US3608662A - Air cushion vehicle - Google Patents

Air cushion vehicle Download PDF

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Publication number
US3608662A
US3608662A US2810A US3608662DA US3608662A US 3608662 A US3608662 A US 3608662A US 2810 A US2810 A US 2810A US 3608662D A US3608662D A US 3608662DA US 3608662 A US3608662 A US 3608662A
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Prior art keywords
air
vehicle
vanes
steering
downstream flow
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Hugo S Ferguson
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COGSWELL ARNOLD
AIR CUSHION VEHICLES Inc
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AIR CUSHION VEHICLES Inc
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Assigned to COGSWELL, ARNOLD reassignment COGSWELL, ARNOLD ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: ROWLEY, RICHARD R.
Assigned to ROWLEY, RICHARD R. reassignment ROWLEY, RICHARD R. ASSIGNMENT OF ASSIGNORS INTEREST. Assignors: HARVEY, JONATHAN P.
Assigned to ROWLEY, RICHARD R. reassignment ROWLEY, RICHARD R. ASSIGNOR BY BILL OF SALE DOES HEREBY GRANT, BARGAIN, SELL AND CONVEY UNTO ASSIGNEE THE ENTIRE INTEREST. (SEE RECORDS FOR DETAILS). Assignors: HARVEY, JONATHAN P., TRUSTEE FOR AIR CUSHION VEHICLES, INC., (BANKRUPT)
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/14—Propulsion; Control thereof

Definitions

  • a single propeller mounted toward the front of the vehicle provides both propulsion and air cushion.
  • This invention relates to air cushion vehicles. Although particularly directed to a relatively small and inexpensive vehicle capable of carrying one or two passengers, some of the features may be applied to larger and more elaborate vehicles.
  • air cushion vehicles utilize an arrangement for producing a cushion of air under pressure beneath the vehicle so asto raise the vehicle a short distance from the supporting surface in operation.
  • the supporting surface may be water, ground, snow, ice, etc.
  • Two principal types of structure are commonly employed for producing the air cushion.
  • One type employs an open plenum chamber beneath the vehicle with a relatively large volume of low-pressure air supplied thereto.
  • the plenum chamber usually is formed by a downwardly extending peripheral wall or skirt which, together with the bottom of the vehicle, forms a chamber which is open at the bottom.
  • the other principal type employs a peripheral slot or jet which procedures a downwardly and inwardly sloping curtain of air under relatively high pressure.
  • the open plenum chamber has the virtue of simplicity.
  • the air curtain type is in general more efficient, in that less air is lost, but involves a much more complicated structure. In either case, sufficient air must be continuously furnished to maintain the pressure under the vehicle to raise it from the supporting surface, and to replace the air exhausted around the bottom periphery of the vehicle.
  • an air cushion vehicle When raised from the ground in operation, an air cushion vehicle is essentially floating on air and the propelling and steering means must be designed to take this into account.
  • Many means have been provided in the past for creating thrusts in difi'erent directions to propel the vehicle forwards, to brake forward motion or produce rearward motion, and to turn the vehicle.
  • vanes in the peripheral skirt are controlled to change the direction of the air issuing therefrom.
  • a supply chamber for delivering pressurized air to a peripheral air curtain is provided with vanes on the sides thereof, and at the front and rear, and the vanes are controlled to produce movement of the vehicle in the desired direction. Vanes inside a plenum chamber have also been suggested for propulsion and control.
  • rudders In vehicles using propellers in the open air, rudders have been used for steering. With a single propeller the rudder is commonly at the rear. With propellers and respective engines mounted fore and aft on the vehicle, individual rudders may be located behind each propeller for steering purposes.
  • the present invention provides an air cushion vehicle which requires only a single engine and propeller for producing the air cushion, propulsion and steering, while providing both fore and aft steering control, and which has other advantageous features which will be described hereinafter.
  • air propelling means is mounted toward the forward end of the vehicle.
  • a single propeller and engine sufiice For the relatively small vehicles particularly contemplated, a single propeller and engine sufiice.
  • Means for producing an air cushion under the vehicle is provided, and preferably a portion of the air from the air propelling means is used for the purpose.
  • front steering means are provided for changing the direction of the downstream flow of air to lateral angles on either side of the vehicle, thereby providing a steering force toward the front of the vehicle.
  • Air-channeling means spaced downstream of the front steering means is provided for receiving portions of the downstream flow of aid, under the control of the front steering means, and directing the flow of air therethrough to the rear of the vehicle.
  • Rear steering means is positioned toward the rear of the vehicle on each side thereof to receive the downstream flow of air from the air-channeling means and divert the air supplied thereto to lateral angles on either side of the vehicle, thereby providing a steering force toward the rear of the vehicle.
  • the downstream flow of air In forward travel over a horizontal surface without a crosswind, the downstream flow of air is generally longitudinal of the vehicle and propels the vehicle forward. In turning, a portion of the downstream flow of air is diverted outside the airchanneling means to provide a turning moment, the amount diverted depending on the sharpness of the turn. The remainder of the air is directed by the air-channeling means to the rear steering means to provide a turning moment thereat.
  • the air-channeling means is designed and spaced from the front steering means so that, under all normal steering conditions, a sufficient amount of air is directed to the rear steering means for adequate control. For normal turns the lateral angles of the front and rear steering means are in opposite directions so that both turning moments are effective and the center of turning is between the two steering means, and advantageously near the center of the vehicle.
  • the front and rear 1 steering means may be turned to lateral angles in the same direction, so as to prevent skidding.
  • the normal turning lateral angles may be modified to take into account the tendency to skid.
  • the lower portion of the downstream air from the propeller is supplied to the open plenum chamber beneath the vehicle through an opening in the floor of the body, and the propeller axis is inclined somewhat downwards and rearwards to facilitate supplying air to the open plenum chamber.
  • Fixed vanes are provided in the opening to divert a portion of the air toward the front of the underside of the vehicle, thereby approximately equalizing air pressure over the bottom surface.
  • a set of generally vertically extending vanes is provided immediately behind the propeller and controllable to direct downstream flow of aid generally longitudinally of the vehicle or to lateral angles on either side of the vehicle.
  • a centrally located body structure is provided behind which the operator sits, and suitable controls are placed therein.
  • This body structure is designed to divert the downstream flow of air along the sides thereof.
  • a set of generally vertically extending vanes is provided on each side of the vehicle to receive air passing through the respective channel.
  • the angle of the front vanes is changed in the direction of the desired turn, and the angle tending the rear vanes is changed in the opposite direction.
  • the rear vanes produce an outward tilting moment which is considerably smaller, so that the net result is to tilt the vehicle into the turn, as is desirable.
  • both front and rear vanes may be turned in the same direction so as to produce a counteracting side thrust which opposes the side wind.
  • the vehicle body is constructed largely of foamed plastic material which provides a simple, inexpensive structure having many desirable qualities including lightweight, rigidity, flotation, bumper protection and vibration absorption.
  • FIGS. 1 and 2 are perspective views of an aircushion vehicle in accordance with the invention, from side front and side rear, respectively;
  • FIGS. 3 and 4 are plan and side elevation views of the vehicle
  • FIGS. 5 and 6 are longitudinal and lateral cross sections taken along the lines 5-5 and 6-6 of FIG. 3, respectively,
  • FIG. 7 is a diagrammatic showing of the steering controls, and FIG. 7a shows a partial modification thereof;
  • FIGS. 8-11 are schematics illustrating steering vane positions and airflow under difi'erent operating conditions
  • FIG. 12 illustrates a variable ratio pulley construction for the rear steering vanes and FIG. 12a is a graph showing the relationship between front and rear steering vane angles as a function of the steering wheel angle;
  • FIGS. 13-45 illustrate a modified steering arrangement, FIGS. 14 and 15 being cross sections taken along line 14-14 and 15-15 of FIG. 13.
  • the vehicle has a body platform 10, advantageously of foamed plastic providing sufiicient buoyancy to support the vehicle and passengers in water, even if the vehicle is overturned.
  • a body platform mounteded on the body platform toward the front end thereof is an air propeller 1 1 driven by an engine 12 (FIGS. 4,5).
  • a shroud 13 around the propeller is designed in accordance with known aerodynamic principles to form a short duct which improves the propeller efficiency.
  • the shroud is designed as a ring airfoil.
  • the downstream portion of a true airfoil is, in effect, cut off to reduce the length of the shroud.
  • a set of upwardly extending front steering vanes 14 mounted for rotation about upwardly extending axes 15 (FIGS. 4,5) so that, by turning the vanes in either direction, the downstream flow of air from the propeller is directed to lateral angles on either side of the vehicle.
  • Upwardly extending rear steering vanes are mounted near the rear of the vehicle on each side thereof, and are here shown as two sets of vanes 16 and 16', mounted for rotation about upwardly extending axes 17 (FIG. 6).
  • front vanes 14 also serve to reduce the rotation of the air from the propeller.
  • Air-channeling means is mounted on the body platform between the front and rear steering vanes.
  • An inner member has upwardly and rearwardly extending laterally spaced walls 18 and 18' which are joined at the front thereof as indicated at 18".
  • the upper portion of the front end or nose 18" is rounded to promote a smooth flow of air.
  • the lower portion may be flat to provide room for engine 12.
  • Upwardly and rearwardly extending outer walls 19 and 19' are laterally spaced from respective inner walls 18, 18' to form respective open-ended laterally spaced channels 20, 20' (FIGS. 8-11) which receive respective portions of the downstream flow of air from the propeller, under the control of the front steering vanes 14, and direct the flow of air therethrough to respective sets 16, 16' of the rear steering vanes.
  • the channels are provided with top members 21, 21' which extend to the upper part of the shroud 13 over the propeller, thereby preventing rearward flow of air from the propeller above the top members.
  • the space between the front steering vanes and the air channels is open laterally to the ambient air and the functioning thereof will be described later.
  • a steering wheel 22 is mounted on a panel 23 attached to the sidewalls 18, 18' of the inner channel member, and a seat 30 is provided for the operator.
  • a gasoline tank, storage battery, etc. may be mounted under the seat, as indicated in FIG. 5.
  • a compartment 24 provides a backrest for the operator and support for the rear vane structure, and is advantageously hollow with a hinged cover for storage purposes.
  • a pair of horizontal airfoils 25, 25' are mounted on horizontal axles 26, 26, and may be manually angled upwards or downwards by respective handles 27, 27 to serve as stabilators which take into account different weights of the operator. Detents are provided to retain the stabilators in any position of adjustment, but are not shown in detail.
  • a railing 28 may be provided in front of the operator's position, and a hand throttle 29 mounted thereon. The latter is spring biased to its closed position.
  • the body platform 10 is provided with a downwardly extending peripheral wall 31 forming an open plenum chamber 32 beneath the vehicle. Air from the lower portion of the propeller 11 is admitted to the plenum chamber through a slotlike opening 33. Curved fixed vanes 34 are provided to direct a portion of the air to the forward part of the plenum chamber 32, so as to approximately equalize the air pressure in various parts of the plenum chamber.
  • a steering wheel for the front vanes and a foot treadle for the rear vanes or vice versa.
  • a joint steering control including override means for changing the relative orientation of front and rear vanes.
  • a connecting link 41 (FIGS. 5 and 7) is pivotally connected to the rear ends of each of the front steering vanes 14, and flexible steering cables 42, 42' are connected to each end of the connecting link 41, or to suitably spaced points therealong.
  • Pulleys 43 are provided for guiding the steering cables, as indicated in FIG. 7, but are not specifically illustrated in FIG. 5 to avoid confusion in the drawing. Cables 42, 42' are led back through suitable guide means to a pulley 44 attached to a shaft in the steering wheel column 45, and the ends suitably affixed to the pulley.
  • the steering wheel 22 is attached to the end of the shaft.
  • connecting links 47 and 47' are pivotally connected to the rear ends of each of the set of rear steering vanes l6, l6 and a rigid member 48 connects the links.
  • Flexible steering cables 49, 49' are connected to respective links 47, 47 and are connected at their ends to a pulley 51 on the steering wheel shaft.
  • Guide pulleys such as indicated at 52, 52 are provided as required.
  • FIG. 70 may be employed.
  • a pair of pulleys 53, 53' are mounted on the vehicle.
  • a flexible cable 54 is attached at each end to respective links 47, 47' so that both links move simultaneously in the same direction.
  • pulley 44 is designed as an overriding clutch, and a pair of foot-operated pedals 55, 55 are pivoted intermediate their ends about a horizontal axis and their upper ends attached to respective cables 42, 42' leading to the front steering vanes.
  • the foot pedals are attached to short tubes which encircle a shaft mounted between the inner walls 18, 18' of the body structure.
  • FIG. 8 the condition of normal forward propulsion on a level surface is shown, in the absence of any appreciable crosswind.
  • the front steering vanes 14 are aligned fore and aft and direct the downstream flow of air from propeller l1 equally to the two laterally spaced air channels 20, 21, as indicated by the arrows.
  • the channels direct the airflow to respective sets of rear steering vanes 16, 16' which are likewise aligned fore and aft. This produces a forward thrust, as indicated by arrows 61.
  • FIG. 9 shows the condition for a medium right turn.
  • the front steering vanes 14 are turned so as to direct the downstream flow of air at a small lateral angle toward the port side of the vehicle.
  • a portion of the air will be diverted outside the left channel 20, to the ambient air as indicated by arrow 62, and consequently will produce a front steering force toward the right, as indicated by dotted arrow 63.
  • a considerable portion of the downstream flow of air will continue to flow through the port air channel 20, and a somewhat smaller portion will flow through the starboard channel 20'.
  • FIG. shows a hard right turn wherein the front and rear steering vanes are turned at greater angles.
  • the lateral airflow outside channel 20, to the ambient air indicated by arrow 66 will be greater, thus producing a greater steering force tending to force the front end of the vehicle to the right, as indicated by dotted arrow 67.
  • Considerable airflow will still pass through the port channel 20 to the rear set of steering vanes 16, producing a flow of air in the direction indicated by arrow 68. This will produce a turning component 69, as well as a propulsion component.
  • the airflow in the starboard channel 20' will be still further reduced and, depending upon the detailed design and the angle of vanes 14, may be negligible. However, sufficient air will still flow through the port channel 20 to produce adequate steering control at the rear.
  • FIG. 11 shows a condition where it is desired to move the vehicle forward along a straight line, in the presence of a crosswind from the right, as indicated by arrow 71, or to travel along a sidehill.
  • the front and rear steering vanes are angled in the same direction so as to provide front and rear thrusts indicated by arrows 72 and 73, 73.
  • the components of these forces acting laterally are indicated by dotted arrows 74, 75, and are in the same direction to oppose the crosswind 71.
  • the side thrust produced by the front steering vanes will be greater than that produced by the rear steering vanes since a portion of the downstream flow of air will have been diverted laterally of the vehicle.
  • the point about which the vehicle turns will depend on a number of factors including the center of gravity of the vehicle (including the operator),
  • the resultant turning point is usually in the vicinity of the center of the vehicle, much closer to the front steering vanes than to the rear steering vanes.
  • the effective lever arm for the rear steering vanes is considerably greater than that for the forward steering vanes, so that the efiective turning moment of the rear steering vanes is comparable to that of the front steering vanes for at least moderate turns.
  • the rear steering vanes provide a more sensitive control, that is, the rear steering vanes are more effective in producing a turning force than the front steering vanes. Consequently, it has been found desirable to vary the ratio between the angles of the front and rear steering vanes as a function of the turning angle desired.
  • this is accomplished by providing a variable ratio pulley 51 for the rear steering vanes as is shown in FIG. 12.
  • the pulley includes two spaced discs 81, only one of which is shown, between which are four posts 82-85. Cables 49, 49' from the rear steering vanes pass over a guide pulley 86 and around posts 83, to post 82 where their ends are secured at 87.
  • the radial positions of posts 82-85 and the distance from the center 88 of the pulley to the point 89 where the cables pass around guide pulleys 86 are selected so that the combined lengths of cables 49, 49 from post 82 to point 89 is approximately constant as pulley 51 rotates through 90 in either direction from that shown.
  • the overall length of cables 49, 49' to the rear vanes provides sufficient elasticity to accommodate the variation. More perfect results could be obtained with properly shaped cam surfaces, but would be more expensive.
  • the effective radius of the pulley 44 which controls the front vanes may be selected to yield the desired relative vane angles for each position of the steering wheel.
  • the radius was 1% inches, lying between the minimum and maximum effective radii of pulley 51.
  • the dotted line 92 in FIG. 12a shows the front vane angle as a function of steering wheel angle.
  • the front vanes turn more rapidly than the rear.
  • the rate of turning of the rear vanes increases until it equals and then exceeds that of the front vanes.
  • the ratio between the turning angles of the rear and front vanes varies from smaller values at small turning angles to larger values at large turning angles within the turning range.
  • a steering wheel 101 is attached to an inner steering tube member 102.
  • Variable ratio pulley 51 for the rear steering vanes, has a hub 103 which is affixed to tube 102 by clamp 104.
  • Pulley 105 for controlling the front steering vanes, has a hub 106 attached to an outer steering tube member 107 by clamp 108.
  • a hub 109 is rotatably mounted on tube 102, and is part of or afiixed to the outer tube member 107.
  • a spacer tube 111 encircles the outer tube 107 and a short tubular section 112 is clamped to tube 107 by clamp 113.
  • Grommet 114 is mounted in a suitable opening in panel 23 and allows the steering tubes to turn therein.
  • Another grommet 115 is mounted in a structural member 116 to allow rotation of the steering tube 102.
  • Hub 109 has a pair of wings 117 between which a detent 118 is pivoted at 119.
  • An inner plate 121 of the steering wheel has slots 122 formed therein at suitable angular intervals.
  • Detent 118 is biased by spring 123 so that a projection 124 thereof enters one of slots 122. By pressing downwards on detent 118, and rotating it, the detent may engage in any one of slots 122. Inasmuch as the detent is mounted on hub 109,'
  • the relative angles of the front steering vanes with respect to the rear steering vanes may be manually adjusted to counteract crosswinds, sideslip on the slope of a hill, etc.
  • the vehicle In performing a turn, it is desirable for the vehicle to lean into the turn.
  • the downstream flow of air from the propeller toward the rear of the vehicle is inclined somewhat downward from the horizontal.
  • the height of the rear steering vanes may be less than that of the front steering vanes, and will still intercept substantially all of the air directed thereto through the channels 20 and 20'.
  • both forces will be efi'ective to tilt the vehicle, force 63 tending to tilt the vehicle inwards of the turn and force 65 outwards.
  • the effective point of application of the force 63 will be higher on the vehicle than the effective point of application of force 65, yielding a greater lever arm for the tilting moment (force times distance).
  • the force 63 will be larger than force 65, since all the downstream flow of air traveling above the vehicle platform will pass through the front vanes 14, whereas in a turn only a portion will reach the rear vanes, and that portion will become smaller as the turn becomes more severe. This is because the front vanes divert more and more air outside the air channels, as has been explained in connection with FIGS. 8-10. Consequently the net result will be a tilting moment tending to tilt the vehicle into the turn, and that of the front vanes will predominate more and more as the turn becomes more severe.
  • the nose 18" of the inner walls of the air channels may be moved somewhat toward the port side so that approximately equal thrusts are obtained on both sides when traveling in the forward direction.
  • the front vanes 14, 14 may be turned at a slight angle for the central position of the steering wheel, to compensate for the difference in thrust on port and starboard sides in travelling straight ahead.
  • the lateral spacing of the outer walls 19 and 19' of the air channels is selected so that the downstream flow of air, with the front vanes 14 in their midposition, is slightly inside the walls.
  • the spacing of the outer walls from the front vanes is selected so that, with the front vanes at an angle of 45 to the centerline of the vehicle, approximately one-half of the air is directed outside the channel which is on the side of the vehicle toward which the air is diverted.
  • the lateral positioning of outer walls 19, 19' of the channels is such that the high velocity flow of air is slightly inside the walls.
  • the airflow indicated by arrow 66 is about one-half the total downstream airflow from propeller 11.
  • the front edges of outer walls 19, 19' may be positioned closer to, or farther from, vanes 14 to change the proportion of air directed outside the channels for any given vane angle, as meets the judgement of the designer for optimum steering control.
  • the tilt of the propeller shaft and the cross section of opening 33 may be selected to provide adequate air for the cushion, and angles of 15 and 1 156 from the horizontal have been employed with success. For a given area of opening 33, the smaller tilt gives a greater propulsion thrust.
  • the height of the rear vanes and horizontal airfoils 25, 25' may be selected so that the airstream extends somewhat above the airfoils, thereby enabling effective trim control.
  • the body platform 10 and the downwardly extending peripheral wall 31 are advantageously formed of foamed material, cemented or otherwise joined together to form a unitary structure.
  • platform 10 was molded of foamed, closed-cell, rigid polyurethane with a tough skin produced by maintaining the mold at a suitable temperature to form the desired skin thickness, in accordance with considerations known in the art. This yields a density of around 4 lbs/cu. ft. in the core, and around 30 lbs./cu ft. in the skin.
  • the peripheral wall is formed of foamed, closed-cell, semirigid polyethylene having a density of about 2 lbs./cu. ft.
  • the wall is conveniently fabricated from sheet material adhered by heat, and then cemented to the body platform.
  • the semirigid wall has sufiicient flexibility to avoid serious damage when travelling over rough terrain, and serves as a bumper to avoid damage when striking piers, docks, aboveground objects, etc. Further, the structure has the marked advantage of absorbing vibration from the motor.
  • the body structures mounted on the platform including walls 18, 18', 19, 19', shroud 13, seat 30, etc., are also advantageously molded of foamed, closed-cell, rigid polyurethane with a tough skin, similar to platform 10, thereby yielding a rugged, yet lightweight superstructure.
  • the overall weight may be kept to about 250-300 lbs, with sufficient flotation to support 1,000 lbs. or more, and capable of carrying a load (including operator) of about 300 lbs.
  • the invention provides a lowcost air cushion vehicle capable of carrying one or two people, with a single propeller providing both air cushion and propulsion, and with two-point steering control.
  • the steering control can be apportioned between front and rear vanes as desired.
  • the operator is protected from the blast of air from the propeller, and air curtains are formed on either side of the operator to protect against spray, dust and the like.
  • An air cushion vehicle including a body, and means for propelling and supporting said body on an air cushion including air propelling means mounted toward the forward end of said body and adapted to produce a downstream flow of air in the rearward direction of the vehicle, in which the improvement comprises a. front steering means for changing the direction of said downstream flow of air to lateral angles on either side of the vehicle,
  • rear steering means positioned toward the rear of the vehicle on each side thereof and adapted to divert downstream flow of air supplied thereto to lateral angles on either side of the vehicle
  • An air cushion vehicle which comprises a body platform,
  • steering means for turning said front and rear steering vanes to change the direction of airflow therefrom to respective lateral angles on either side of the vehicle
  • a vehicle in accordance with claim 3 in which the spacing between said front steering vanes and the outer walls of said channels and the lateral spacing of the outer walls are predetermined so that for at least larger lateral angles within the turning range of the front steering vanes a substantial portion of the downstream flow of air is directed outside the channel which is on the side of the vehicle toward which the air is diverted.
  • a vehicle in accordance with claim 4 including a shroud over at least the upper portion of said propeller means, and
  • top members extending over said channels between respective inner and outer walls thereof, said top members extending to said shroud, whereby downstream flow of aid from said propeller means above said top members is substantially prevented.
  • a vehicle in accordance with claim 5 in which said top members are inclined downward from front to rear and said air propeller means is inclined backward to produce a downstream flow of air to the rear steering vanes which is inclined downward from the horizontal, and the height of the upper ends of the rear steering vanes is substantially less than the height of the upper ends of the front steering vanes.
  • said steering means includes joint control means for simultaneously turning said front and rear steering vanes in opposite direction, and including variable ratio means coupling said joint control means to said front and rear steering vanes for changing the ratio between the turning angles of the rear and front vanes from smaller values at small turning angles to larger values at large turning angles within the turning range, and means for changing the relative angles of the front and rear steering vanes controlled by said joint control means.
  • said means for producing the air cushion includes an opening in said body platform behind the lower portion of said air propeller means for directing air from said lower portion to the space beneath said body platform, and vane means in said opening for directing a portion of the air flowing therethrough to the forward part of said space.
  • a vehicle in accordance with claim 8 including a peripheral wall adhered to said body platform to form a unitary structure therewith and extending outwardly and downwardly thereof, said body platform being formed primarily of a foamed, closed-cell, rigid plastic and said peripheral wall being formed primarily of a foamed, closedcell, semirigid plastic.
  • a vehicle in accordance with claim 3 including a shroud over at least the upper portion of said propeller means, and top members extending over said channels between respective inner and outer walls thereof, said top members extending to said shroud, whereby downstream flow of air from said propeller means above said top members is substantially prevented.
  • a vehicle in accordance with claim 10 including an operator position located behind said front joining section of the air-channeling means and laterally between the laterally spaced channels provided thereby, whereby air flowing through said channels to the rear steering vanes on respective sides of the vehicle provides air curtains on either side of an operator in said operator position.
  • top members are inclined downward from front to rear thereof to produce a downstream flow of air to the rear steering vanes which is inclined downward from the horizontal.
  • a vehicle in accordance with claim 12 in which said air propeller means is inclined backward from the vertical to produce a downstream flow of air approximately parallel to said top members.
  • said means for producing the air cushion includes an opening in said body platform behind the lower portion of said air propeller means for directing air from said lower portion to the space beneath said body platform, and vane means in said opening for directing a portion of the air flowing therethrough to the forward part of said space.
  • a vehicle in accordance with claim 3 including a peripheral wall adhered to said body platform to from a unitary structure therewith and extending outwardly and downwardly thereof, said body plad'orm being formed primarily of a foamed, closed-cell, rigid plastic and said peripheral wall being formed primarily of a foamed closedcell, semirigid plastic.
  • said steering means includes joint control means for simultaneously turning said front and rear steering vanes in opposite directions, and means for changing the relative angles of the front and rear steering vanes controlled by said joint control means.
  • said steering means includes joint control means for simultaneously turning said front and rear steering vanes in opposite directions, and variable ratio means coupling said joint control means to said front and rear steering vanes for changing the ratio between the turning angles. of the rear and front vanes from smaller values at small turning angles to larger values at large turning angles within the turning range.
  • a vehicle in accordance with claim 3 in which said means for producing the air cushion includes means for directing a portion of the air from said air propeller means to the space beneath said body platform.
  • An air cushion vehicle which comprises a. a body,
  • means for propelling and supporting said body on an air cushion including air propelling means mounted toward the forward end of said body and adapted to produce a downstream flow of air in the rearward direction of the vehicle,
  • front steering means for changing the direction of said downstream flow of air to lateral angles on either side of the vehicle
  • rear steering means positioned toward the rear of the vehicle on each side thereof and adapted to divert downstream flow of air supplied thereto to lateral angles on either side of the vehicle
  • the rearward position and lateral spacing of said air channels being predetermined so that, over a substantial portion of the steering range of the front steering means, an increasing lateral angle of the downstream flow of air from the front steering means on either side of the vehicle produces an increasing airflow laterally outside the air channel on the respective side and a decreasing airflow to the air channel on the other side while maintaining airflow to the air channel on said respective side.
  • An air cushion vehicle which comprises a. a body,
  • means for propelling and supporting said body on an air cushion including air propeller means mounted toward the forward end of said body and adapted to produce a downstream flow of air in the rearward direction of the vehicle,
  • the rearward position and lateral spacing of said air channels being predetermined so that, over a substantial portion of the steering range of the front steering vanes, an increasing lateral angle of the downstream flow of air from the front steering vanes on either side of the vehicle produces an increasing airflow laterally outside the air channel on the respective side and a decreasing airflow to the air channel on the other side while maintaining airflow to the air channel on said respective side.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Body Structure For Vehicles (AREA)
  • Special Spraying Apparatus (AREA)
US2810A 1970-01-14 1970-01-14 Air cushion vehicle Expired - Lifetime US3608662A (en)

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Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3861491A (en) * 1972-12-14 1975-01-21 Hugo S Ferguson Air cushion vehicle
US3869020A (en) * 1973-07-12 1975-03-04 Douglas W Holland Air cushioned vehicle
US3887030A (en) * 1972-12-15 1975-06-03 Christopher John Fitzgerald Duct systems for air cushion vehicles
WO1987000492A1 (en) * 1985-07-22 1987-01-29 Howell Murrell D Pitch controlled ground effect vehicle
US4643268A (en) * 1982-04-05 1987-02-17 American Antigravity Co., Inc. Air lifted and propelled vehicle
US5042605A (en) * 1989-01-07 1991-08-27 Sorekkusu Kabushiki Kaisha Apparatus for controlling air cushion vehicle
US5097919A (en) * 1989-07-05 1992-03-24 Dowty Woodville Polymer Limited Surface effect vehicle
US5738302A (en) * 1996-04-02 1998-04-14 Freeland; Verne L. Airborne vehicle
US5941331A (en) * 1992-02-13 1999-08-24 Gastesi; Ignacio Air cushion vehicle control system
US20050095930A1 (en) * 2003-10-31 2005-05-05 Garcia Phillip P. System to propel an air powered boat
US20050194196A1 (en) * 2003-11-12 2005-09-08 Mattel, Inc. Hovercraft
US20060019556A1 (en) * 2004-07-26 2006-01-26 BALDWIN Charles Air-boat sound suppressor and directional control system
US20080149780A1 (en) * 2006-12-22 2008-06-26 Pendzich Jerome S Vertical lift vehicle
WO2009068909A1 (en) * 2007-11-30 2009-06-04 Fergus Johnathan Ardern Hover dodgem
US20110266081A1 (en) * 2009-01-05 2011-11-03 Ivan Novikov-Kopp Method for comprehensively increasing aerodynamic and transport characteristics, a wing-in-ground-effect craft for carrying out said method (variants) and a method for realizing flight
US20160052503A1 (en) * 2014-08-25 2016-02-25 Cameron HOWELL Apparatus including user-platform assembly and air-thrusting assembly and method therefor
US10160435B2 (en) * 2015-10-14 2018-12-25 Foshan Quark Brother Technology Co., Ltd. Hovercraft using single ducted fan with vectoring propulsion

Families Citing this family (1)

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Publication number Priority date Publication date Assignee Title
SE446965B (sv) * 1984-05-17 1986-10-20 Skold Bjorn Ake Svevarkonstruktion

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US2364677A (en) * 1940-11-13 1944-12-12 Douglas K Warner Compression airplane
US3066753A (en) * 1960-02-26 1962-12-04 Curtiss Wright Corp Ground effect machine
US3127949A (en) * 1961-05-11 1964-04-07 Walter T Harter Ground effect machine with controls therefor
US3150731A (en) * 1960-03-25 1964-09-29 Curtiss Wright Corp Air cushion vehicle construction including control valves
US3162260A (en) * 1959-06-10 1964-12-22 Hovercraft Dev Ltd Vehicle for travelling over land and/or water
US3173507A (en) * 1962-04-17 1965-03-16 Lucas Industries Ltd Weighbridges
US3208543A (en) * 1961-07-19 1965-09-28 American Mach & Foundry Air cushion vehicle
US3243003A (en) * 1961-08-30 1966-03-29 Gen Delivery Ground effect machine
US3259097A (en) * 1964-07-10 1966-07-05 John Van Veldhuizen Air-propelled boat
US3262510A (en) * 1962-06-04 1966-07-26 Alphons J Froehler Air cushion vehicle with lift, turn, and brake controls
US3292721A (en) * 1963-10-02 1966-12-20 Franklin A Dobson Toy air car
US3322223A (en) * 1963-05-16 1967-05-30 William R Bertelsen Ground effect machines
US3401766A (en) * 1964-11-02 1968-09-17 Aircars Inc Air-cushion vehicle
US3467213A (en) * 1966-08-17 1969-09-16 Dowty Rotol Ltd Gas turbine powered air-cushion vehicle with propulsive jet means
US3486577A (en) * 1965-10-21 1969-12-30 Arthur M Jackes Axial flow ground effect machine

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Publication number Priority date Publication date Assignee Title
US2364677A (en) * 1940-11-13 1944-12-12 Douglas K Warner Compression airplane
US3162260A (en) * 1959-06-10 1964-12-22 Hovercraft Dev Ltd Vehicle for travelling over land and/or water
US3066753A (en) * 1960-02-26 1962-12-04 Curtiss Wright Corp Ground effect machine
US3150731A (en) * 1960-03-25 1964-09-29 Curtiss Wright Corp Air cushion vehicle construction including control valves
US3127949A (en) * 1961-05-11 1964-04-07 Walter T Harter Ground effect machine with controls therefor
US3208543A (en) * 1961-07-19 1965-09-28 American Mach & Foundry Air cushion vehicle
US3243003A (en) * 1961-08-30 1966-03-29 Gen Delivery Ground effect machine
US3173507A (en) * 1962-04-17 1965-03-16 Lucas Industries Ltd Weighbridges
US3262510A (en) * 1962-06-04 1966-07-26 Alphons J Froehler Air cushion vehicle with lift, turn, and brake controls
US3322223A (en) * 1963-05-16 1967-05-30 William R Bertelsen Ground effect machines
US3292721A (en) * 1963-10-02 1966-12-20 Franklin A Dobson Toy air car
US3259097A (en) * 1964-07-10 1966-07-05 John Van Veldhuizen Air-propelled boat
US3401766A (en) * 1964-11-02 1968-09-17 Aircars Inc Air-cushion vehicle
US3486577A (en) * 1965-10-21 1969-12-30 Arthur M Jackes Axial flow ground effect machine
US3467213A (en) * 1966-08-17 1969-09-16 Dowty Rotol Ltd Gas turbine powered air-cushion vehicle with propulsive jet means

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3861491A (en) * 1972-12-14 1975-01-21 Hugo S Ferguson Air cushion vehicle
US3887030A (en) * 1972-12-15 1975-06-03 Christopher John Fitzgerald Duct systems for air cushion vehicles
US3869020A (en) * 1973-07-12 1975-03-04 Douglas W Holland Air cushioned vehicle
US4643268A (en) * 1982-04-05 1987-02-17 American Antigravity Co., Inc. Air lifted and propelled vehicle
WO1987000492A1 (en) * 1985-07-22 1987-01-29 Howell Murrell D Pitch controlled ground effect vehicle
US4666012A (en) * 1985-07-22 1987-05-19 Howell Murrell D Pitch controlled ground effect vehicle
US5042605A (en) * 1989-01-07 1991-08-27 Sorekkusu Kabushiki Kaisha Apparatus for controlling air cushion vehicle
US5097919A (en) * 1989-07-05 1992-03-24 Dowty Woodville Polymer Limited Surface effect vehicle
US5941331A (en) * 1992-02-13 1999-08-24 Gastesi; Ignacio Air cushion vehicle control system
US5738302A (en) * 1996-04-02 1998-04-14 Freeland; Verne L. Airborne vehicle
US20050095930A1 (en) * 2003-10-31 2005-05-05 Garcia Phillip P. System to propel an air powered boat
US7090549B2 (en) * 2003-10-31 2006-08-15 Garcia Phillip P System to propel an air powered boat
US7032698B2 (en) * 2003-11-12 2006-04-25 Mattel, Inc. Hovercraft
US20050194196A1 (en) * 2003-11-12 2005-09-08 Mattel, Inc. Hovercraft
WO2005047095A3 (en) * 2003-11-12 2006-02-16 Mattel Inc Hovercraft
US20060019556A1 (en) * 2004-07-26 2006-01-26 BALDWIN Charles Air-boat sound suppressor and directional control system
US7101235B2 (en) 2004-07-26 2006-09-05 BALDWIN Charles Air-boat sound suppressor and directional control system
US7717209B2 (en) 2006-12-22 2010-05-18 Pendzich Jerome S Vehicle with vertical lift
US20080149780A1 (en) * 2006-12-22 2008-06-26 Pendzich Jerome S Vertical lift vehicle
US7481290B2 (en) * 2006-12-22 2009-01-27 Pendzich Jerome S Vertical lift vehicle
US20090140103A1 (en) * 2006-12-22 2009-06-04 Jerome Pendzich Vehicle with vertical lift
WO2009068909A1 (en) * 2007-11-30 2009-06-04 Fergus Johnathan Ardern Hover dodgem
GB2467252A (en) * 2007-11-30 2010-07-28 Fergus Johnathan Ardern Hover dodgem
US20100300787A1 (en) * 2007-11-30 2010-12-02 Fergus Johnathan Ardern Hover dodgem
US20110266081A1 (en) * 2009-01-05 2011-11-03 Ivan Novikov-Kopp Method for comprehensively increasing aerodynamic and transport characteristics, a wing-in-ground-effect craft for carrying out said method (variants) and a method for realizing flight
US8657053B2 (en) * 2009-01-05 2014-02-25 Ivan Novikov-Kopp Method for comprehensively increasing aerodynamic and transport characteristics, a wing-in-ground-effect craft for carrying out said method (variants) and a method for realizing flight
US20160052503A1 (en) * 2014-08-25 2016-02-25 Cameron HOWELL Apparatus including user-platform assembly and air-thrusting assembly and method therefor
US10160435B2 (en) * 2015-10-14 2018-12-25 Foshan Quark Brother Technology Co., Ltd. Hovercraft using single ducted fan with vectoring propulsion

Also Published As

Publication number Publication date
BE761536A (fr) 1971-07-13
DE2101427A1 (de) 1971-07-22
SE371146B (enExample) 1974-11-11
FR2076103B1 (enExample) 1974-09-06
GB1332197A (en) 1973-10-03
FR2076103A1 (enExample) 1971-10-15

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