US3561559A - Skirting system for surface effect machine - Google Patents
Skirting system for surface effect machine Download PDFInfo
- Publication number
- US3561559A US3561559A US728726A US3561559DA US3561559A US 3561559 A US3561559 A US 3561559A US 728726 A US728726 A US 728726A US 3561559D A US3561559D A US 3561559DA US 3561559 A US3561559 A US 3561559A
- Authority
- US
- United States
- Prior art keywords
- diaphragm means
- points
- diaphragm
- support structure
- bearing surface
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/16—Flexible skirts
Definitions
- PATENTEUFEB slam 3561 559 SHEET 1 0r 4 PATENTEDFEB' slam 3.561.559
- the present invention relates to improvements to the flexible skirt devices used for bounding pressurized fluid cushions in ground-effect machines, more particularly the lobated or multilobed skirts, an embodiment of which is illustrated in FIG. 6 of U5. Pat. No. 3,346,063.
- One of the objects of the invention is to provide a means of retaining a flexible skirt of the kind specified.
- Other objects of the invention are to counteract to some extent the natural tendency of flexible skirts to assume a circular shape as a result of the internal pressure exerted on the skirts, and to give the skirts a shape which causes only low aerodynamic and hydrodynamic drag, and also to make the skirts more readily fittable to the structure of the machine.
- Another object of the invention is to ensure that the internal stresses are uniformly distributed throughout the material of the skirt.
- the present invention obviates the folds in the peripheral skirt, gives it a greater flexibility, and brings the internal elementary cushions closer to one another.
- the present invention applies the principle of the so-called suspended bridge, to ensure that at the place where the skirt is lobed, forces are distributed uniformly by a parabolic definition, thus reducing strains and risks of breakages.
- the lobes of a multilobed flexible skirt are connected by a diaphragm, such as a canvas, which is only partly continuous, since it is cut away over a predetermined curve, and which is attached on the one hand to the skirt at the cuspidal edge junction of its lobes, and on the other hand to the skirt support.
- a diaphragm such as a canvas
- the diaphragm is cut away over a single or multiple parabolic curve extending between two points of attachment to the support.
- the curve can take a catenary form.
- FIG. 1 is a diagrammatic perspective view of a two-lobe skirt having a cutaway diaphragm according to the present invention
- FIGS. 2-4 are diagrams showing different shapesin which the diaphragm may be cutaway
- FIG. 5 is a diagrammatic perspective view of a multilobe and multidiaphragm skirt
- FIG. 6 shows an adaptation of the diaphragm to a machine of the peripheral fluid curtain type
- FIG. 7 illustrates an arrangement of the fetaining diaphragms of a multilobed peripheral skirt
- FIG. 8 is a diagrammatic vertical half-section showing a variant method of attachment.
- FIGS. 9 and 10 illustrate another variant embodiment.
- FIG. 1 shows a flexible skirt 1 laterally boundinga pressurized fluid cushion and having two frustoconical lobes 2, 3 which, viewed in plan, take the form of incomplete circles joined in a plane of intersection which will in general be perpendicular to the extension of the free edge of the skirts and which comprises an axis A-A extending through the chord of intersection, and a central axis B-B substantially perpendicular to the axis A-A, the third axis C-C being parallel to the central longitudinal plane of the ground-effect machine, for instance an air-cushion vehicle.
- the skirt 1 is retained by means of a canvas or diaphragm 4 cut away over an outline 5 to be defined hereinafter.
- the partly continuous diaphragm is rigidly connected to the skirt 1 along two generatrices or cuspidal edges 6, 6, at the intersection of the lobes 2, 3.
- the diaphragm is attached to the support (not shown), which can be the platform of the vehicle, at two upper points 7, 7 disposed on the transverse axis A-A, and at a lower point 8 disposed on the axis B-B.
- FIG. 2 is a partial section, taken along the transverse plane AABB of FIG. 1. and shows more clearly the shape of the cutaway portion 5 of the diaphragm 4.
- the curve takes the form of a parabola having an axis X-X and its apex at the point 9.
- the point 9 can be brought to a place III on the edge 6, as shown in FIG. 3, the internal edge 5 of the diaphragm 4 still maintaining a parabolic outline.
- the internal edge 5 can take a catenary shape.
- FIG. 5 shows the application of retaining diaphragms 4 to a skirt 11 having six lobes; the skirt can either be an internal elementary skirt, or a peripheral enveloping skirt. Since the assembly is symmetrical about the axis 8-3, the lower point 8 of attachment will be shared by the three diaphragms 4, while three pairs of upper points 7, 7 of attachment will be provided.
- the retaining diaphragm according to the invention is applicable not only to cushions of the so-called plenum chamber type, as described hereinbefore, but also to cushions of the peripheral fluid curtain type.
- FIG. 6 illustrates an application of this kind.
- the nozzle 13 for forming the fluid curtain 12 is shown between the inner 14 and outer 15 edges of the peripheral curtain; the edges 14, 15 can be connected by tie rods or cables 16, 16, or by a suitably profiled radial struttingcanvas.
- FIG. 7 shows a preferred embodiment of the invention, applied to a multilobed skirt enclosing; a plurality of downwardly tapering frustoconical internal elementary skirts J aligned in two rows parallel with the longitudinal axis C-C on either side thereof.
- three dihedrally-paired retaining diaphragms 4 are provided; the paired canvasses of one diaphragm are not in the continuation of one another, but at a certain relative inclination, as can be clearly seen in FIG. 7, cables or tie rods 18 ensuring that the relative inclination is maintained.
- FIG. 7 again shows the upper points 7, 7 of attachment shown in FIG. 1, but the lower attachment is now at two points 19a, 19b which could be disposed in the central longitudinal plane B-BC-C, but are in fact at a distance therefrom.
- FIG. 8 clearly illustrates an arrangement of this kind. It can be seen that points l9a l9b of attachment are connected via tie rods 20, 21 to the axis 8-8 by the agency of any suitable mechanism.
- FIG. 8 shows a conical member 22 attached to the floor 23 of the apparatus. This conical member 22 acts as a hanging attachment to a first clevislike connecting member 24 from which a connection 25 terminating in a ring 26 is suspended. In all cases, the outline 5a, 5b is parabolic.
- the required parabolic outline can be determined by means of a steel or glass wire or cable 27 (cf. FIGS. 9 and 10) tensioned by the canvas diaphragm 4 and transmitting the forces to attachments 7, 8.
- the canvas diaphragm 4 must adhere to the wires 27 so that it can be loaded. thereby; this can be done by the interposition of a moulded channel 28 which adheres both to the diaphragm 4 and the wire 27.
- a surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface, said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane, and further means for attaching said diaphragm means to said support structure at two tiered points of said diaphragm means, both lying intermediate to and at a lower level than said two upper points, said further means comprising an attachment member secured to said support structure and positioned in said longitudinal medial plane
- said diaphragm means has a cutout portion of curved outline composed of two arcuate sections interconnected at a point of inflection which is said uppermost one of said two tiered points and which is attached to said first tie.
- a surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface.
- said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane.
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Mechanical Engineering (AREA)
- Diaphragms And Bellows (AREA)
- Tents Or Canopies (AREA)
Abstract
A multilobed flexible skirt device for a surface effect machine, comprising a flexible diaphragm, such as a canvas, connecting the lobes of the skirt, the diaphragm being only partly continuous, since it is cut away over a predetermined curve, and being attached on the one hand to the skirt at the cuspidal edge junctions of its lobes and on the other hand to the skirt support structure of the machine.
Description
United States Patent lnventor Appl. No.
Filed Patented Assignee v Priority Guy Robert Delamare llerblay, France May 13, 1968 Feb. 9, 1971 Societe DEtudes Et De Developpement Des Aeroglisseurs Marins S.E.D.A.M. Paris, France a company of France May 18, 1967 France SKIRTING SYSTEM FOR SURFACE EFFECT MACHINE 3 Claims, 10 Drawing Figs.
Int. Cl B60v H16 [50] Field of Search 180/127,
[56] References Cited UNITED STATES PATENTS 3,414,075 12/1968 Bertin 180/121 3,416,627 12/1968 Francis et a1. 180/127 Primary Examiner--A. Harry Levy Attorney-Stevens, Davis, Miller & Mosher ABSTRACT: A multilobed flexible skirt device for a surface effect machine, comprising a flexible diaphragm, such as a canvas, connecting the lobes of the skirt, the diaphragm being only partly continuous, since it is cut away over a predetermined curve, and being attached on. the one hand to the skirt at the cuspidal edge junctions of its lobes and on the other hand to the skirt support structure of the machine.
PATENTEUFEB slam 3561 559 SHEET 1 0r 4 PATENTEDFEB' slam 3.561.559
SHEET u 0F 4 I Fig-'8 4 7 B 23 SKIRTING SYSTEM FOR SURFACE EFFECT MACHINE The present invention relates to improvements to the flexible skirt devices used for bounding pressurized fluid cushions in ground-effect machines, more particularly the lobated or multilobed skirts, an embodiment of which is illustrated in FIG. 6 of U5. Pat. No. 3,346,063.
One of the objects of the invention is to provide a means of retaining a flexible skirt of the kind specified. Other objects of the invention are to counteract to some extent the natural tendency of flexible skirts to assume a circular shape as a result of the internal pressure exerted on the skirts, and to give the skirts a shape which causes only low aerodynamic and hydrodynamic drag, and also to make the skirts more readily fittable to the structure of the machine.
Another object of the invention is to ensure that the internal stresses are uniformly distributed throughout the material of the skirt.
In the case of a peripheral skirt enclosing a plurality of internal elementary cushions (another embodiment disclosed in the aforementioned patent), the present invention obviates the folds in the peripheral skirt, gives it a greater flexibility, and brings the internal elementary cushions closer to one another.
It has already been suggested to stabilize the lobes of a mu]- tilobed skirt by cables or chains connected to the skirt support, or by continuous or solid partitions. However, embodiments of this kind either cause high local concentrations of stresses in the skirt, leading to breakages of the canvas, or produce prohibitive conditions of weight.
The present invention applies the principle of the so-called suspended bridge, to ensure that at the place where the skirt is lobed, forces are distributed uniformly by a parabolic definition, thus reducing strains and risks of breakages.
According to the present invention, the lobes of a multilobed flexible skirt are connected by a diaphragm, such as a canvas, which is only partly continuous, since it is cut away over a predetermined curve, and which is attached on the one hand to the skirt at the cuspidal edge junction of its lobes, and on the other hand to the skirt support.
In one embodiment of the invention, the diaphragm is cut away over a single or multiple parabolic curve extending between two points of attachment to the support. As avariant, the curve can take a catenary form.
In the accompanying drawings:
FIG. 1 is a diagrammatic perspective view of a two-lobe skirt having a cutaway diaphragm according to the present invention;
FIGS. 2-4 are diagrams showing different shapesin which the diaphragm may be cutaway;
FIG. 5 is a diagrammatic perspective view of a multilobe and multidiaphragm skirt;
FIG. 6 shows an adaptation of the diaphragm to a machine of the peripheral fluid curtain type;
FIG. 7 illustrates an arrangement of the fetaining diaphragms of a multilobed peripheral skirt;
FIG. 8 is a diagrammatic vertical half-section showing a variant method of attachment; and
FIGS. 9 and 10 illustrate another variant embodiment.
FIG. 1 shows a flexible skirt 1 laterally boundinga pressurized fluid cushion and having two frustoconical lobes 2, 3 which, viewed in plan, take the form of incomplete circles joined in a plane of intersection which will in general be perpendicular to the extension of the free edge of the skirts and which comprises an axis A-A extending through the chord of intersection, and a central axis B-B substantially perpendicular to the axis A-A, the third axis C-C being parallel to the central longitudinal plane of the ground-effect machine, for instance an air-cushion vehicle.
According to the present invention, the skirt 1 is retained by means of a canvas or diaphragm 4 cut away over an outline 5 to be defined hereinafter. The partly continuous diaphragm is rigidly connected to the skirt 1 along two generatrices or cuspidal edges 6, 6, at the intersection of the lobes 2, 3. The diaphragm is attached to the support (not shown), which can be the platform of the vehicle, at two upper points 7, 7 disposed on the transverse axis A-A, and at a lower point 8 disposed on the axis B-B.
FIG. 2 is a partial section, taken along the transverse plane AABB of FIG. 1. and shows more clearly the shape of the cutaway portion 5 of the diaphragm 4. In this embodiment. in which the skirt 1 has two frustoconical lobes 2, 3, the curve takes the form of a parabola having an axis X-X and its apex at the point 9. However, with different operation of the pressure inside the cushion, different shape of the skirt, etc., the point 9 can be brought to a place III on the edge 6, as shown in FIG. 3, the internal edge 5 of the diaphragm 4 still maintaining a parabolic outline. In the variant shown in FIG. 4, the internal edge 5 can take a catenary shape.
FIG. 5 shows the application of retaining diaphragms 4 to a skirt 11 having six lobes; the skirt can either be an internal elementary skirt, or a peripheral enveloping skirt. Since the assembly is symmetrical about the axis 8-3, the lower point 8 of attachment will be shared by the three diaphragms 4, while three pairs of upper points 7, 7 of attachment will be provided.
The retaining diaphragm according to the invention is applicable not only to cushions of the so-called plenum chamber type, as described hereinbefore, but also to cushions of the peripheral fluid curtain type. FIG. 6 illustrates an application of this kind. The nozzle 13 for forming the fluid curtain 12 is shown between the inner 14 and outer 15 edges of the peripheral curtain; the edges 14, 15 can be connected by tie rods or cables 16, 16, or by a suitably profiled radial struttingcanvas.
FIG. 7 shows a preferred embodiment of the invention, applied to a multilobed skirt enclosing; a plurality of downwardly tapering frustoconical internal elementary skirts J aligned in two rows parallel with the longitudinal axis C-C on either side thereof.
In the embodiment illustrated, three dihedrally-paired retaining diaphragms 4 are provided; the paired canvasses of one diaphragm are not in the continuation of one another, but at a certain relative inclination, as can be clearly seen in FIG. 7, cables or tie rods 18 ensuring that the relative inclination is maintained.
FIG. 7 again shows the upper points 7, 7 of attachment shown in FIG. 1, but the lower attachment is now at two points 19a, 19b which could be disposed in the central longitudinal plane B-BC-C, but are in fact at a distance therefrom.
FIG. 8 clearly illustrates an arrangement of this kind. It can be seen that points l9a l9b of attachment are connected via tie rods 20, 21 to the axis 8-8 by the agency of any suitable mechanism. FIG. 8 shows a conical member 22 attached to the floor 23 of the apparatus. This conical member 22 acts as a hanging attachment to a first clevislike connecting member 24 from which a connection 25 terminating in a ring 26 is suspended. In all cases, the outline 5a, 5b is parabolic.
The required parabolic outline can be determined by means of a steel or glass wire or cable 27 (cf. FIGS. 9 and 10) tensioned by the canvas diaphragm 4 and transmitting the forces to attachments 7, 8. The canvas diaphragm 4 must adhere to the wires 27 so that it can be loaded. thereby; this can be done by the interposition of a moulded channel 28 which adheres both to the diaphragm 4 and the wire 27.
Iclaim:
1. A surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface, said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane, and further means for attaching said diaphragm means to said support structure at two tiered points of said diaphragm means, both lying intermediate to and at a lower level than said two upper points, said further means comprising an attachment member secured to said support structure and positioned in said longitudinal medial plane in spaced relation with said two tiered points, a first tie extending between the uppermost one of said two tiered points and said attachment member, a spacer member depending from said attachment member and having a lower end, and a second tie extending between the lowermost one of said two tiered points and said lower end of said spacer member.
2. Machine as claimed in claim I, wherein said diaphragm means has a cutout portion of curved outline composed of two arcuate sections interconnected at a point of inflection which is said uppermost one of said two tiered points and which is attached to said first tie.
3. A surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface. said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane. and further means for attaching said diaphragm means to said support structure at a third point of said diaphragm means lying intermediate to and at a lower level than said two upper points, said third point being spaced from a transverse plane through said straight line and orthogonal to said longitudinal medial plane, and said diaphragm means being of dihedral shape.
Claims (3)
1. A surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface, said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane, and further means for attaching said diaphragm means to said support structure at two tiered points of said diaphragm means, both lying intermediate to and at a lower level than said two upper points, said further means comprising an attachment member secured to said support structure and positioned in said longitudinal medial plane in spaced relation with said two tiered points, a first tie extending between the uppermost one of said two tiered points and said attachment member, a spacer member depending from said attachment member and having a lower end, and a second tie extending between the lowermost one of said two tiered points and said lower end of said spacer member.
2. Machine as claimed in claim 1, wherein said diaphragm means has a cutout portion of curved outline composed of two arcuate sections interconnected at a point of inflection which is said uppermost one of said two tiered points and which is attached to said first tie.
3. A surface effect machine movable above a generally horizontal bearing surface and having a longitudinal medial plane orthogonal to said bearing surface, said machine comprising a support structure spaced above said bearing surface and generally parallel thereto, and a lobated flexible skirting device depending from said structure and including an outer skirt defining juxtaposed lobes joined along cuspidal edges, and an inner diaphragm means interconnecting said cuspidal edges and attached thereto, said diaphragm means being only partly solid and having a cutout portion of curved outline, wherein the improvement comprises: means for attaching said diaphragm means to said support structure at two spaced upper points of said diaphragm means lying on a straight line substantially perpendicular to said longitudinal medial plane, and further means for attaching said diaphragm means to said support structure at a third point of said diaphragm means lying intermediate to and at a lower level than said two upper points, said third point being spaced from a transverse plane through said straight line and orthogonal to said longitudinal medial plane, and said diaphragm means being of dihedral shape.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR106832A FR1532422A (en) | 1967-05-18 | 1967-05-18 | Skirting device for ground effect vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
US3561559A true US3561559A (en) | 1971-02-09 |
Family
ID=8631040
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US728726A Expired - Lifetime US3561559A (en) | 1967-05-18 | 1968-05-13 | Skirting system for surface effect machine |
Country Status (4)
Country | Link |
---|---|
US (1) | US3561559A (en) |
DE (1) | DE1756368B1 (en) |
FR (1) | FR1532422A (en) |
GB (1) | GB1228981A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3887030A (en) * | 1972-12-15 | 1975-06-03 | Christopher John Fitzgerald | Duct systems for air cushion vehicles |
US3951227A (en) * | 1974-01-04 | 1976-04-20 | Societe D'etudes Et De Developpement Des Aeroglisseurs Marins, Terrestres Et Amphibies S.E.D.A.M. | Ground-effect vehicles |
US4060147A (en) * | 1975-02-18 | 1977-11-29 | Bertin & Cie | Vehicles riding on air cushions |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3414075A (en) * | 1961-06-30 | 1968-12-03 | Bertin & Cie | Flexible skirting system for surface effect machines |
US3416627A (en) * | 1965-09-22 | 1968-12-17 | British Hovercraft Corp Ltd | Flexible skirts for air cushion borne vehicles |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1089395A (en) * | 1964-03-11 | 1967-11-01 | British Hovercraft Corp Ltd | Improvements in or relating to air-cushion borne vehicles |
FR1421301A (en) * | 1964-04-20 | 1965-12-17 | Bertin & Cie | Ground Effect Flying Platforms Improvements |
FR1421331A (en) * | 1964-07-07 | 1965-12-17 | Bertin & Cie | Advanced soft skirt for air cushion vehicle |
-
1967
- 1967-05-18 FR FR106832A patent/FR1532422A/en not_active Expired
-
1968
- 1968-05-13 US US728726A patent/US3561559A/en not_active Expired - Lifetime
- 1968-05-14 DE DE19681756368 patent/DE1756368B1/en not_active Withdrawn
- 1968-05-15 GB GB1228981D patent/GB1228981A/en not_active Expired
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3414075A (en) * | 1961-06-30 | 1968-12-03 | Bertin & Cie | Flexible skirting system for surface effect machines |
US3416627A (en) * | 1965-09-22 | 1968-12-17 | British Hovercraft Corp Ltd | Flexible skirts for air cushion borne vehicles |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3887030A (en) * | 1972-12-15 | 1975-06-03 | Christopher John Fitzgerald | Duct systems for air cushion vehicles |
US3951227A (en) * | 1974-01-04 | 1976-04-20 | Societe D'etudes Et De Developpement Des Aeroglisseurs Marins, Terrestres Et Amphibies S.E.D.A.M. | Ground-effect vehicles |
US4060147A (en) * | 1975-02-18 | 1977-11-29 | Bertin & Cie | Vehicles riding on air cushions |
Also Published As
Publication number | Publication date |
---|---|
DE1756368B1 (en) | 1970-11-26 |
FR1532422A (en) | 1968-07-12 |
GB1228981A (en) | 1971-04-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3318405A (en) | Flexible skirt deflecting means for ground effect vehicles | |
US3232366A (en) | Ground effect machine with permeable material support member | |
GB1455009A (en) | Adjustable seats particularly for use in aircraft | |
US3561559A (en) | Skirting system for surface effect machine | |
ATE47099T1 (en) | CABLE CAR WITH MULTIPLE ROPES. | |
US3363717A (en) | Vehicles for travelling over a surface and equipped with inflatable cushionretainingwalls | |
GB1196751A (en) | Improvements in or relating to Flexible Skirt Assemblies for Ground Effect Machines. | |
US3513933A (en) | Multiskirt ground effect machine | |
ES293449A1 (en) | Control system for ground effect vehicles | |
US3651609A (en) | Air inflated structure | |
GB1529952A (en) | Air cushion vehicles | |
US3752253A (en) | Flexible skirts for gas-cushion supported equipment | |
US3272275A (en) | Movable platform resting on an air cushion enclosed inside at least one yielding prefrably circular skirt | |
GB1105264A (en) | Improvements in or relating to ground effect machines | |
US3572461A (en) | System for confining pressure fluid cushions, more particularly for ground-effect machines | |
US3006577A (en) | Car support for non-rigid airships | |
US3365018A (en) | Skirt construction for surface effect device | |
US3327797A (en) | Ground effect vehicle with detachable flexible skirt | |
US3388766A (en) | Fluid cushion device for ground effect vehicles and the like | |
US4516651A (en) | Vehicles travelling on air cushions allowing movement of the latter over all types of terrain | |
US4488614A (en) | Air-cushion vehicles | |
US3189114A (en) | Vehicles for travelling over land and/or water | |
US3643757A (en) | Flexible skirts for surface-effect machines | |
GB1474391A (en) | Air cushion vehicles | |
GB1191945A (en) | Improvements in or relating to Flexible Skirt Assemblies for Gaseous Cushion Supported Vehicles |