Abstract: The present invention concerns an all-terrain vehicle for use over a variety of terrain. The vehicle includes a main body having a cabin, a forward side, a backward side and two lateral sides; a pair of ground effect wings connected to the lateral sides of the main body, each wing having an angle of attack; a lift engine having necessary auxiliary equipment for operation thereof, wherein the lift engine is connected to the backward side of the main body and supplies a lift power to the vehicle; at least one lift fan connected to the lift engine; an engine mounted to the main body to provide energy to propel the vehicle forward; a wheel connected to the forward side of the main body, wherein the wheel is connected to the main body by a drive shaft; a control system to control the angle of attack.

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 trimaran type WIG (Wing-In-Ground) effect ship with a minimum waterplane area is disclosed. This WIG ship comprises a main hull and two half-submerged sub-hulls each having a minimum waterplane area capable of minimizing the wave resistance and appendage resistance of the ship, thus reducing speed loss on rough water. The WIG ship also has main and sub-wings and an effective propelling mechanism, designed such that they produce a strong lift force allowing a take-off of the ship sailing on water even at a low speed. The WIG ship is thus excellent in its seakeeping and maneuverability on the rough water. In the WIG ship, the main hull is intermediately positioned between the main wings and comprises a slender and half-submerged body, and bears 60% of the total displacement of the ship. The sub-hulls are respectively provided under the outer ends of the main wings, and each bear 20% of the total displacement, and act as an end plate.

Abstract: A ground effect vehicle apparatus comprising a vehicle body of integral and contiguous construction including a medial portion having an aerodynamic upper surface, and a pair of spaced apart laterally positioned portions separated by the medial portion. Lower extremities of the laterally positioned portions extend downwardly below the medial portion to restrain air flow between them as it moves toward the rear of the body. Forward extremities of the laterally positioned portions extend forward of the medial portion to, again, restrain air flow from moving laterally. Power plants are mounted within the medial portion and support aircraft type propellers positioned forward of the medial portion of the body. The propellers are mechanized for moving over an arcuate vertical range, such that their force vectors are directable between the horizontal and approximately 45 degrees above the horizontal.

Abstract: A ground effect vehicle apparatus comprising a vehicle body of integral and contiguous construction including a medial portion having an aerodynamic upper surface, and a pair of spaced apart laterally positioned portions separated by the medial portion. Lower extremities of the laterally positioned portions extend downwardly below the medial portion to restrain air flow between them as it moves toward the rear of the body. Forward extremities of the laterally positioned portions extend forward of the medial portion to, again, restrain air flow from moving laterally. Power plants are mounted within the medial portion and support aircraft type propellers positioned forward of the medial portion of the body. The propellers are mechanized for moving over an arcuate vertical range, such that their force vectors are directable between the horizontal and approximately 45 degrees above the horizontal.

Abstract: A motorcycle suspension system, which permits, interrelated front and rear shock absorbers of different physical characteristics and having different loading factors. However, an interrelated control is provided for balancing these differences and for providing good dive and squat control without bouncing. In addition, an improved arrangement for testing the cylinder of a hydraulic shock absorber is disclosed.

Abstract: An assembly “(42)” including a fluid levitated caster and a debris scraper “(31)” device positioned external to a levitation membrane “(11)”. Assembly “(42)” levitates heavy loads upon a near frictionless pressurized fluid, and also sweeps aside potentially membrane destructive debris “(25)” from a floor “(27)” in the path of movement. The external debris scraper “(31)” function does not noticeably increase movement friction, and does not require increased power air flow or consumption.

Abstract: A system for distributing road surface information comprising means for sensing numerical information on slipperiness of a road surface; means for sensing positional information of the travelling vehicle; means for transmitting the numerical information and/or positional information from the vehicle; means for collecting the information transmitted by a plurality of vehicles; means for preparing road surface information of a road on the basis of each information; means for distributing the road surface information also to a vehicle other than the vehicle; and means for receiving the distributed road surface information. By changing a parameter of road surface information in a vehicle movement control system such as an ABS or a VSC, the performance of the control can be improved.

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 tracked vehicle capable of traversing a variety of surfaces without damaging the surface traversed. The vehicle is capable of light or heavy-duty applications. An embodiment of the vehicle includes a track with a substantially smooth outer surface, and an inner surface including a portion having lugs, a driver sprocket assembly engaging the lugs, and a plurality of wheels spaced to minimize flexing of the track between each wheel in contact with the track while the track contacts the traversed surface.

Abstract: A novel means of stability for a lifting platform utilizing toroidal vortex airflow through air guide means. A toroidal vortex created by the airflow means efficiently maintains a raised air pressure zone beneath the lifting platform or body. Airflow is directed downwards by means of air guides, which serve to produce lift and control rotational motion of the lifting platform to achieve stability of the body during operation. The system can also be easily modified to function as an attractor device. Overall, the present invention explores the uses of vortex airflow towards maintaining rotational stability.

Abstract: A personal transportation apparatus has a frame defining a surface for supporting a load, and a plurality of air-cushion cells mounted to the frame and depending from a lower side thereof, the air-cushion cells each having a changeable height to accommodate variations in an underlying terrain during a translation of the frame over the terrain. A pressure source is mounted to the frame and is operatively connected to the air-cushion cells for supplying air under pressure to the cells, thereby generating an air-cushion support for the frame. An elevation mechanism is mounted to the frame for lifting the frame from one step to a next higher step of a stairway so that the frame ascends the stairway from a lowermost step to an uppermost step of the stairway.

Abstract: An automated guided apparatus capable of accurately determining its position within a walled environment such as a mine or building. A mobile unit incorporating an inertial measurement unit and a gray scale vision system processor/camera and/or a laser pointer is able to initialize its location and then update its location within the environment. The apparatus is especially adapted for producing tunnel plan views (“TOPES”) and also for guiding equipment through such environments.

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 novel Ground Effect Machine capable of operating in low airflow and low air-pressure conditions. By using an air bladder, partially filed with liquid, in lieu of a skirt, the invention is able to reduce airflow, and consequently maximize the lift provided by air pressure pump, thus minimizing the amount of air pressure required. In addition, by alternating between positive and negative air pressure within a pressure chamber beneath the ground effect machine, the invention may lift and transport heavy loads or securely fasten the ground effect machine to the floor surface.

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: A jack up work platform is recited. The work platform comprises a hovercraft vessel outfitted with several jack up legs. The hovercraft can traverse environmentally sensitive terrain such a brackish and freshwater marshes without the need to dig canals that may cause or exacerbate salt water intrusion. Once the drilling or exploration site is reached, the jack up legs may be lowered, lifting the work platform above the surface. Once the vessel is secured on the legs, it may be used like a conventional oil field work platform for drilling, exploration, or construction jobs for which other work platforms or vessels are typically used. The deck of the hovercraft may serve as the work platform or the deck may be provided with a cantilevered work platform extension. The hovercraft will preferably be provided with typical oil field heavy machinery such as a crane for assembly of the legs, and drill stem as well as for work on other structures.

Abstract: A method and system for floating an upper vehicle part from a lower vehicle frame includes a primary floating device, coupled to either the upper vehicle part or the lower vehicle frame, floats the upper vehicle part freely separate from the lower vehicle frame. A plurality of sensors sense appropriate road inputs. An electronic control unit, coupled to the primary floating device and the plurality of sensors, receives the road inputs and generates control signals for controlling the primary floating device in order to minimize movement of the upper vehicle part with respect to the lower vehicle frame.

Abstract: The present disclosure is directed to a method and apparatus for drilling rig mobilization and demobilization. The rig is assembled or constructed at a remote site. It is later taken apart and transported to another remote site or back to a staging point. The rig itself comprises a rig floor which is supported on a set of vertical rig legs which support the rig floor for movement between raised and lowered positions. An equipment module is preferably installed on the rig floor. It goes above the rig floor while other modules are attached under the rig floor and provide additional equipment and service space. The method involves the transportation of the rig floor, the legs, equipment module and other modules to and from the rig site by hover craft while riding on a top deck on the hover craft for lateral transfer and installation.

Abstract: The invention relates to a ground-effect vehicle for the rapid transport of people and/or freight, with at least one body, a drive train and ground-effect bearing surfaces, a guidance system for directional control and a drive system on the body and/or bearing surface in the form of propeller or fan drives. The aim of the invention is to provide a ground-effect vehicle which is inexpensive to build, avoids the prior art drawbacks in particular and is especially economical to operate. According to the invention, the ground-effect vehicle consists of at least one aircraft fuselage (1), the ground-effect bearing surfaces (2) are secured directly at least to parts of the existing bearing surfaces (6) of the aircraft or at least on the existing spars (12) surrounding them or secured thereto beneath the existing bearing surfaces (6) and that the drive system (4; 15; 16) has means which increase the power and/or reduce friction in the take-off and landing phases.

Abstract: A method and apparatus for measuring the lift generated by airfoils of an aircraft. This real-time analysis is accomplished by measuring a differential pressure between the upper and lower lift surfaces of the airfoils. The system comprises the steps of: a) measuring an actual differential pressure between the upper and lower lift surfaces for a given aircraft speed, b) transmitting this actual differential pressure measurement to a computer, c) comparing the actual differential pressure measurement with an optimal pressure differential for the same aircraft speed. The apparatus comprises a fixed array of differential pressure sensor mechanisms for measuring actual pressure differentials and a computer for comparing optimal differential pressure measurements to the actual differential pressure measurements. Each sensor mechanism preferably contains a piezoelectric sensor that communicates with the upper and lower lift surfaces.

Abstract: An air bearing assembly transports loads across a smooth and flat surface when pressurized with air. The air bearing assembly includes a frame and an air bearing. The frame has a flat side for supporting a load and has an inner ring extending from its other side. The air bearing includes a backing plate and a flexible diaphragm that forms an enclosed footprint on the surface when pressurized. The footprint of the diaphragm uniformly overlap the ring of the frame. A damping chamber is formed by the inner ring of the frame and by the backing plate. The damping chamber is sealed when the diaphragm is pressurized by the upward force exerted by the diaphragm upon the backing plate against the inner ring.

Abstract: An upright vacuum cleaner includes a main body, a floor nozzle unit, and a float plate or float unit. The main body has a motor fan for generating a suction force and a dust-collection chamber for collecting dust. The motor fan provides the suction force to the dust collection chamber. The floor nozzle unit is disposed under the main body. The floor nozzle unit has an inlet port connected to the dust-collection chamber for attracting dust on a floor into the dust-collection chamber by the suction force of said motor fan. The float plate or float unit is disposed on a lower face of the floor nozzle unit. The float plate or float unit includes a floor opposing face where an outlet port is formed for spouting discharge air to the floor from the motor fan. The float face is located around the outlet port to receive a lifting force produced by pressure of the discharge air between the float face and the floor to be cleaned.

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 present invention is for a hovercraft load transport assembly which incorporates an air cushion assembly having a fan powered by an engine. The fan draws air into the device downwardly to fill the neoprene skirt of the device. This causes the device to essentially "float" above the ground on a cushion of air. The neoprene skirt is supported on a metal frame. In one embodiment, optional thrust tubes at the back of the device allow for directional movement. Thrust and throttle controls allow for variance in the lift, speed and movement of the device. There is also a load carrying and dumping receptacle which is hydraulically actuated.

Abstract: A hovercraft includes a plurality of energy storing containers for storing a low-temperature, high-pressure gas therein, a heat exchange device for performing heat exchange between the gas from the containers and a high-temperature exhaust from a gas turbine engine unit, and an air-cushion generating device accepting the gas from the heat exchange device so as to form an air cushion. The air-cushion producing method for the hovercraft includes producing the high-temperature exhaust from the gas turbine engine unit, providing the low-temperature, high-pressure gas, performing heat exchange between the gas from the containers and the exhaust from the gas turbine engine unit, combining the gas and the exhaust after the heat exchange by siphon action, and directing the gas and the exhaust into the air-cushion generating device.

Abstract: An apparatus (1) that can be converted into an air cushion support or into an air cushion support for a vehicle (3). This apparatus can be folded into a compact container or put onto its own wheels (2) permitting it to be hauled as a trailer. The apparatus comprises a latticed folding base composed of hingedly connected main sections (10) and perimeter sections (11-14), a flexible inflatable air cushion skirt (5) and coupling means (8,9) for coupling the vehicle (3) to the main sections of the base, to propulsion and blowing means (6) and to a steering gear mechanism (7). The lower surface of latticed sections is covered by elastic airtight sheet material (33,34) which forms a chamber (35) of the flexible inflatable skirt and an air cushion chamber (37).

Abstract: An airborne vehicle generally comprises a body, a lifting mechanism for lifting the vehicle, and a steering mechanism operable by a user for steering the vehicle. The lifting mechanism comprises first and second counter-rotating propellers mounted in a front end and a rear end, respectively, of the vehicle body. The lifting mechanism further comprises a front air intake and a rear air intake mounted in proximity to and above the first and second propellers, respectively. The steering mechanism comprises a plurality of louvers mounted on a bottom of the vehicle body below the first and second propellers. The operator uses a steering mechanism in a passenger position to adjust inclinations of the louvers so as to steer the vehicle.

Abstract: An apparatus for measuring the lift generated by airfoils of an aircraft. This real-time analysis is accomplished by measuring a differential pressure between the upper and lower lift surfaces of the airfoils. The apparatus a) measures an actual differential pressure between the upper and lower lift surfaces for a given aircraft speed, b) transmits this actual differential pressure measurement to a computer, c) compares the actual differential pressure measurement with an optimal pressure differential for the same aircraft speed, and d) evaluates performance of the aircraft based on the result of the comparison. The apparatus comprises a fixed array of differential pressure sensor mechanisms for measuring actual pressure differentials and a computer for comparing optimal differential pressure measurements to the actual differential pressure measurements. Each sensor mechanism preferably contains a piezoelectric sensor that communicates with the upper and lower lift surfaces.

Abstract: A ground effect vehicle wherein a flap coupled to a spoiler is provided on the wings in order to break lift when the craft starts to leave ground effect travel in order to avoid flight out of ground effect.

Abstract: This invention relates to a toy supported by a self-generated air-cushion. The toy has a platform, a pillow, a fan and a motor to drive the fan. The platform sits above the pillow. The fan and its motor are located centrally and substantially within the pillow and close to the surface over which the toy hovers. The fan draws air into the pillow and expels air through perforations in a bottom sheet of the pillow. This generates an air-cushion between the pillow and a surface over which the toy hovers. The air-cushion enables the toy to glide along the surface upon application of an external force, such as a push from a child's hand. The platform supports a figure which can be a real or animated character.

Abstract: An upright vacuum cleaner has a floating function for lifting the upright vacuum cleaner in a cleaning operation by spouting discharge air flow to a floor to be cleaned, and at least a suction-air inlet port for sucking air with dusts is arranged at an outer portion of a bottom face of a floor nozzle unit of the upright vacuum cleaner.

Abstract: A system for automatically steering a vehicle through an irregular structure. A flexible lighting tube, in proximity to the back of the structure, communicates with at least one canted video camera. A processor takes the output of the camera, determines the position of the vehicle, and provides guidance to the vehicle's steering mechanism.

Abstract: A trailer-container for a vehicle (1) which can be converted into a support base on an air cushion comprising a rigid sectionalized platform (4) equipped with a flexible inflatable air cushion skirt (5) with removable rotor-type power plants (6) and means for coupling them to the drive of the vehicle (1) mounted on the platform. The platform (4) of the trailer-container is made of rigid interconnected sections which can be folded into a compact package. The sections are connected to the flexible inflatable skirt (5). Each of the power plants (6) is made as a blower fan and a variable-pitch air screw which are mounted coaxially in a common ring housing. The platform (4) together with the skirt (5) is fitted with disengagable attachment joints for securing it to the wheelbase of the vehicle (1) so that disturbances of the platform and skirt can be damped by suspension of the vehicle when in motion.

Abstract: A delta wing form body is provided having a central forward apex as well as rear opposite side apices. Each apex includes a vertical powered fan duct assembly extending therethrough and the rear of the wing form body includes forward thrust developing horizontal fan duct assemblies while the center of the body includes laterally and longitudinally shiftable weight structure for omnidirectional shifting of the center of gravity of the wing form body. The center and opposite side fan duct assemblies open downwardly into central and opposite side downwardly opening longitudinal tunnels, respectively, each including retractable and extendable front and rear flap assemblies. The wing form body also includes rear forward thrust developing propulsion fan duct assemblies and all of the fan duct assemblies are variably speed driven from a single power source.

Abstract: A method and apparatus for measuring the lift generated by airfoils of an aircraft. This real-time analysis is accomplished by measuring a differential pressure between the upper and lower lift surfaces of the airfoils. The system comprises the steps of: a) measuring an actual differential pressure between the upper and lower lift surfaces for a given aircraft speed, b) transmitting this actual differential pressure measurement to a computer, c) comparing the actual differential pressure measurement with an optimal pressure differential for the same aircraft speed. The apparatus comprises a fixed array of differential pressure sensor mechanisms for measuring actual pressure differentials and a computer for comparing optimal differential pressure measurements to the actual differential pressure measurements. Each sensor mechanism preferably contains a piezoelectric sensor that communicates with the upper and lower lift surfaces.

Abstract: The present invention describes an air-floated vacuum cleaner comprising a housing having an air inlet opening, an open bottom and an inner wall, an impeller for pressurizing air within the housing to float the housing above a support surface, and a novel vacuum module/agitator located below the impeller. The vacuum module/agitator is rotatable with the impeller for agitating dust and debris on the support surface and for simultaneously suctioning the dust and debris upwards for lateral displacement against the inner wall. The dust and debris is then centrifuged to a duct communicating with the inner wall. The air-floated vacuum cleaner further includes a flotation plate module for entrapping and sealing within the housing pressurized air generated by the impeller.

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 simple and low maintenance Ride Control System (RCS) for Air Cushion Vehicles (ACV) is presented. This RCS reduces the effect of water wave generated pressure pulses on ACV ride by venting the pressure pulses from the pressurized supporting gas cushion and/or restricting gas flow into a powered blower that supplies the pressurized supporting gas cushion as the pressure pulses occur. The preferred embodiment utilizes high aspect ratio low moment of inertia vanes that are individually driven by brushless electric servo motors and the vanes can rotate in either direction through 360 degrees. A vane braking and locking mechanism is presented that brakes and locks the vanes in a closed position in the event of power failure to the vane drive motors. A further feature of the invention is a venturi that is positioned between the powered blower and the pressurized supporting gas cushion to reduce the effect of the pressure pulses on blower operation.

Abstract: This invention makes use of a pressure sensor, which is installed on the wing's surface of the aircraft, to sense the varied air pressure which comes from ground-effect on the wing's surface. A control apparatus is comprised of pressure sensor, a device of signal treatment and the device of elevator control. This apparatus solves the problems of excessively low ground-effected flying altitude and low efficiency of the whole aircraft.

Abstract: A simple, low cost, and reliable, normally cyclic, fluid control valve that in preferred configuration includes one or more rotary valve elements where such valve elements have openings that align with each other and/or with a flow passageway thus forming an aperture for fluid flow during valve cycles. Rotary valve elements may be oriented in different directions to connecting ducts and may have a variety of shapes with a preferred shape being cylindrical. Simple motors drive rotary valve elements such that a rate of valve cycling and/or amount of aperture can be easily controlled by a controller such as a microprocessor. Easy valve servicing and installation are other features. Dynamic sealing of the fluids is preferably accomplished by use of simple low cost labyrinth seals.

Abstract: A hovercraft is described having a fan mounted to rotate about a vertical axis. The airflow from the fan is directed to the skirt to create lift and to horizontally aligned outlets to positively propel the craft in both forward and reverse directions and, if necessary, provide a braking force. A valve arrangement is provided to alter the relative airflow between the different horizontally aligned outlets.

Abstract: Two wheels of different modes are provided which add guidance capabilities to air cushioned vehicles. A tractor utilizes the wheel of the first mode, a wheel mounted upright upon a hollow tubular hub, being a half-torus. A trailer utilizes the wheel of the second mode, a wheel mounted upright upon a sphere which is cut off at the base to allow for ample platform clearance. Both vehicles are air cushioned, enabling them to hover above a support surface. Steering is affected by directing the tractor vehicle with the aid of a novel curved gear series on the inside rim of the wheel of the first mode. Twisting action upon the rim and wheel resulting from stress created between the steering sprocket and a drive sprocket, being synchronized when normal by a timing belt. The steering sprocket is effected by operator control and encounters the curved portions of the special gear teeth, thereby causing the tractor to turn. The wheels of both modes can be tilted by the operator's actions.

Abstract: Noise due to the rotation of the air propeller or fan of an air-cushion vehicle is reduced by: 1) reducing the cross-sectional area of the interior of a duct encompassing the fan on the downstream side relative to the upstream side; 2) using wide-chord fan blades of chords increasing from blade root to tip; 3) using a duct and a nose cone on the hub of the fan both having a sound-absoring structure; and 4) mounting the engine and the duct on a common rigid support base and reducing to a minimum the tip clearance between the tips of the fan blades and the duct inner wall surface.

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: Fingers having air bearings along the bottom thereof are used to quickly load and unload overseas transport containers. Sheet material, such as ribbed plastic (nylon) sheeting, is automatically dispensed between the fingers and loading deck so that it provides a smooth surface as the finger traverses the dock. A frame is mounted to the front of the finger, with a shaft on which the sheet material is coiled mounted to the frame, and an air motor for applying a generally constant tension (e.g. about 10 lbs. per square inch) to the plastic sheet. A hook or magnet is mounted in a recess in the deck and engages the free, leading end of the sheet material to hold it stationary on the deck as the finger traverses the deck, and thereby provide for automatic dispensing and take up of the sheet material.

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: An amphibious vehicle comprises a fuselage having a pair of support pods at the front end thereof and a single support pod at the rear. In accordance with one embodiment of the invention, each pod has a fan therein and in accordance with another embodiment, the pods serve as floats. The vehicle has a top wing adjacent the rear thereof and a bottom wing adjacent the front, each of which have elevator surfaces thereon. Port and starboard engines are positioned adjacent the rear of the vehicle.

Abstract: The present invention concerns hull shapes for a surface effect ship, including a catamaran type supported structure with two side walls (100) connected by a center platform (200), able to operate either as a buoyant displacement vehicle, or as an air cushion supported vehicle, the side walls (100) confining, with two sealing devices (310, 320), the supporting center air cushion (c).