| Document |
Document Title |
|
WO/2024/054193A1 |
The present invention particularly relates to a hydrogen-powered, scalable, multi-purpose, hybrid general amphibious platform (1) which can instantly transform itself into an air-skirted (7) or caterpillar-tracked (10) structure on deman...
|
|
WO/2024/050649A1 |
A cargo or passenger vehicle floats on a cushion of air, which is generated initially by electrically driven compressors, and having a forward propulsion engine such as a linear induction motor or jet engine. As forward velocity increase...
|
|
WO/2024/044199A1 |
A measuring device, method of measuring, and transport vessel including the measuring device measuring the ground effect region for the vessel in real time and controlling the transport vessel, e.g., a Wing In Ground Effect (WIG) vessel,...
|
|
WO/2024/035885A1 |
A craft comprises at least one hull, at least one wing configured to generate upwards aero lift as air flows past the at least one wing to facilitate wing-borne flight of the craft, at least one retractable hydrofoil configured to genera...
|
|
WO/2024/008982A1 |
The invention relates to a medium-high speed seaplane that uses a system that allows it to travel on land, on water and in the air. The seaplane is formed by one or more parallel hulls or half hulls (1) comprising on the underside thereo...
|
|
WO/2023/195859A1 |
An air supported vessel comprising a basically V-shaped hull with a starboard keel part and a port keel part and with a V-shaped bow, which includes an outer bow support surface, where the basically V-shaped hull has at least one air cus...
|
|
WO/2023/180449A1 |
The invention relates to a vehicle, which can be used either as an aircraft or ground effect vehicle or as an aircraft and ground effect vehicle, comprising a fuselage (4) and at least two front wings (2), wherein the fuselage (4), when ...
|
|
WO/2023/156481A1 |
The invention relates to a rail vehicle (100), in particular a road-rail vehicle (100), comprising a chassis (101), which is designed for a track/rail/line guiding process and on which at least two axles with two respective wheels (110) ...
|
|
WO/2023/118873A1 |
A vehicle (1) for capturing a falling object comprises a plurality of air cushion units (100), wherein each of the air cushion units is configured to generate a propulsive force to drive the vehicle and a lift force to elevate the vehicl...
|
|
WO/2023/092645A1 |
A hovertrain and a track, drawing on the principle of hovercraft suspension; a rectangular space, which is slightly shorter and narrower than an upper carriage (3), is enclosed at the bottom of the upper carriage (3) by a rubber plate el...
|
|
WO/2023/087038A1 |
According to the invention, a ground effect vehicle is provided, comprising a first hull (1) and a second hull (2) which are arranged substantially parallel to each other, and a leading wing (4) and a trailing wing (5), the ends of which...
|
|
WO/2023/091202A1 |
A craft comprises a hull, a wing, a hydrofoil, and a control system. The wing is configured to generate upwards aero lift as air flows past the wing to facilitate wing-borne flight of the craft. The hydrofoil is configured to generate up...
|
|
WO/2023/277720A1 |
A nuclear-powered ground-effect aircraft carrier is capable of travelling above the surface of water at a maximum speed of up to 550-600 km/h and has a twin-hulled catamaran design. Disposed between the hulls is a large wing, the aircraf...
|
|
WO/2022/250545A1 |
A flap (22) for an air supported vessel with a hull is disclosed, the hull being provided with an exterior hull recess at the bottom of the hull for an air cushion. The hull recess extends in a longitudinal direction of the hull, and is ...
|
|
WO/2022/189685A1 |
Disclosed is a ground-effect amphibious hovercraft vehicle, characterised in that it comprises a system of retractable wings (8), which are retracted (parking mode) by retracting arms (17a and 17b) of both wings by means of a head (19). ...
|
|
WO/2022/170733A1 |
A drag reduction device (2), comprising a first part (21) and a second part (22). The first part is connected to the second part, and the second part is detachably connected to a body (1); the first part is made of a flexible material, a...
|
|
WO/2022/173948A1 |
A wing-in-ground effect vehicle (100) includes (i) a main wing (104) having main wing control surfaces (118, 120); (ii) a tail (106) having tail control surfaces (126); (iii) a blown-wing propulsion system comprising an array of electric...
|
|
WO/2022/086321A1 |
A ground effect flight vehicle comprising, a fuselage (1), a wing assembly (4, 5), an engine assembly comprising one or more engines or engine sets (6, 7, 8), and a hull (2) for enabling floatation of the vehicle; wherein the wing assemb...
|
|
WO/2022/035946A1 |
Techniques involve an air flow assembly to provide pressurized air, e.g., for use by an air cushion vehicle (ACV) or other craft. The air flow assembly includes a volute having a central chamber, a lift duct, and a thruster duct. The air...
|
|
WO/2022/017629A1 |
The invention relates to an engine (2) for an aircraft (1), comprising a ring-shaped vortex guide element (3) which has, in a sectional view, an air inlet opening (6) which is located centrally in relation to a longitudinal center axis (...
|
|
WO/2021/137368A1 |
An air-cushion vehicle having a stealth function according to the present invention comprises: a hull part in which a cabin is formed; a power generation unit provided in the hull part and supplying a buoyant force by which the hull part...
|
|
WO/2021/089386A1 |
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 generat...
|
|
WO/2021/044143A1 |
The present disclosure relates to a control system for a vehicle, comprising: at least one compressor arranged to generate compressed fluid having a massflow rate; at least one fluidic control effector in fluidic communication with the a...
|
|
WO/2020/247939A9 |
A lightweight gearbox control mechanism for air cushion vehicles provides change in direction of rotation for the vehicle lift fan and allows the gearbox to be used at port or starboard vehicle locations without the use of specialty tools.
|
|
WO/2021/028368A1 |
The present invention relates to method of spraying a field with an unmanned aerial vehicle (UAV). The method comprises: flying an UAV over a crop within a field and spraying the crop with a liquid spray, wherein the UAV comprises a wing...
|
|
WO/2021/026072A1 |
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 c...
|
|
WO/2021/020999A1 |
The invention relates to wing-in-ground-effect vehicles having an aerodynamic "composite wing" configuration. The technical result is an increase in safety by providing for the static, non-oscillatory and oscillatory stability of a wing-...
|
|
WO/2021/009507A1 |
A landing apparatus for an airship or hybrid air vehicle. The landing apparatus comprises a hollow, non-toroidal, flexible enclosure (103), having a substantially vertical axis (104), and a substantially circular cross-section centred on...
|
|
WO/2020/157052A1 |
The invention relates to an aircraft (1). Said aircraft is characterized by a wing (2) which, viewed in section, is delimited on one side by a first profiled surface (4), which is at the bottom when the aircraft (1) is operated as intend...
|
|
WO/2020/128877A1 |
The subject of the invention is stabilisation and levitation mechanism for a dedicated vehicle (1), taking into account interoperability with existing transport systems in the vicinity of switches and routes of conventional vehicles, con...
|
|
WO/2020/098529A1 |
A water, land and air multipurpose hovercraft, comprising a hull (1). At least one first duct (2) is provided on the hull (1); the first duct (2) penetrates through the hull (1) and is perpendicular to the hull (1); a first rotor (3) is ...
|
|
WO/2020/070521A1 |
Disclosed is a transportation device (1) for transporting a load over a surface, for example, formed from water or earth. The transportation device comprises propulsion element(s) (5, 6) that generate an aerodynamic lift force and a driv...
|
|
WO/2019/215839A1 |
The purpose of the present invention is to provide a moving object comprising a configuration suitable for compactization in a view from at least one direction, and to provide a method for using the same. Provided is a moving object comp...
|
|
WO/2019/209804A1 |
A ground-based vectored thrust system for landings and take-off of vertical take-off and landing (VTOL) aircraft. The vectored thrust system provides an upward thrust on the VTOL aircraft when in proximity to the pad. The upward thrust c...
|
|
WO/2019/184707A1 |
A paddle wheel propelled hovercraft, comprising a hull (1), a power system, a hover system, and a propelling system. Said hover system comprises a hover fan (10) and an apron (3). Said propelling system comprises a pair of paddle wheel p...
|
|
WO/2019/148352A1 |
A hovercraft, comprising a ship body (1) and a propeller; a first side wall (3a) and a second side wall (3b) respectively located at two sides of the ship body (1) are provided the bottom of the ship body (1), and the first side wall (3a...
|
|
WO/2019/116057A1 |
The invention relates to an air deflector system that can be installed in motor vehicles through minor conversion of the vehicle. Starting from the front of the vehicle, the first component of the air deflector system is a wind grille (1...
|
|
WO/2019/090118A1 |
A wheel, a magnet-wheel system and a method including a wheel for a transport vehicle movable along a guideway in a transportation system. The transportation system includes a conductive surface arranged substantially parallel to the gui...
|
|
WO/2019/084639A1 |
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...
|
|
WO/2018/197749A1 |
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 propelle...
|
|
WO/2018/171419A1 |
An air bottom skirt sleeve for boats, comprising: a hull (4), an air pump (1), an air pipe (2), an airbag skirt (5) and a sleeve bottom (6); the airbag skirt (5) is arranged around the sleeve bottom (6), and the sleeve bottom (6) is fixe...
|
|
WO/2018/098323A1 |
A modular structure, configured to be connectable with a plurality of modular structures to form an enclosed transportation path, each modular structure including a bottom element structured and arranged to provide a track support surfac...
|
|
WO/2018/004389A1 |
The utility model relates to transport, and particularly to amphibious wheeled propulsors for use in water transport and in air-cushion vehicles. A wheel propulsor comprises a cylindrical rim, and blades in the form of radially-directed ...
|
|
WO/2017/194870A1 |
According to the invention relates mainly to a vehicle supported by air that is economical in terms of energy, low in bulk, and stable. According to the invention, the vehicle comprises what is referred to as a "support" sole (100), arra...
|
|
WO/2017/196978A1 |
A friction-braking apparatus for a transportation system, having at least one caliper, at least one piston structured and arranged to move the at least one caliper; and at least one brake pad arranged on the at least one caliper. The at ...
|
|
WO/2017/130091A1 |
The performance of a passive-levitation vehicle is improved for moving over a path, wherein the vehicle has a levitation skid slidable on the path and capable of developing a levitation force to support a compartment at a certain distanc...
|
|
WO/2017/129953A1 |
Wing-in-ground effect vehicle (1) having a lift system with a pressure vessel (2) and a set of nozzles (3-14). The lift system allows the wing-in-ground effect vehicle to take off. The pressure vessel holds a fluid, such as air, under pr...
|
|
WO/2017/063205A1 |
A hovercraft capable of performing vector propulsion by using a single-ducted fan (2) comprises a hull (1) and a single-ducted fan disposed on the hull. The single-ducted fan comprises a barrel-shaped housing (21) and a paddle assembly (...
|
|
WO/2017/046562A1 |
An equipment handling system (1) comprising a pallet (2) provided with air casters (3), a shipping container (4) with a floor (5) arranged to support the air casters (3), and a support structure (6) with a surface (7) arranged to support...
|
|
WO/2017/042757A1 |
The present invention consists of a hovercraft vehicle which autonomously performs several tasks. These tasks include, among others, following a route automatically, inspecting a terrain which may include plants, land or water, depositin...
|
