Abstract: A system for cushioning airdropped cargo includes a pallet supporting associated cargo. At least one lower inflatable impact attenuator in the form of a pneumatic cushion is positioned between the pallet and the cargo. A compression pad is positioned between the lower pneumatic cushion and the cargo. At least one upper pneumatic cushion is positioned atop the cargo. A parachute is connected by parachute rigging to the pallet.

Abstract: A trim system for an airboat having a hull and a deck comprises an engine support carriage elevated from the deck and having a first end pivotably mounted to the deck via a rigid frame, and at least one remotely operated hydraulic ram with each including a first end braced upon the deck or an intervening structure and a second end coupled to a free moving second end of the engine support carriage opposite the first end. In a method of adjusting trim on an airboat, during operation of an engine mounted to the engine support carriage, a thrust line of the engine is selectively changed by remotely causing the at least one linearly actuated lift to selectively extend and retract.

Abstract: A movable support platform is disclosed that includes a platform, a skirt coupled to a periphery of the platform that provides an enclosed space below the platform that retains pressurized gas, and a thrust propulsion device coupled to the platform for pressurizing gas in the enclosed space. The thrust propulsion device includes an array of gas-propelling devices “distributed thrusters” that propel gas into the enclosed space below the platform. The distributed thrusters may be comprised of Nano Molecular Solid-state Electrodynamic Thrusters (“NMSET”).

Abstract: A ground effect transport system comprising a plenum roof platform for location beneath a load carrying means, a skirt depending from the platform to form a plenum chamber with the platform, fan means on or in the platform for supplying air to the plenum chamber, wherein the skirt extends downwardly towards the ground surface and has a ground engaging support member for supporting the bottom of the skirt above the ground surface and a separate detachable sealing member for providing a seal between the bottom of the skirt and the ground surface.

Abstract: A modular system that provides multiple support surfaces for a large heavy object and enables movement of that object with no friction (e.g., on a cushion of air). Each module has an object support surface and a bearing that enables the modules and the heavy object being supported thereby to be moved across a floor with no friction. Each module restrains a portion of the object on top within a frame that opens to allow the supported portion of the object to move off the support surface of the module and onto a stationary object support structure (e.g., a milling machine bed), using a cushion of air at an elevated height from the floor equal to that of the top surface of each module. The modules can be used independently or locked together to move a very large and heavy object or can be used to build a type of bridge which the air bearings underneath the object can cross.

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: An air-cushioned vehicle or hovercraft includes a three-dimensional frame comprising a latticework of tubular members. A pressure plate is coupled to the underside of the frame and includes at least one aperture therein and a skirt attached adjacent a periphery thereof. At least one lifting fan is positioned relative to the at least one aperture to generate a current of air therethrough. The frame may be configured to generate a visual indication of damage thereto. Methods of making and air-cushion vehicle are disclosed. Methods of using an air-cushion vehicle are also disclosed.

Abstract: A mobile robot generally including a first suction module, a second suction module and a hinge assembly pivotably connecting the suction modules together. Each of the suction modules includes a support frame defining a vacuum chamber and a vacuum unit supported on the support frame and communicating with the vacuum chamber. The vacuum unit includes a rotating impeller and an exhaust cowling surrounding the impeller. The impeller has an axis of rotation and is adapted to draw air from the vacuum chamber into the impeller in a direction generally parallel to the impeller axis of rotation and to discharge the drawn air in a direction substantially perpendicular to the impeller axis of rotation. The exhaust cowling is adapted to redirect the discharged air, whereby a thrusting force is applied to the support frame in a direction opposite of the direction of the drawn air from the vacuum chamber.

Abstract: An aircraft including a fuselage and at least one wing which may vary incidence with respect to the fuselage for the purpose of extremely short take off and landing and an air cushion system mounted beneath the fuselage for the purpose of surface independent taxi, take off, and landing. The wings may be straight, forward swept, swept, or have the ability to change shape and sweep based on the conditions of flight. The air cushion system may use engine thrust for lift or may use a separate lift system, which is specifically used for the air cushion. The air cushion skirt may also be rigid, non-rigid, or semi-rigid, but shall incorporate a flotation and support system, to allow flotation on water and parking of the aircraft on solid surfaces.

Abstract: In accordance with the present invention, there is provided a workstation or other heavy object which is easily moved, yet steady and stable when parked. Underneath this object is attached a multiple air-bearing device having a backplate, a membrane which is selectively bonded to the backplate, and a stencil and dimple which further prevent separation of the membrane from the backplate and which also provide a bearing surface for the workstation to rest with stability against the floor. Pressurized air is introduced through the base and behind the unbonded portions of the membrane, inflating the membrane and creating lift, and additionally forming a pneumatic seal against the floor. Air passages through the membrane and within the sealed footprint allow air to flow into and through the region between the membrane and the floor, creating an air-lubricated bearing that allows nearly frictionless motion of the heavy object.

Abstract: Skirts for air cushion vehicles that are formed from material that is tensively strengthened in at least one direction, and preferably two different directions, so as to resolve and reduce the axial and radial stresses in the skirt. The material may be strengthened by incorporation of reinforcing cords arranged to reduce the axial and radial stresses in the skirt both when a vehicle comprising such a skirt is static and when it is in motion.

Abstract: A multi-mission/purpose ground-effect craft is provided which is derived from a common modular platform which includes a hull; an inner floor structure adapted to be installed over the hull; a body adapted to be attached to at least one of the top surface of the hull and the inner floor structure, such that a interior compartment is formed thereinside; a tail wing assembly adapted to be attached to the aft end of the body; a forward nose cowl adapted to be attached to at least one of the forward nose portion of the hull and the forward body portion of the body; a windshield integrated into the forward end of the body; at least one door assembly integrated into the left or right body side; at least one window assembly integrated into the left or right body side; a propulsion system integrated within the aft end of the body; and a retractable skirt attached and draped from the outer or inner perimeter of the hull.

Abstract: A light air-cushion vehicle has a thrust reverser bucket arranged at an output end of an air nozzle, at least one direction rudder having control surfaces at the output end of the air nozzle and at least one direction rudder having control surfaces in a lift contour, a control system for the thrust reverser bucket and a control system for the direction rudders. The direction rudders are kinematically connected to each other and to a steering device. The control surfaces at the output end of the air nozzle turn around an axis in the vertical direction and the control surfaces in the lift contour turn around an axis in the longitudinal direction axis.

Abstract: The present invention relates to an improved amphibious craft or vehicle and, in particular, but not exclusively, to a craft or vehicle that may be used for commercial and rescue tasks in a great variety of weather conditions. To achieve this, an amphibious vehicle comprises a fixed geometry planing hull (2) and a skirt system (4). This has as an advantage that the fixed geometry planing hull (2) allows the craft or vehicle to operate in high waves, strong winds or other adverse conditions too severe for known hovercraft of a similar size, while the skirt system (4) contains a cushion of air providing the craft or vehicle with a full amphibious capability so that the craft can operate as a conventional hovercraft in good conditions or enter and leave water in any conditions.

Abstract: The present invention is an air cushion vehicle and a control mechanism for steering and turning the vehicle. The air cushion vehicle includes a frame having a skirt body extending around the perimeter. An air flow generator may be positioned on the frame for providing a lift flow and thrust flow. At least one vane is disposed on the frame to direct the thrust flow. At least one fin is disposed on the frame downstream of the vane for directing the thrust flow. A turning controller may be used for moving the vane and fin in a coordinating movement to affect the direction or the motion of the air cushion vehicle.

Abstract: A marine air cushion vehicle provides a hull having a hull periphery, an inflatable bag connected to the hull at the hull periphery, an inflatable skirt connected to the bag, and a pair of inflatable lateral stability seals, each extending generally perpendicular to the hull central longitudinal axis and to port and starboard positions. A plurality of inflatable open cones are attached to the inflatable bag, the open cones being positioned in between the lateral stability seals in a fore to aft direction. The skirt includes in part the inflatable open cones. In another embodiment, the open cones can be alternatively placed in between the lateral stability seals or in front of the lateral stability seals, in between a lateral stability seal and the hull bow. In another alternative embodiment, inflatable open cones can be positioned in between a lateral stability seal and the hull stern.

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: An exemplary embodiment sets forth an apparatus, including a non-collapsible single unit stair comprising: a pair of opposing side rails supporting at least a top step and a bottom step; a coupler adapted to couple the apparatus to an edge of a horizontal surface; and a height adjustable user-support arm, coupled to one of the side rails with a rotatable coupling, wherein the user-support arm is moveable between a support position and a storage position.

Abstract: An air board including a platform upon which an operator of the vehicle can be supported; and a support arrangement for providing an air flow for supporting the platform above a surface, wherein the direction of movement of the air board is at least partially controlled by varying the weight distribution of the operator on the platform.

Abstract: A multi-modal forced vortex device is described having a top plate and a side wall creating a partially enclosed volume. The top plate includes one or more adjustable fluid openings to permit, or restrict, fluid flow into and out of the partially enclosed volume. Rotating blades housed within the partially enclosed volume are manipulated (through control of their pitch and, possibly, their speed) in conjunction with the adjustable fluid openings to generate a variable magnitude attractive force in a first mode, a variable magnitude down or pushing force in a second mode, a variable magnitude up or lifting force in a third mode or variable magnitude yaw, pitch and roll forces in a fourth mode.

Abstract: A lightweight and durable skirt assembly for an air cushion vehicle having a rigid support structure. The skirt comprises at least one air chamber. The air chamber is formed from a substantially air impermeable, laminated sheet material. The laminated sheet material comprises a fabric made substantially from yarns that are formed from polymers of ultra-high molecular weight polyethylene. The fabric is laminated with a thermoplastic film.

Abstract: A hybrid air boost vehicle makes use of the porous panels and suction devices of a vehicle aerodynamic drag reduction system, and makes use of the air consumed by such a system, to provide the energy and air to power a land or water based ground effects vehicle. Energy and air consumed by the suction system, and normally wasted, is recycled by providing an air cushion to partially support the vehicle. The entire hybrid air boost vehicle system is more efficient than either a drag reduction system or a ground effects vehicle alone, and the benefits of both are realized, as well as benefits unique to the hybrid vehicle.

Abstract: A transporting apparatus (10) comprises a transporting plane (11) and a transporting platform which can be displaced in different directions in a largely friction-free manner on an air cushion above the transporting plane (11), the air cushion being generated by air nozzles (13) which are distributed in the transporting plane (11) and can be optionally opened and closed individually in each case by means of a valve, and through which compressed air flows out in the upward direction from beneath through the transporting plane (11), and the valves of the air nozzles (13) and the transporting platform being designed such that they interact with one another depending on the position of the transporting platform.

Abstract: A transportation system has an air cushion vehicle in a U-shaped or W-shaped channel in the ground. The channel provides support and directional stability for the air cushion vehicle during transit along its length. This system assures high speed overland transport of heavy equipment which is faster than trains, and the system is cost effective since it does not incur expensive nonrecurring capital investments and expensive recurring maintenance costs. This transportation system is adaptable to existing overland right-of-ways.

Abstract: Control of air cushion vehicles is obtained by controlling the translation of the vehicle independently from control of the rotation (yaw). Lateral translation of the vehicle is controlled by creating side-directed thrusts the direction of which passes through or as close as possible to the yaw axis by diverting variably controllable flows of air from the flow of air used to create a propulsive air thrust for forward translation of the vehicle to left and right lateral control ports located more or less parallel to the fore-aft axis of the vehicle sufficiently proximate to a plane which passes through the yaw axis and is perpendicular to the fore-aft axis of the vehicle so that diverted air flows exiting the ports approximately perpendicular to the fore-aft axis create thrusts which predominantly pass through the yaw axis. (In the absence of external forces the yaw axis passes through the center of gravity of the vehicle.

Abstract: An inflated roll-stabilizing keel system has a first trough-shaped bladder nd a second trough-shaped bladder attached to the underside of a forward portion of the first trough-shaped bladder. Holes pass through from the first trough-shaped bladder to the second trough-shaped bladder to allow inflation to flow therein. A plurality of shaped bladders are attached successively along and to the first trough-shaped bladder immediately aft of the second trough-shaped bladder. Each shaped bladder has a rectangular base portion attached to the underside of the first trough-shaped bladder. Each shaped bladder tapers downward from its base portion to an open apex. An inflation hole passes through from the first trough-shaped bladder to each of the shaped bladders to allow inflation air to flow therein. Once inflated, adjacent shaped bladders contact one another between the base portion and open apex in an area of contact.

Abstract: The hybrid dirigible craft belongs to the category of flying vehicles which use an air cushion and take off and land at any type of airfield. The air of the invention is to design an improved dirigible craft capable of taking off from and landing on water and low-load bearing surfaces.

Abstract: A surface effect vehicle includes a vehicle body having opposed longitudinally extending sides and a longitudinally extending deck having an upper and lower surfaces extending widthwise between the sides. The lower surface together with opposed inner surfaces of the sides form a downwardly depending air entrapment chamber extending longitudinally beneath the lower surface. The chamber is reactive to provide substantial surface effect ram air lifting force on the vehicle in response to forward motion of the vehicle. In addition, the vehicle includes an airfoil spaced above and interconnected with the vehicle body to provide substantial out of surface effect lifting force on the vehicle in response to such forward motion. Further the vehicle vertical stabilizers serving not only to provide vertical stabilization but also to interconnect the airfoil with the vehicle body.

Abstract: A surface effect vehicle for traversing a water or ground surface is provided. The surface effect vehicle comprises an elongate body and forward and rear scoops, preferably having a large angle of attack inducing stall conditions on the scoops. Each scoop has an arched leading edge defining, in conjunction with the surface, a forwardly facing opening. Preferably, each scoop also has an opening with a fan mounted therein. Forward and rear skirts are movably mounted relative to the forward and rear scoops. Propulsion apparatus are provided for moving the surface effect vehicle across the surface. When the forward and rear skirts are placed in extended positions covering the forwardly facing openings and the front and rear fans are activated, the surface effect vehicle may be lifted relative to the surface to be traversed.

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: An air cushion vehicle having a low drag, high stability non-scooping skirt system including closed loop finger sleeves. An enlarged bag combines to provide a more responsive skirt profile. The sleeves of this invention are trimmed at an angle to the supporting surface, thereby exposing the sleeve opening to the air cushion. The sleeve is maintained at the air cushion pressure unless the vehicle rolls enough to submerge and close the sleeve opening. A pressure build up occurs as the opening is submerged and a significantly greater differential pressure is obtained with an enhanced restoring moment. The interior wall of the sleeve that faces the air cushion is angled slightly inward on the bow and side seals to allow momentary collapse of the sleeve and release of an extraordinary force of a rough sea. In addition the effective air cushion area, the platform of the vehicle, is extended to its maximum to provide greater stability.

Abstract: A static trimmer for a hovercraft is provided for shifting the center of buoyancy of an air-cushion of the hovercraft in relation to the center of gravity. The static trimmer includes a peripheral elastic skirt (2) having a plurality of skirt segments (5) each having a back skirt (3) and a finger skirt (4). The peripheral elastic skirt (2) further includes at least four independent lateral sections (6, 7, 8, 9) which can be moved in an inward or outward direction independently of each other. The static trimmer further includes at least two tension cables (15, 16) disposed in each independent lateral section (6, 7, 8, 9) for moving each finger skirt (4) of each of the plurality of skirt segments (5). Each of the tension cables (15, 16) further include a first partial tension cable and a second partial tension cable.

Abstract: The air cushion chambers of an air cushion vehicle are horizontally delimited by a skirt. The skirt comprises brushes with elongated downwards extended filaments (9), which have downwards diminishing cross-sectional area thereby providing the brushes with sufficient stiffness to maintain the pressure in the air cushion chamber and such a large flexibility in the lower section of the skirt that ice can hardly deposit thereon. The filament members are mounted in a guide profile (2) in such a manner that above the members there is a chamber (12) for dispersion and conveying of deicing fluid which form the chamber (12) via a flow passage in every filament member may pass down into a clearspace (10) between the filaments (9). At least one of the filaments (109) has forward protruding web (115) on one of its sides and a backwards protruding web (116) on its other side.

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: A small-sized air cushion vehicle includes a hull having a planar bottom surface with an upstanding lower flange disposed at a predetermined angle with respect to the bottom surface. A plurality of apertures are formed in the peripheral flange. An upper hull is mounted on the lower hull and includes a centrally located occupant area. The upper hull engages the lower hull to form a hollow plenum chamber extending internally around the periphery of the upper and lower hulls. A plurality of inflatable members are mounted on the exterior surface of the peripheral flange and are each disposed in fluid flow communication with an aperture in the peripheral flange. A motor driven fan is mounted on the upper hull and directs a portion of an air stream rearward of the vehicle to propel the vehicle and another portion of the air stream into the plenum chamber to inflate the inflatable members and to lift the vehicle a short distance above an underlying surface.

Abstract: A combined propulsion and lift unit for an air-cushion vehicle is provided comprising an elongate shaft mounted for rotation about its central longitudinal axis, bearings for rotatably supporting the shaft, an axial wheel with two or more blades mounted on the shaft for rotation therewith, a first housing extending peripherally about the shaft, the housing provided with an air inlet and an air outlet, a drive device connected to the shaft for rotating same at a selected speed, a centrifugal fan wheel mounted on the shaft for rotation therewith, the fan wheel provided with an air inlet, the fan wheel located inside the first housing, and a second housing extending about the perimeter of the axial wheel and the first housing, the second housing having a larger diameter than the first housing thereby defining an air passageway therebetween, the second housing provided with an air inlet and an air outlet.

Abstract: The present invention relates to a method of mounting a skirt on an air cushion vehicle body in an air cushion vehicle (trade name, Hovercraft) to easily mount or dismount the skirt on the air cushion vehicle body and having the step of respectively mounting a pair of latch members for forming a surface adhesive fastener at the skirt mounting position and the skirt opening peripheral edge mounting position of the air cushion vehicle body, thereby easily mounting and dismounting the skirt.

Abstract: A device comprising a main body, a motor and drive wheels mounted on the main body, a partitioning member mounted on the main body and defining a pressure reduction space in cooperation with the main body and a wall surface, and a vacuum pump for reducing the pressure of the pressure reduction space. The device can suction-adhere to the wall surface by the pressure of an ambient fluid acting on the main body owing to the difference in fluid pressure between the inside and outside of the pressure reduction space and move along the wall surface by the action of the moving member. The partitioning member has an outside wall portion extending from its one end to a contacting portion contacting the wall surface and an inside wall portion extending from the contacting portion to its other end.

Abstract: In an air cushion load transport vehicle, an annular sealing assembly comprising an annular inflatable hanger on the underside of a load-bearing base and an annular sealing means on the underside of the hanger confines a load-supporting air cushion that is continuously supplied with compressed air during operation. Stability is promoted by a number of design features in the inflatable hanger, the annular sealing means, the flexible connection between them and the load support structure. These include means for automatically closing off flow through hanger damping eyelets during initial hanger pressurization together with means to keep the eyelets open at all operating hanger heights. Additional covered ports are provided in the outer hanger wall positioned to automatically vent if the hanger is over-inflated thereby avoiding dynamic instability. A check valve is incorporated into the device to prevent damage from inadvertantly inflating the hanger before the cushion is pressurized.

Abstract: A device comprising a main body, a motor and drive wheels mounted on the main body, a partitioning member mounted on the main body and defining a pressure reduction space in cooperation with the main body and a wall surface, and a vacuum pump for reducing the pressure of the pressure reduction space. The device can suction-adhere to the wall surface by the pressure of an ambient fluid acting on the main body owing to the difference in fluid pressure between the inside and outside of the pressure reduction space and move along the wall surface by the action of the moving member. The partitioning member has an outside wall portion extending from its one end to a contacting portion contacting the wall surface and an inside wall portion extending from the contacting portion to its other end.

Abstract: A fluid-cushion-supported pallet or water skate in which the cushion-fluid is generally defined by a multi-part or segmental, flexible skirt, in which the contiguous skirt members have their downwardly and inwardly extending lateral portions flanked by tie portions extending inwardly from the lateral portion toward the space occupied by the fluid-cushion, the contiguous tie portions are secured outwardly of the inner edges to restrict the escape of the cushioning fluid, and the segmental flexible skirt prevents sideways deflection of the skirt segments caused by relative movement between the device and surface over which the device operates.

Abstract: Fluid cushion equipment comprising a floor having valves supplied by a matrix of fluid supply lines and a fluid cushion platform. Positioning of the platform on or above the valves actively causes them to open to supply fluid beneath the platform which is trapped by flexible hollow tubular skirts. The platforms are driven in the described direction by one or more wheeled drives which are only in contact with the floor when thrust is required.

Abstract: An amphibious air cushion vehicle includes a body defining an air containment wall, and an inflatable tube is attached to the body and defines a rearward opening. A fan is positioned within the body to force pressurized air into the compartment, and a gate is provided in operative relationship with the body and with the opening for selectively enabling pressurized air to exit rearwardly through the opening from the compartment to impart forward motion to the vehicle.

Abstract: A surface effect transport vehicle is provided having a structure supported by a cushion of pressurized air generated from a blower. The propulsive source of the vehicle is independent from the power source of the blower. The propulsion source includes at least one retractable propeller device adapted to be made operative during travel over the water and nonoperative during travel over land, and at least one retractable wheel device, for travelling over land or in shallow water, which is made operative when the propeller device is retracted to its nonoperaitve condition, and vice-versa. Preferably the wheel device has at least two lateral faired propellers operative when the propeller device for propulsion over water is retracted to its nonoperative position. The supported structure includes automatic controls that simultaneously controlling the lift properly speaking, the attitude of the vehicle as well as its stability when passing over an obstacle or at the time of a dynamic disturbance.

Abstract: An air cushion vehicle capable of operation over land or water, which includes a hull carrying at least one air supply unit, an outer inflatable member connected to and extending around the entire perimeter of the hull, which supports a flexible skirt system which extends down from the inflatable member, which it is part of, and air under pressure is supplied by the air supply unit to the skirt system in a regulated manner, to provide a balanced cushion at the bow, sides and stern and to prevent decaying of the cushion and ploughing. Self contained ballast apparatus is provided to trim the vehicle.

Abstract: A self-trailering hovercraft is disclosed, having wheels such that the wheels can remain in the same position when the hovercraft is trailering or in the hover mode, or retracted for additional ground clearance while in hover mode if desired. A trailer hitch is provided that can be adjusted to various hitch heights for trailering or removed completely for operation in hover mode. Further, cockpit covering and unique U-shaped skirts having good closing and susceptable to easy repair are disclosed.

Abstract: To make a skirt part of a surface-effect vehicle readily and reliably retainable to the vehicle while able to be folded to be sent to the position of use, the skirt part has an enlarged bead to be slid into a restricted-mouth channel on the vehicle, the core of the bead being an elongate spiral spring of stainless steel. End-plugs are fitted to prevent endwards escape from the channel.

Abstract: An improved seal design for a Surface Effect Ship, having an inflatable ir seal member, and outer seal member composed of a pliable sheet material scrollably affixed to the hull fore and aft of the inner seal member. The seal may be retracted for hullborne operation by deflating the inner seal member and scrolling the outer seal member tight to hull. The inner seal member has transverse webbing for stability. The outer seal member is periodically scrolled foreward to expose an unworn section to the water surface thereby reducing seal failure due to wear.

Abstract: The purpose of this invention is to improve the life of transversely stiffened membrane (TSM) seals. To this end the inventors have introduced a segmented glass reinforced plastic (GRP) plank into the lower stiffened lobe portion, which is positioned beneath the bag segments of the TSM seal. The segmented (GRP) planks consist of planks separated by rubber spacers and sandwiched between two sheets of rubber coated nylon fabric.