrafts. More particularly, to controllable outflow nozzles and controlling systems for hovercrafts.

A hovercraft including imaginary longitudinal, transverse and vertical axes; a propulsion system (12), configured to generate airflow; a base (50) and, a skirt (13) wherein the skirt (13) further including air permeable regions (130) and at least two set of outflow nozzles (220); wherein the air permeable regions (130) and the set of outflow nozzles (20, 21) are in fluid communication; wherein each set of nozzles (20, 21) comprises, at least, one outflow nozzle (22), said outflow nozzle (22) including two opposing ends, a first end (221) and a second end (222); the hovercraft further including actuating means (30) suitable to control the opening of at least one end (221 or 222) of the nozzles (22) managing the passage of airflow through the end (221 or 222). The technical features and functionalities described herein are applicable to the field of hovercrafts. More particularly, to controllable outflow nozzles and controlling systems for hovercrafts.

A pneumatic boat is provided. The pneumatic boat includes a floating body which is suitable for floating on a water surface and a pneumatic propulsion device arranged on the floating body, wherein the pneumatic propulsion device is suitable for forming airflow to generate a propulsive force, so as to push the floating body to move. Technical solutions of the present invention have a higher flexibility.

A pneumatic boat is provided. The pneumatic boat includes a floating body which is suitable for floating on a water surface and a pneumatic propulsion device arranged on the floating body, wherein the pneumatic propulsion device is suitable for forming airflow to generate a propulsive force, so as to push the floating body to move. Technical solutions of the present invention have a higher flexibility.