US3339657A - Wall device for bounding an air cushion - Google Patents

Wall device for bounding an air cushion Download PDF

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US3339657A
US3339657A US547633A US54763366A US3339657A US 3339657 A US3339657 A US 3339657A US 547633 A US547633 A US 547633A US 54763366 A US54763366 A US 54763366A US 3339657 A US3339657 A US 3339657A
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Prior art keywords
plate device
cushion
bearing surface
wall means
inner periphery
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US547633A
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Bertin Jean Henri
Faure Marc Henri Jean
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Bertin Technologies SAS
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Bertin et Cie SA
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion
    • B60V1/04Air-cushion wherein the cushion is contained at least in part by walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion
    • B60V1/16Flexible skirts

Definitions

  • This invention relates to vehicles supported by at least one pressure-fluid cushion, more particularly vehicles supported by several air cushions each of which is surrounded by a deformable wall made of solid material.
  • the invention relates generally to the obtaining of characteristic stability of a cushion during its dynamic operation, i.e., the elimination of instability resulting in the spontaneous vertical oscillation of the part of the vehicle disposed above the cushion and resting on it, and the entry into resonance of the cushion when the latter is subjected to periodic influences of the sort that occur during the movement of the vehicle at normal speed over undulating ground, land or water.
  • a vehicle with an air cushion has at least one composite envelope comprising two parts, a side wall advantageously sloping outwards towards the top and an annular support plate which is at least substantially flat and horizontal in the norm-a1 position, the side wall being articulated in a sealing-tight manner by its top edge to the outer circumference of the annular support plate and the latter likewise being articulated in a sealing-tight manner on the vehicle proper at its inner circumference and returned to the normal position by any resilient elements known in the field of suspension.
  • the resilient elements are preferably provided with shock absorbers.
  • the side wall and the support plate are advantageously made of materials that are inextensible under the action of the internal pressure of the supporting fluid cushion, so that variations in their external diameter and their local bending in elevation correspond to variations in the volume provided for the cushion which, if they are present at all, are at least negligible compared with the variations in the volume resulting from the movements of the support plate.
  • FIGURE 1 shows a half cross-section of an envelope defining an air cushion according to the invention in the normal operating position
  • FIGURE 2 shows the envelope in the temporarily raised position
  • FIGURES 3 and 4 are two views from below illustrating two modifications, respectively polygonal and circular, of the envelope in FIGURES 1 and 2.
  • FIG. 1 is a platform or the bottom of a vehicle supported by at least one pressure-fluid cushion 2.
  • the latter is fed in any appropriate known manner and I preferably independently of the other cushions, for ex-
  • the cushion is contained by a composite envelope, the structure of which forms the essential part of the invention.
  • This envelope generally designated 5, comprises mainly a side wall 50 and an annular plate 51 supporting this wall, which, seen in plan, has any closed form, for example a circular, rectangular or polygonal one.
  • This wall preferably slopes outwards towards the top, as shown in the drawings. It is made of a material which is inextensible but advantageously deformable, such as fabric coated to make it impermeable.
  • the annular plate 51 is also practically inextensible under the influence of the variations in the pressure of the cushion 2 defined by the composite envelope, but it can be deformed vertically so as to vary the volume of the cushion appropriately.
  • the perimeter of the connecting line of the wall 50 and the plate 51 may comprise several rigid, flat elements 51a, trapezoidal in plan, the radial edges of which have overlapping joints 51b.
  • Articulations or hinges are provided at 53 while the inner circumference of the elements 51a is connected to the platform El, or more exactly to the base of the feed conduit 4, by a diaphragm 52a made of a deformable and advantageously elastic material such as rubber.
  • a band seal 52b also made of rubber, can be associated with the hinges 53 (FIGURES l to 3).
  • the annular plate 51 comprises a simple diaphragm made of radially ribbed metal sheet and advantageously plastics-lined so as to make it stronger and diminish any vertical vibrations of the composite envelope 50, 51.
  • this plate can be secured to the conduit 4 so that it can be deformed vertically, and it may have yieldable connections akin to articulations 521) on its outer circumference.
  • the change of the plate to the position shown in FIGURE 2 (which corresponds to the highest accelerations applied to the platform 1 by its movement over uneven country) may cause its outer perimeter and also that of the wall 50 to be reduced, and this, coupled with its vertical deformation, will reduce the volume of the cushion 2 and temporarily increase the desired damping effect, in spite of the inevitable increase in volume in this case in which the skirt is relatively extensible.
  • Resilient elements 6 and shock absorbers 7 are advantageously disposed between the platform 1 and the plate 51 to keep the latter in a normally approximately horizontal position and prevent resonance due to the characteristic elasticity of the composite envelope made in this way.
  • the plan area defined by the bottom edge 50:: of the wall 50 is greater than the one defined by the articulations at 52a of the plate 51 on the platform.
  • the operation of a composite envelope as described compared with that of conventional inextensible skirts the top edges of which are directly secured to a platform, has the feature that any chance increase in the internal pressure of the fluid cushion 2 tends to act on the difference in the areas mentioned above and to raise the plate 51.
  • this is articulated to the platform along its inner circumference at 52a, it will be raised on the outer side, becoming deformed slightly as shown on FIGURE 2.
  • the volume of the cushion 2 is immediately reduced and the periodic movement of the platform that this pressure increase might cause is quickly diminished.
  • a chance reduction in pressure causes a relative lowering of the outer circumference of the plate 51 and the bottom edge 50a of the Wall 50.
  • the springs 6 and even the shock absorbers 7 can be replaced by light inflatable structures.
  • a pressure responsive, deformable plate device in the general shape of an annulus with an inner periphery adjacent said projected section of said protruding portion and an outer periphery adjacent said cushion confining wall means, said plate device extending to form a substantially fluidtight, cushion bounding physical wall on the side of said pressure fluid cushion opposite to said bearing surface whereby said pressure fluid .cushion is bounded endwise by said plate device and said bearing surface and sidewise by said confining wall means, said plate device being deflectable conical-wise upon exertion of pressure thereon with said outer periphery thereof moving bodily toward and away from said rigid structure while said inner periphery thereof remains in proximity to said projected section of said protruding portion, whereby said outer periphery of said plate device extends entirely on a same side of said inner periphery thereof,
  • second means for hingedly connecting said outer periphery of said plate device to said cushion confining wall means, whereby said wall means move bodily with respect to said inner periphery upon conical-wise deflection of said deformable plate device.
  • Movable body as claimed in claim 1 further comprising resilient return means extending between said rigid structure and said deformable plate device for urging the same to deflect conical-wise about said first hinge means toward said bearing surface.
  • Movable body as claimed in claim 2 further comprising damping means extending between said rigid structure and said deformable plate device and forming, in cooperation with said resilient return means, a suspension system for said cushion confining wall means and plate device hinged assembly on said rigid structure about said first hinge means.
  • said rigid protruding portion comprises a pressure fluid supply duct opening into the space bounded laterally by said cushion confining wall means and endwise by said plate device and said bearing surface, said duct being integral with said rigid structure and being hingedly connected to said plate device through said first means.
  • said cushion confining wall means comprises a skirt made of flaccid, fluidtight material and has a longitudinal outline which tapers toward said bearing surface.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Fluid-Damping Devices (AREA)
  • Mattresses And Other Support Structures For Chairs And Beds (AREA)
  • Vibration Prevention Devices (AREA)

Description

$ept.5,1967 J. H. BERTIN ETAL 3,339,657
WALL DEVICE FOR BOUNDING AN AIR CUSHION Filed May 4, 1966 Fig.: 1
United States Patent 9 Claims. for. 1807) This invention relates to vehicles supported by at least one pressure-fluid cushion, more particularly vehicles supported by several air cushions each of which is surrounded by a deformable wall made of solid material.
The invention relates generally to the obtaining of characteristic stability of a cushion during its dynamic operation, i.e., the elimination of instability resulting in the spontaneous vertical oscillation of the part of the vehicle disposed above the cushion and resting on it, and the entry into resonance of the cushion when the latter is subjected to periodic influences of the sort that occur during the movement of the vehicle at normal speed over undulating ground, land or water.
Theoretical studies carried out by the applicants show that the volume of the cushion and the law of the variation of that volume under the influence of the variations of the pressure of the cushion are essential parameters of the dynamic stability of the vehicle borne by the cushion.
It was found to be very desirable to have an air cushion bounded by means defining by the cushion an internal volume which was variable in inverse proportion to the pressure of the gas contained in that volume, and this invention relates particularly to such an arrangement.
According to the invention, a vehicle with an air cushion has at least one composite envelope comprising two parts, a side wall advantageously sloping outwards towards the top and an annular support plate which is at least substantially flat and horizontal in the norm-a1 position, the side wall being articulated in a sealing-tight manner by its top edge to the outer circumference of the annular support plate and the latter likewise being articulated in a sealing-tight manner on the vehicle proper at its inner circumference and returned to the normal position by any resilient elements known in the field of suspension. The resilient elements are preferably provided with shock absorbers.
The side wall and the support plate are advantageously made of materials that are inextensible under the action of the internal pressure of the supporting fluid cushion, so that variations in their external diameter and their local bending in elevation correspond to variations in the volume provided for the cushion which, if they are present at all, are at least negligible compared with the variations in the volume resulting from the movements of the support plate.
The invention will now be described with reference to the accompanying drawings, in which:
FIGURE 1 shows a half cross-section of an envelope defining an air cushion according to the invention in the normal operating position;
FIGURE 2 shows the envelope in the temporarily raised position, and
FIGURES 3 and 4 are two views from below illustrating two modifications, respectively polygonal and circular, of the envelope in FIGURES 1 and 2.
In the drawings 1 is a platform or the bottom of a vehicle supported by at least one pressure-fluid cushion 2. The latter is fed in any appropriate known manner and I preferably independently of the other cushions, for ex- The cushion is contained by a composite envelope, the structure of which forms the essential part of the invention. This envelope, generally designated 5, comprises mainly a side wall 50 and an annular plate 51 supporting this wall, which, seen in plan, has any closed form, for example a circular, rectangular or polygonal one. This wall preferably slopes outwards towards the top, as shown in the drawings. It is made of a material which is inextensible but advantageously deformable, such as fabric coated to make it impermeable.
The annular plate 51 is also practically inextensible under the influence of the variations in the pressure of the cushion 2 defined by the composite envelope, but it can be deformed vertically so as to vary the volume of the cushion appropriately. In the ordinary case in which the perimeter of the connecting line of the wall 50 and the plate 51 does not vary, the latter may comprise several rigid, flat elements 51a, trapezoidal in plan, the radial edges of which have overlapping joints 51b. Articulations or hinges are provided at 53 while the inner circumference of the elements 51a is connected to the platform El, or more exactly to the base of the feed conduit 4, by a diaphragm 52a made of a deformable and advantageously elastic material such as rubber. A band seal 52b, also made of rubber, can be associated with the hinges 53 (FIGURES l to 3).
In a modification shown in FIGURE 4, the annular plate 51 comprises a simple diaphragm made of radially ribbed metal sheet and advantageously plastics-lined so as to make it stronger and diminish any vertical vibrations of the composite envelope 50, 51.
If desired, this plate can be secured to the conduit 4 so that it can be deformed vertically, and it may have yieldable connections akin to articulations 521) on its outer circumference. In this case, if it is flat in the normal position (FIGURE 1), the change of the plate to the position shown in FIGURE 2 (which corresponds to the highest accelerations applied to the platform 1 by its movement over uneven country) may cause its outer perimeter and also that of the wall 50 to be reduced, and this, coupled with its vertical deformation, will reduce the volume of the cushion 2 and temporarily increase the desired damping effect, in spite of the inevitable increase in volume in this case in which the skirt is relatively extensible.
Resilient elements 6 and shock absorbers 7 are advantageously disposed between the platform 1 and the plate 51 to keep the latter in a normally approximately horizontal position and prevent resonance due to the characteristic elasticity of the composite envelope made in this way.
The plan area defined by the bottom edge 50:: of the wall 50 is greater than the one defined by the articulations at 52a of the plate 51 on the platform. In these conditions, the operation of a composite envelope as described, compared with that of conventional inextensible skirts the top edges of which are directly secured to a platform, has the feature that any chance increase in the internal pressure of the fluid cushion 2 tends to act on the difference in the areas mentioned above and to raise the plate 51. As this is articulated to the platform along its inner circumference at 52a, it will be raised on the outer side, becoming deformed slightly as shown on FIGURE 2. As a result, the volume of the cushion 2 is immediately reduced and the periodic movement of the platform that this pressure increase might cause is quickly diminished. Conversely, a chance reduction in pressure causes a relative lowering of the outer circumference of the plate 51 and the bottom edge 50a of the Wall 50.
The embodiment which has just been described can, of course, be modified, for example by the substitution of equivalent technical means. For example, the plate 51,
the springs 6 and even the shock absorbers 7 can be replaced by light inflatable structures.
What is claimed is:
1. A ground effect machine movable along a bearing surface and comprising a rigid structure having a side facing said bearing surface and including a rigid portion protruding from said structure toward said bearing surface and fixedly secured to said rigid structure with a projected section spaced from said side, and wall means for confining laterally a pressure fluid cushion formed against said bearing surface, wherein the improvement comprises a system for supporting said cushion confining wall means relatively to said protruding portion, comprising:
a pressure responsive, deformable plate device in the general shape of an annulus with an inner periphery adjacent said projected section of said protruding portion and an outer periphery adjacent said cushion confining wall means, said plate device extending to form a substantially fluidtight, cushion bounding physical wall on the side of said pressure fluid cushion opposite to said bearing surface whereby said pressure fluid .cushion is bounded endwise by said plate device and said bearing surface and sidewise by said confining wall means, said plate device being deflectable conical-wise upon exertion of pressure thereon with said outer periphery thereof moving bodily toward and away from said rigid structure while said inner periphery thereof remains in proximity to said projected section of said protruding portion, whereby said outer periphery of said plate device extends entirely on a same side of said inner periphery thereof,
first means for hingedly connecting said inner periphery of said plate device to said projected section of said protruding portion in spaced relationship with said rigid structure whereby said plate device is deflectable conical-wise to adopt generally V-shaped cross sections of varying angular extents, and
second means for hingedly connecting said outer periphery of said plate device to said cushion confining wall means, whereby said wall means move bodily with respect to said inner periphery upon conical-wise deflection of said deformable plate device.
2. Movable body as claimed in claim 1, further comprising resilient return means extending between said rigid structure and said deformable plate device for urging the same to deflect conical-wise about said first hinge means toward said bearing surface.
3. Movable body as claimed in claim 2, further comprising damping means extending between said rigid structure and said deformable plate device and forming, in cooperation with said resilient return means, a suspension system for said cushion confining wall means and plate device hinged assembly on said rigid structure about said first hinge means.
4. Movable body as claimed in claim 1, wherein at least one of said first and second hinged connecting means comprises a flexible strip of fluidtight material extending peripherally of said plate device to ensure fluidtight hinged connection thereof.
5. Movable body as claimed in claim 1, wherein said plate device comprises a plurality of rigid elements in edgewise overlapping relation.
6. Movable body as claimed in claim 1, wherein said rigid protruding portion comprises a pressure fluid supply duct opening into the space bounded laterally by said cushion confining wall means and endwise by said plate device and said bearing surface, said duct being integral with said rigid structure and being hingedly connected to said plate device through said first means.
7. Movable body as claimed in claim 1, wherein said cushion confining wall means comprises a skirt made of flaccid, fluidtight material and has a longitudinal outline which tapers toward said bearing surface.
8. Movable body as claimed in claim 1, wherein said plate device extends, in a normal position thereof, in a plane generally containing both said inner periphery and said outer periphery thereof and is deflectable conicalwise bodily on one side or bodily on the other side of said plane from said normal position thereof.
9. Movable body as claimed in claim 8, wherein said plate device, when in said normal position thereof, extends substantially parallel to said bearing surface.
References Cited UNITED STATES PATENTS 3,119,598 1/1964- Petersen et al. -7X 3,185,240 5/1965 Eggington et al 1807 3,209,848 10/1965 Holloway a- 180-7 3,233,692 2/1966 Guienne 180-7 3,260,322 7/1966 Mackie 180-7 FOREIGN PATENTS 80,047 1/ 1963 France.
A. HARRY LEVY, Primary Examiner.

Claims (1)

1. A GROUND EFFECT MACHINE MOVABLE ALONG A BEARING SURFACE AND COMPRISING A RIGID STRUCTURE HAVING A SIDE FACING SAID BEARING SURFACE AND INCLUDING A RIGID PORTION PROTRUDING FROM SAID STRUCTURE TOWARD SAID BEARING SURFACE AND FIXEDLY SECURED TO SAID RIGID STRUCTURE WIHT A PROJECTED SECTION SPACED FROM SAID SIDE, AND WALL MEANS FOR CONFINING LATERALLY A PRESSURE FLUID CUSHION FORMED AGAINST SAID BEARING SURFACE, WHEREIN THE IMPROVEMENT COMPRISES A SYSTEM FOR SUPPORTING SAID CUSHION CONFINING WALL MEANS RELATIVELY TO SAID PROTRUDING PORTION, COMPRISING: A PRESSURE RESPONSIVE, DEFORMABLE PLATE DEVICE IN THE GENERALLY SHAPE OF AN ANNULUS WITH AN INNER PERIPHERY ADJACNET SAID PROJECTED SECTION OF SAID PROTRUDING PORTION AND AN OUTER PERIPHERY ADJACENT SAID CUSHION CONFINING WALL MEANS, SAID PLATE DEVICE EXTENDING TO FROM A SUBSTANTIALLY FLUIDTIGHT, CUSHION BOUNDING PHYSICAL WALL ON THE SIDE OF SAID PRESSURE FLUID CUSHION OPPOSITE TO SAID BEARING SURFACE WHEREBY SAID PRESSURE FLUID CUSHION IS BOUNDED ENDWISE BY SAID PLATE DEVICE AND SAID BEARING SURFACE AND SIDEWISE BY SAID CONFINING WALL MEANS, SAID PLATE DEVICE BEING DEFLECTABLE CONICAL-WISE UPON EXERTION OF PRESSURE THEREON WITH SAID OUTER PERIPHERY THEREOF MOVING BODILY TOWARD AND AWAY FROM SAID RIGID STRUCTURE WHILE SAID INNER PERIPHERY THEREOF REMAINS IN PROXIMITY TO SAID PROJECTED SECTION OF SAID PROTRUDING PORTION, WHEREBY SAID OUTER PERIPHERY OF SAID PLATE DEVICE EXTENDS ENTIRELY ON A SAME SIDE OF SAID INNER PERIPHERY THEREOF, FIRST MEANS FOR HINGEDLY CONNECTING SAID INNER PERIPHERY OF SAID PLATE DEVICE TO SAID PROJECTED SECTION OF SAID PROTRUDING PORTION IN SPACED RELATIONSHIP WITH SAID RIGID STRUCTURE WHEREBY SAID PLATE DEVICE IS DEFLECTABLE CONICAL-WISE TO ADOPT GENERALLY V-SHAPED CROSS SECTIONS OF VARYING ANGULAR EXTENTS, AND SECOND MEANS FOR HINGEDLY CONNECTING SAID OUTER PERIPHERY OF SAID PLATE DEVICE TO SAID CUSHION CONFINING WALL MEANS, WHEREBY SAID WALL MEANS MOVE BODILY WITH RESPECT TO SAID INNER PERIPHERY UPON CONICAL-WISE DEFLECTION OF SAID DEFORMABLE PLATE DEVICE.
US547633A 1965-05-07 1966-05-04 Wall device for bounding an air cushion Expired - Lifetime US3339657A (en)

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FR16284A FR1442531A (en) 1965-05-07 1965-05-07 Improvement to the walls used to delimit an air cushion

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FR (1) FR1442531A (en)
GB (1) GB1150162A (en)
OA (1) OA01959A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3444951A (en) * 1966-06-15 1969-05-20 Hovercraft Dev Ltd Plural cushion load transporter device
US3463264A (en) * 1966-07-15 1969-08-26 Bertin & Cie Bellows type fluid cushion confining device for surface effect machines
US3608664A (en) * 1968-05-08 1971-09-28 British Hovencraft Corp Ltd Cushion barriers for air cushion vehicles
US3625157A (en) * 1968-06-24 1971-12-07 Tracked Hovercraft Ltd Gas cushion load-supporting device
US3643757A (en) * 1968-05-09 1972-02-22 Aeroglisseurs Marins Flexible skirts for surface-effect machines
US3804197A (en) * 1970-01-26 1974-04-16 Bertin & Cie Fluid-cushion-containing facility for ground effect machine
US3908785A (en) * 1972-02-16 1975-09-30 Jack F Vaughen Air cushion conveyances
US20040244633A1 (en) * 2003-05-08 2004-12-09 Witmer Warner H. Cats-constrained airplane transportation system

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR80047E (en) * 1961-06-30 1963-03-01 Bertin Et Cie Soc Ground Effect Flying Platforms Improvements
US3119598A (en) * 1962-08-28 1964-01-28 Douglas Aircraft Co Inc Air film supported weighing jack
US3185240A (en) * 1962-01-25 1965-05-25 Vickers Armstrongs Ltd Air-cushion borne vehicles
US3209848A (en) * 1961-07-19 1965-10-05 American Mach & Foundry Air cushion vehicle
US3233692A (en) * 1962-10-27 1966-02-08 Bertin & Cie Gas supply apparatus for ground-effect platforms with multiple air cushions
US3260322A (en) * 1962-01-10 1966-07-12 Gen Motors Corp Multiple pad air cushion support

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB935825A (en) * 1958-09-01 1963-09-04 Hovercraft Dev Ltd Improvements in or relating to vehicles for travelling over land and/or water
US3170530A (en) * 1961-03-23 1965-02-23 Richard W Black Mobile air supported vehicle
NL299079A (en) * 1962-10-18 1900-01-01
FR1371776A (en) * 1963-01-24 1964-09-11 Vickers Armstrongs Ltd Improvements to vehicles moving on air cushions

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR80047E (en) * 1961-06-30 1963-03-01 Bertin Et Cie Soc Ground Effect Flying Platforms Improvements
US3209848A (en) * 1961-07-19 1965-10-05 American Mach & Foundry Air cushion vehicle
US3260322A (en) * 1962-01-10 1966-07-12 Gen Motors Corp Multiple pad air cushion support
US3185240A (en) * 1962-01-25 1965-05-25 Vickers Armstrongs Ltd Air-cushion borne vehicles
US3119598A (en) * 1962-08-28 1964-01-28 Douglas Aircraft Co Inc Air film supported weighing jack
US3233692A (en) * 1962-10-27 1966-02-08 Bertin & Cie Gas supply apparatus for ground-effect platforms with multiple air cushions

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3444951A (en) * 1966-06-15 1969-05-20 Hovercraft Dev Ltd Plural cushion load transporter device
US3463264A (en) * 1966-07-15 1969-08-26 Bertin & Cie Bellows type fluid cushion confining device for surface effect machines
US3608664A (en) * 1968-05-08 1971-09-28 British Hovencraft Corp Ltd Cushion barriers for air cushion vehicles
US3643757A (en) * 1968-05-09 1972-02-22 Aeroglisseurs Marins Flexible skirts for surface-effect machines
US3625157A (en) * 1968-06-24 1971-12-07 Tracked Hovercraft Ltd Gas cushion load-supporting device
US3804197A (en) * 1970-01-26 1974-04-16 Bertin & Cie Fluid-cushion-containing facility for ground effect machine
US3908785A (en) * 1972-02-16 1975-09-30 Jack F Vaughen Air cushion conveyances
US20040244633A1 (en) * 2003-05-08 2004-12-09 Witmer Warner H. Cats-constrained airplane transportation system

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DE1290436B (en) 1969-03-06
GB1150162A (en) 1969-04-30
FR1442531A (en) 1966-06-17
OA01959A (en) 1970-02-04

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