Abstract: 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.

Abstract: A recharging system for a rechargeable battery (281) of an inverted pendulum type vehicle (1) comprises a stand (86) for holding the vehicle in a substantially upright posture by using a supporting member (91, 96) that engages a prescribed part of the vehicle, a power feed device (95, 152) is provided on the stand, and a power take device (88, 151) provided on the vehicle. The power take device is positioned so as to couple with the power feed device when the prescribed part of the vehicle is engaged by the supporting member of the stand. The stand allows the vehicle to be placed in an upright posture simply leaning the vehicle against a part of the supporting member, and the electric connection between the rechargeable battery of the vehicle and the power source can be established at the same time without requiring any extra effort.

Abstract: An air cushion platform for carrying a manipulator arm, having a base, on the bottom side of which an air cushion system is attached for lifting the base from a standing position into a moving position above a bottom. At least one actuator device is mounted on the base, which actuator device is optionally in constant contact with the bottom in order to move the base at the bottom. A controller is connected to the air cushion system and the at least one actuator device in order to actuate the actuator device only if the air cushion platform is located in a moving position. A moveable robot is provided, particularly for the controlled guiding of a tool. The moveable robot has an air cushion platform, a foundation mounted on the air cushion platform and moveably supported thereby, and a manipulator arm having one end section that is attached to the foundation and another end that carries a tool.

Abstract: A system and method retracts and lets-out a laterally extending flexible bow seal on an air cushion vehicle having a bow ramp. Attachment loops on the forward outside surface of the bow seal receive a skirt cable. A separate cable routing system is connected to opposite ends of the skirt cable for selectively retracting and letting-out the bow seal. The cable routing systems also include ramp cables connected to the bow ramp to raise or lower the bow ramp. The cable routing systems retract the bow seal with the skirt cable simultaneously as the bow ramp is lowered by letting out the ramp cables, and the cable routing systems let-out the bow seal with the skirt cable simultaneously as the bow ramp is raised by drawing in the ramp cables.

Abstract: Wrapped-cone fingers for use in an air-cushion vehicle (ACV) skirt system are described. Wrapped-cone fingers may include an inner cone that is “wrapped” or generally enclosed by an outer finger. The inner cone may include an inner cone opening through which air may travel. The outer cone may include a back face opening. When inflated, the inner cone blocks the back face opening in the outer finger, allowing for increased air pressure in the outer finger and thus inflating the inner cone and outer finger of the wrapped-cone finger. Wrapped-cone fingers according to the present invention may be lightweight, inexpensive and resistant to scooping and snagging. Embodiments are also directed to ACV skirt systems and methods of manufacturing wrapped-cone fingers for use with an ACV skirt system.

Abstract: A flexible skirt-cell system is provided for a hovercraft having a propulsion system mounted to interface with water and a flexible skirt having an upper flexible panel section and a lower flexible finger section. The panel section extends around the bow, stern and two sides of the hovercraft hull and the finger section extends around the hull below the panel section and is connected to the panel section from a forward-abeam location and forward along the two sides and across the bow. Fans create pressurized air that is fed through air ducts to form a pressurized air cushion that supports the hovercraft. Interconnected flexible cells are connected between the panel and finger sections from the forward-abeam locations rearward to the stern. Additional air ducts pass pressurized air from the fan units to inflate the cells, thereby elevating the stern and raising the propulsion system above the water.

Abstract: A multiple unit surface effect vehicle movable through an aquatic environment is provided including connected units and lift fans. The multiple unit surface effect vehicle may further include a coupling system and/or a plurality of skirt portions connecting one of the connected units with another of the connected units. The multiple unit surface effect vehicle includes the connected units connected to form a continuous movable unit movable in an aquatic environment. Each connected unit includes a forced air containment chamber defined within each of the connected units. The forced air containment chambers of each of the connected units are connected to form a continuous pressurized air cushion. The lift fans force air into the forced air containment chamber to pressurize the continuous pressurized air cushion.

Abstract: Wrapped-cone fingers for use in an air-cushion vehicle (ACV) skirt system are described. Wrapped-cone fingers may include an inner cone that is “wrapped” or generally enclosed by an outer finger. The inner cone may include an inner cone opening through which air may travel. The outer cone may include a back face opening. When inflated, the inner cone blocks the back face opening in the outer finger, allowing for increased air pressure in the outer finger and thus inflating the inner cone and outer finger of the wrapped-cone finger. Wrapped-cone fingers according to the present invention may be lightweight, inexpensive and resistant to scooping and snagging. Embodiments are also directed to ACV skirt systems and methods of manufacturing wrapped-cone fingers for use with an ACV skirt system.

Abstract: In a controlled levitation vehicle that has a levitation apparatus where multiple air pads are connected to the undersurface of a chassis that also doubles as a duct connected to a blower, and where damper valves are connected between the blower and chassis and to the chassis, it is furnished with: a controller (S1, S2) that closes the damper valve between the blower and chassis when starting and that also regulates the frequency of the inverter to the standby frequency that is below the levitation frequency; the controller (S6, S7) also closing the chassis damper valve responsive to an instruction to levitate and also increasing the frequency from a standby frequency to a levitation frequency to cause the vehicle to levitate; and the controller also lowering (S9-S12) the frequency from the levitation frequency to the standby frequency upon an instruction to land and also opening the blower and chassis damper valves to stop the vehicle rapidly.

Abstract: A system for facilitating movement of a shipping container uses a plurality of air bearing pontoons interposed between a shipping container and a h, soft or water surface. Each air bearing pontoon includes an inflatable skirt and its own controllable air supply that allows the skirt to float on a cushion of air above the surface.

Abstract: A self-propelled hovercraft having a body or hull around the periphery of which is a segmented skirt. The segmented skirt of the hovercraft comprises a plurality of bags, one adjacent to another, completely encircling the hovercraft body. Each of the bags has front and side portions and, in one embodiment, at least some of the bags at the forward end of the hovercraft are provided with semi-rigid lower front surfaces constructed of material less flexible than material of other bags and which may be provided with internal cushion devices which support the front semi-rigid material against water surface contact.

Abstract: In a preferred embodiment, a hovercraft motorcycle for travel over a ground surface, comprising: a body portion having a front end, a rear end, a longitudinal centerline extending from the rear end to the front end, and a lower surface spaced above the ground surface; a generally horizontal, continuous, inflatable, resilient tubular member attached to, disposed around, and depending from the lower surface of the body portion having an air inlet port; the generally horizontal, continuous, inflatable, resilient tubular member having an air inlet port; an air plenum chamber defined between the tubular member, the lower surface of the body portion, and the ground surface; an apparatus to supply pressurized air to the air plenum chamber; a front wheel assembly, attached to the front end of the body portion and on the longitudinal centerline of the body portion, having a front wheel mounted thereon; and a rear wheel assembly, attached to the rear end of the body portion and on the longitudinal centerline of the bod

Abstract: An air cushion vehicle has a substantially-endless downward and inward directed rigid primary nozzle supplied with air under pressure for producing an air curtain that creates and confines a central primary air cushion beneath the vehicle which mainly supports it. The vehicle also has at least two substantially-endless downward and inward directed rigid secondary nozzles arranged on generally opposite sides of the primary nozzle and each supplied with air under pressure for producing an air curtain that creates and confines a stabilizing air cushion beneath the vehicle smaller than the primary air cushion. The two stabilizing cushions are preferably of the same size and shape and each smaller than the primary cushion. When the vehicle leans or dips toward one of the stabilizing cushions when travelling over a surface, e.g. land or water, the pressure of that one stabilizing cushion increases and tends to push the vehicle back up to a level position.

Abstract: An end plate is provided for a ram-wing boat having two airfoils (7-8) and (7a-8a), in the form of ailettes, disposed at a distance from each other and in tandem at approximately the same height, which airfoils are connected with each other at their outer ends by flat end plates (1). Each end plate (1) is configured as a hollow body with an essentially trapezoidal cross section, and consists of upper chord (2) and lower chord (3) connected by planking (4 and 5) along the length thereof. To complete the static assemblage, ribs (6) which divide the hollow body into compartments (9) are disposed at a distance from each other in the hollow space of the end plate (1).

Abstract: An externally propelled load transporting apparatus that transports a uniformly distributed, non-uniformly distributed, or shifting load upon a cushion of air by first directing pressurized air into at least two plenum chambers and then through at least one flexible perforated sheet, wherein each plenum is substantially, independently pressurized.

Abstract: Disclosed is a hovercraft having a pair of air cushions, associated with each air cushion is a rotatable fan which partly produces lifting force and partly propels and maneuvers the craft. The fans are mounted perpendicular to the direction of travel, peripherally on the craft, wherewith the forces produced have long moment arms, and consequently produce a strong turning torque. The fans are mounted on the craft in such a manner that their orientation may be adjusted both horizontally and vertically with respect thereto.

Abstract: A hovercraft includes a rigid body and a flexible skirt pending from a lower periphery thereof. A main engine and propeller are coupled to the rigid body and provide a main propeller thrust. A plurality of thrust control vanes are located downstream of the propeller and divide the main propeller thrust into a horizontal thrust component directed rearwardly of the thrust control vanes and a vertical thrust component directed to a location under the rigid body so as to cooperate with the flexible skirt to form an air cushion on which the hovercraft rides. A plurality of steering control vanes are located downstream of the thrust control vanes and control the forward direction of the hovercraft. A single control stick controls the operation of both the thrust control vanes and the steering control vanes.

Abstract: An air-cushion vehicle of the type having a flat rigid platform with rigid longitudinal walls attached to the platform. In such an air-cushion vehicle a plurality of transverse trough-shaped skirts are provided so as to form a space bounded by the skirt and the platform which, when supplied with higher pressure air, serves to provide an air cushion chamber. The vertical height of the air cushion chamber can be varied in accordance with the present invention by extending or retracting the material of the trough-shaped skirts by way of an adjustment mechanism. In a preferred embodiment, the adjustment mechanism comprises a skirt bar attached to each of two longitudinal edges of the skirt and a mechanism for moving the skirt bars sideways closer together or further apart, thus varying the skirt's vertical dimension.

Abstract: Fluid-cushion supported apparatus, which may comprise a sidewall gas-cushion vehicle, is supported by a cushion of pressurized air formed and contained between the vehicle body and the surface. The front or bow end of the cushion is contained by an inflatable flexible skirt system comprising a row of ropes or like filamentary support members disposed in spaced, substantially parallel, relationship, with their end portions attached to the vehicle body. Flexible sheet material is draped over the support members so as to form loops extending laterally therebetween. The loops are also curved between the end portions of the support members.

Abstract: A method and apparatus are disclosed to transport and position a drilling rig over dry land, marshland and water. Surface effect vehicles having drive and positioning means that develop thrust against the surface over which they travel are used to lift and transport a drilling barge, after which they may be used as support and supply vehicles. Provision is made to adjust variable cargo loads so as to balance the assembled unit during transport.

Abstract: A water borne air cushion vehicle having a flat rigid upper rectangular sheet-like platform, and a plurality of flat rigid longitudinal walls attached substantially at right angles thereto and depending therefrom substantially parallel with the major axis of the platform. Two of the walls are disposed as side walls along respective edges of the platform, and a plurality of longitudinally spaced laterally aligned arrays of flexible trough-shaped skirts are looped with a space therein and fastened along the longitudinal edge of the underside of the platform flush with, but movable with respect to adjacent pairs of the walls. The skirts are extendable to a lesser depth than that of the walls, and a source of pressurized air is admitted through apertures of fixed size at a relatively high pressure to the skirts.

Abstract: A ground effect vehicle of the type supported by a cushion of gas and especially adapted for use within specially constructed roadways providing guidance along a plurality of axes. The application describes vehicles having skirts with lower margins adapted to conform to the cross sections of the roadways, with the roadways preferably being of arcuate cross section whereby sustenance of the vehicle is accomplished by maintaining an air cushion between the skirt and the bottom portion of the roadway, and whereby turning of the vehicle is accomplished by the banking of the vehicle in combination with the reaction to a curvilinear roadway sidewall, or in response to thrust having a lateral vector, or both.

Abstract: A heave alleviation and control device for a surface effect ship having a central plenum chamber pressurized from a source of pressure interconnected to a stern seal plenum chamber by a duct. The duct contains a first valve positioned between the inlet from the central plenum chamber and the outlet to said stern seal plenum chamber for controlling the flow of pressurized gas therethrough. The rear wall of the duct has an opening therethrough to the atmosphere. A second valve is positioned adjacent the opening within the duct to control the flow of gas under pressure therethrough. The two valves are interconnected by levers to a piston translatable within a cylinder for simultaneous movement with the piston. One side of the piston is exposed to the central plenum chamber pressure and the opposite side is exposed to a source of hydraulic fluid under a preselected pressure. Directional movement of the piston is provided by the pressure differential between the sides of the piston.

Abstract: A vehicle supported by an air cushion extending beneath at least the greater part of the lower surface of the rigid structure of the vehicle. An arrangement of skirts defining the air cushions is described. According to this arrangement, the cushion is bounded on each side of the axis of the vehicle by two parallel skirts, a peripheral skirt and an inner skirt, inclined towards the inside of the vehicle defining between them a series of auxiliary air cushions separated by transverse partitions which form skirts inclined towards the rear. The bottoms of the auxiliary cushions are formed by articulated perforated plates. The edges of the plates are connected to the rigid structure by flexible walls forming a flexible volume connected to the supply of air under pressure for the inner cushion.

Abstract: A ground-effect landing gear for use on aircraft intended for performing take-off and landing on unprepared soft ground comprises a platform mounting a flexible enclosure constructed in the form of a system of inflatable envelopes bounding an overpressure space near the ground surface. During transition to hovering and during movement of the aircraft the space is kept in communication with a compressed air source.

Abstract: This invention relates to ground-reaction machines, such as hovercraft, and is particularly concerned with flexible enclosure arrangements, often referred to as skirts, for enclosing a fluid cushion beneath the loading platform of the machine. According to the invention, air fed into the arrangement to form the cushion, is channelled or directed by cells having walls which are linked in series along the periphery of the platform. This ensures the feed and enclosure of a single undivided central cushion at a pressure which is substantially uniform and of which the boundaries represent an auxiliary structure. In a preferred construction, each of the cells is bounded by two flexible walls, all the horizontal sections of which are of bi-convex, lenticular shape.

Abstract: A vehicle riding on air cushions in which the lift of a platform is ensured by an arrangement of flexible skirts defining a central air-lift area at substantially constant pressure and a partitioned peripheral air-lift area. A closed loop of adjacent tubular skirts is inserted between the central and peripheral air-lift areas to increase the flying stability of the vehicle.

Abstract: An air-lift vehicle has inner and outer multi-lobed peripheral skirts arranged so that the corresponding lobes of the skirts are in register. Means is provided to supply compressed air to the inside of the inner skirt and between the inner and outer skirts for lifting purposes. The space between the skirts comprises a plurality of compartments each defined by two corresponding lobes of the inner and outer skirts. The lower edges of the lobes of the outer skirt at least are located in the same horizontal plane as a result of which the height of lift and the stability of the vehicle are improved.

Abstract: An automatic pitch stabilization and motion alleviation device for air cushion borne vehicles, equally applicable to fully-skirted and to rigid sidewall vehicles. The vehicle's air cushion plenum is divided into bow and stern compartments by a transverse seal. Vehicle lift fans and a unique ducting arrangement supply air flow to the air cushion compartments and seal system. A valve, in a portion of the duct feeding air to the forward compartment, regulates the pressure drop from the stern compartment to the forward compartment. The valve is capable of providing 30-100% higher mean pressure in the aft compartment relative to the forward compartment. The valve is actuated automatically by height, motion, rate, acceleration, and pressure sensors, the outputs of which are fed to the valve servomechanisms to provide effective underway dynamic control of the pressure differential between compartments for motion stabilization in pitch and for improvements of ride quality.

Abstract: The invention has to do with a system designed to support and/or guide a ground effect machine (1) along a supporting surface (2).This system consists of structure (4) carrying a load (F), a floating partition (5) holding the cushion (9) and a flexible partition (10) defining laterally between the structure (4) and the partition (5) an enclosure of suspension (13) having a variable volume which is connected with the cushion (9) through calibrated orifices (6). The enclosure of suspension (13) has a convergent-divergent configuration, for example biconic. The area of the base (S), the area (S.sub.o) at the level of the collar (15) and the angle (.theta.) of the enclosure (13) are predetermined and remain constant.

Abstract: An air-cushion, or ground-effect, vehicle is described which includes a central cushion defining assembly of skirts and a peripheral cushion defining assembly of skirts.The skirts of the central assembly are of lobe-like section and the skirts of the peripheral assembly are cylindrical. Any given skirt of the peripheral assembly is in contact with each two, like, adjacent skirts and with two of the skirts of the central assembly.

Abstract: In and for an installation comprising a fluid source and a plurality of fluid-using receivers to be fed with fluid from said source, a device for supplying fluid from said source to said receivers independently of one another, said device comprising a fluid manifold connected with said fluid source and branching out into a plurality of fluid emission nozzles having each an outlet opening, and a plurality of fluid-receiving pipes each of which is connected with a corresponding receiver and has an inlet opening located in line with and spaced by a gap from the outlet opening of a corresponding emission nozzle, the cross-sectional area of said inlet opening of a receiving pipe being at the very most equal to the cross-sectional area of said outlet opening of said corresponding emission nozzle.

Abstract: The skirt of a surface effects vehicle is made up of a plurality of oblong lements which are slanted toward the stern of the vessel. Each element partially rests against and/or supports the adjacent elements. This configuration reduces skirt drag, cushion leakage, skirt wear, as well as reducing the impact forces transmitted to the vehicle itself and increases obstacle heights which can be successfully crossed.