US3695382A - Devices for supplying the pressurized fluid cushions of a ground-effect vehicle - Google Patents

Devices for supplying the pressurized fluid cushions of a ground-effect vehicle Download PDF

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US3695382A
US3695382A US75474A US3695382DA US3695382A US 3695382 A US3695382 A US 3695382A US 75474 A US75474 A US 75474A US 3695382D A US3695382D A US 3695382DA US 3695382 A US3695382 A US 3695382A
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flow
cushions
scoops
wall
pressure fluid
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US75474A
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Henri Francois Marie Schmitt
Claude Marande
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Aerotrain SA
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Aerotrain SA
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V3/00Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/02Land vehicles, e.g. road vehicles
    • B60V3/04Land vehicles, e.g. road vehicles co-operating with rails or other guiding means, e.g. with air cushion between rail and vehicle

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  • a device in a ground-effect vehicle for supplying the pressurized cushions employed to support or to guide Fore'gn Appllcauon Pnomy Dam the said vehicle which device comprises a collector Sept. 26, 1969 France ..6932898 carried y the machine structure and a plurality of pick-up ducts adapted to be fed with pressurized fluid [52] U.S.C1. ..l/1l6, 104/23 F8 from the collector and p g into the respective [51] Int.
  • This device is the kind in which a collector carried by the machine structure supplies pressurized fluid to a plurality of pick-up ducts, each of which extends first of all into theinterior of said collector in a direction substantially parallel to the axis thereof, then in a direction which intersects said axis so that said duct passes through the wall of said collector as well as the machine structure and opens into the cushion or plenum chamber.
  • the pick-up ducts are divergent over at least part of their length and advantageously comprise two opposite divergent walls connected by substantially parallel third and fourth walls.
  • Such a device enables the fluid cushions to be supplied with pressurized fluid in quasi-independent fashion from a common collector.
  • the velocity of the fluid flowing through the collector maybe substantial, the device in accordance with the invention transferring thekinetic energy of the fluid into pressure energy with a high degreeof efficiency. This is a significant factor since it is the total pressure of the fluid flowing through the collector which is employed, whilst its static pressure may be lower than the pressure required for the cushions.
  • the supply device furthermore enables quasiuniform distribution, amongst all the cushions, of the supplied fluid flow to be effected, this by its association of a variable number of pick-up ducts with each cushion and/or by giving such ducts different entry cross-sections depending upon whether they are close to or far away from the source which generates the fluid pressure.
  • the invention can be employed simultaneously for supplying the cushions which support a machine, and the. cushions which guide it.
  • the entry section of the pick-up ducts is variable and the control of the various ducts can be effected independently in a chosen manner for example as a function of the speed of the machine, depending upon whether they are close to or far away from the fluid pressure generator, or again depending upon whether they are associated with lift cushions or guide cushions.
  • the formation of undesirable addies at the input to the pick-up ducts is avoided by arranging a fairing between them.
  • the invention furthermore makes it possible to supply fluid under pressure to the cushions in the form cornpznying drawings will indicate by way of a nonlimitative example how the invention may be carried into practice.
  • FIG. 1 is a schematic longitudinal section of a machine moving along a track on pressurized fluid cushions supplied in accordance with the invention
  • FIG. 2 is a partial transverse section on a larger scale, taken on the line lI--II of FIG. 1;
  • FIG. 3 is a partial longitudinal section on a larger scale taken on the line llIllI of FIG. 2;
  • FIG. 4 is a view similar to that of FIG. 3, taken on the line IV-IV of FIG. 5 and showing the variable entry section pick-up ducts;
  • FIG. 5 is a partial transverse section on a smaller scale, taken on the line V-V of FIG. 4.
  • the machine shown in FIGS. 1, 2 and 3 is a guided hovercraft designed to move along a track 2 of inverted T-section, the leg of the T 2a being vertically disposed, through the medium of lift cushions 3 and guide cushions 4 which are laterally defined by skirts 5.
  • the supply of pressurized fluid, for example compressed air, to the cushions 3 and 4 located at either side of the central ridge 2a, is effected by a fan 6 whose intake fairing 7 opens forward in order to make use of the ram effect produced by the velocity of the machine 1, this fan delivering into a longitudinal collector 8 located in the lower part of the structure la of the machine.
  • Each cushion is supplied through a tap-off or pick-up duct 9 with a fluid pick-up orifice 10 located inside the collector 8 and facing upstream, said duct curving in order to pass through the collector as well as the structure la and to open into the respective cushion 3 or 4 through an exit orifice 1 l.
  • each cushion Associated with each cushion are one or more pickup ducts 9, the number varying in accordance with the position of the cushion in relation to the fan 6, so that a quasi-uniform distribution of the flow between the various cushions is achieved.
  • This kind of result can equally well be obtained by appropriate choice of the section of each fluid pick-up orifice l0.
  • thepick-up ducts 9 are divergent and of rectangular section, at least in their upstream sections which follow the fluid pick-up orifice l0, and are delimited by two opposite divergent walls 9a linked by third and fourth substantially parallel walls 9b.
  • the walls 9a can be constituted by flat panels 9:: located opposite one another in order that neighboring pick-up ducts serving for example one and the same cushion, such as the cushion 3, can be placed side by side and thus reduce the drag in the collector 8.
  • the aerodynamic conditions of flow prevailing there can be improved by uniting non-adjacent ducts 9, or separate groups of adjacent ducts 9, to a fairing 12 which provides continuity in the collector 8 and ensures that all that emerge are the fluid intake orifices 10 which point upstream.
  • the fluid intake 10 of the pick-up ducts 9 is controllable and in particular can have its entry cross-section regulated as a function of the speed of the machine 1.
  • the duct 9 has an upstream section 13 articulated at 14 at the junction between the fairing l2 and the downstream section 17 of the duct 9, which portion 13 can project to a greater or lesser extent beyond the fairing under the control of a suitable system whose transmission linkage is marked and its coupling link 16.
  • the position of the upstream section 13 as illustrated in FIG. 4 at 13b, corresponds with the minimum crosssection of the fluid intake 10.
  • the up stream section 13 of the duct 9 is provided with lateral extensions 13a cooperating in sealed manner with the substantially parallel walls 9b, whatever the position of the moving section 13.
  • a cushion fluid delivery device comprising a source of pressure fluid, a plenum manifold generally coextensive with said cushion system and into which said source discharges a flow of pressure fluid, and a succession of closely juxtaposed scoops having each: an inlet end projecting into said plenum manifold to tap pressure fluid therefrom and facing in an upstream direction with respect to said flow to recover the dynamic pressure thereof, an outlet end opening into said cushion system, and a divergent section intermediate said inlet and outlet ends.
  • variable area rectangular inlet ends comprise each a generally planar pivotal wall element hinged about an axis substantially perpendicular to said flow, and an opposite, generally planar, stationary wall.
  • pivotal wall is adjustable to an inlet end closure position in which it extends substantially parallel to said flow.

Abstract

A device in a ground-effect vehicle for supplying the pressurized cushions employed to support or to guide the said vehicle, which device comprises a collector carried by the machine structure and a plurality of pick-up ducts adapted to be fed with pressurized fluid from the collector and opening into the respective cushions, wherein the pick-up ducts are divergent towards their exits, over at least a part of their lengths, in order to improve transfer and distribution of pressurized fluid between the collector and the cushions.

Description

United States Patent 15 3,695,382 Schmitt et al. v 4s Oct, 3, 1972 [5 DEVICES FOR SUPPLYING THE 3,583,323 6/ 1971 Paris ..l04/23 FS PRESSURIZED FLUID CUSHIONS OF A 3,559,758 2/1971 Bertin ..104/l34 v GROUND-EFFECT VEHICLE 936,395 10/1909 Worthington ..l04/134 [72] Inventors: Henri Francois Marie schmm Am 3,439,772 4/1969 Giraud ..l80/l 18 tony; Claude Mamnde, Bois D,Arcy, 3,575,116 4/1971 Hart ..l80/1 18 I both of France Primary Examiner-Gerald M. Forlenza [73] Assignee: Societe de LAerotrain, Paris, A i E i l), w K
France Att0mey-Stevehs, Davis, Miller & Mosher [22] Filed: Sept. 25, 1970 [57] ABSTRACT [21] Appl. No.: 75,474
A device in a ground-effect vehicle for supplying the pressurized cushions employed to support or to guide Fore'gn Appllcauon Pnomy Dam the said vehicle, which device comprises a collector Sept. 26, 1969 France ..6932898 carried y the machine structure and a plurality of pick-up ducts adapted to be fed with pressurized fluid [52] U.S.C1. ..l/1l6, 104/23 F8 from the collector and p g into the respective [51] Int. Cl ..B6lb 1/00, B6lb l/06 cushions, wherein the pick-up ducts are divergent [58] Field of Search /1 16, 1 18, 125, 127; owards th ir exits, ov r at least a part of th ir lengths,
104/134, 23 F8 in order to improve transfer and distribution of pressurized fluid between the collector and the cushions. [56] References Cited v 8 Claims, 5 Drawing Figures UNITED STATES PATENTS 3,388,766 6/1968 Bertin ..l80/ 127 PATENTEDncrs I972 3.6954382 sum 1 0F 3 EJQDQCBGCDQQ UU PATENTEDnm 3 1972 SHEET 2 [IF 3 This invention relates to a device for supplying the pressurized fluid cushions which support and/or guide a ground-effect vehicle.
This device is the kind in which a collector carried by the machine structure supplies pressurized fluid to a plurality of pick-up ducts, each of which extends first of all into theinterior of said collector in a direction substantially parallel to the axis thereof, then in a direction which intersects said axis so that said duct passes through the wall of said collector as well as the machine structure and opens into the cushion or plenum chamber.
In accordance with the invention, the pick-up ducts are divergent over at least part of their length and advantageously comprise two opposite divergent walls connected by substantially parallel third and fourth walls.
Such a device enables the fluid cushions to be supplied with pressurized fluid in quasi-independent fashion from a common collector. The velocity of the fluid flowing through the collector maybe substantial, the device in accordance with the invention transferring thekinetic energy of the fluid into pressure energy with a high degreeof efficiency. This is a significant factor since it is the total pressure of the fluid flowing through the collector which is employed, whilst its static pressure may be lower than the pressure required for the cushions.
The supply device furthermore enables quasiuniform distribution, amongst all the cushions, of the supplied fluid flow to be effected, this by its association of a variable number of pick-up ducts with each cushion and/or by giving such ducts different entry cross-sections depending upon whether they are close to or far away from the source which generates the fluid pressure.
The invention can be employed simultaneously for supplying the cushions which support a machine, and the. cushions which guide it. In this case, it.is equally possible to provide different numbers of pick-up ducts and/or ducts with differing entry sections, depending upon whether they are to be used to supply, the lift cushions or the guide cushions.
In one embodiment of the invention, the entry section of the pick-up ducts is variable and the control of the various ducts can be effected independently in a chosen manner for example as a function of the speed of the machine, depending upon whether they are close to or far away from the fluid pressure generator, or again depending upon whether they are associated with lift cushions or guide cushions.
In accordance with one further feature of the invention, the formation of undesirable addies at the input to the pick-up ducts is avoided by arranging a fairing between them.
The invention furthermore makes it possible to supply fluid under pressure to the cushions in the form cornpznying drawings will indicate by way of a nonlimitative example how the invention may be carried into practice.
IN THE DRAWINGS FIG. 1 is a schematic longitudinal section of a machine moving along a track on pressurized fluid cushions supplied in accordance with the invention;
FIG. 2 is a partial transverse section on a larger scale, taken on the line lI--II of FIG. 1;
FIG. 3 is a partial longitudinal section on a larger scale taken on the line llIllI of FIG. 2;
FIG. 4 is a view similar to that of FIG. 3, taken on the line IV-IV of FIG. 5 and showing the variable entry section pick-up ducts;
FIG. 5 is a partial transverse section on a smaller scale, taken on the line V-V of FIG. 4.
The machine shown in FIGS. 1, 2 and 3 is a guided hovercraft designed to move along a track 2 of inverted T-section, the leg of the T 2a being vertically disposed, through the medium of lift cushions 3 and guide cushions 4 which are laterally defined by skirts 5.
The supply of pressurized fluid, for example compressed air, to the cushions 3 and 4 located at either side of the central ridge 2a, is effected by a fan 6 whose intake fairing 7 opens forward in order to make use of the ram effect produced by the velocity of the machine 1, this fan delivering into a longitudinal collector 8 located in the lower part of the structure la of the machine. Each cushion is supplied through a tap-off or pick-up duct 9 with a fluid pick-up orifice 10 located inside the collector 8 and facing upstream, said duct curving in order to pass through the collector as well as the structure la and to open into the respective cushion 3 or 4 through an exit orifice 1 l.
Associated with each cushion are one or more pickup ducts 9, the number varying in accordance with the position of the cushion in relation to the fan 6, so that a quasi-uniform distribution of the flow between the various cushions is achieved. This kind of result can equally well be obtained by appropriate choice of the section of each fluid pick-up orifice l0.
In accordance with the invention, thepick-up ducts 9 are divergent and of rectangular section, at least in their upstream sections which follow the fluid pick-up orifice l0, and are delimited by two opposite divergent walls 9a linked by third and fourth substantially parallel walls 9b.
As FIG. 3 shows, the walls 9a can be constituted by flat panels 9:: located opposite one another in order that neighboring pick-up ducts serving for example one and the same cushion, such as the cushion 3, can be placed side by side and thus reduce the drag in the collector 8. For the same purpose, the aerodynamic conditions of flow prevailing there can be improved by uniting non-adjacent ducts 9, or separate groups of adjacent ducts 9, to a fairing 12 which provides continuity in the collector 8 and ensures that all that emerge are the fluid intake orifices 10 which point upstream.
In the embodiment shown in FIGS 4 and 5, the fluid intake 10 of the pick-up ducts 9 is controllable and in particular can have its entry cross-section regulated as a function of the speed of the machine 1. To this end, the duct 9 has an upstream section 13 articulated at 14 at the junction between the fairing l2 and the downstream section 17 of the duct 9, which portion 13 can project to a greater or lesser extent beyond the fairing under the control of a suitable system whose transmission linkage is marked and its coupling link 16.
The position of the upstream section 13 as illustrated in FIG. 4 at 13b, corresponds with the minimum crosssection of the fluid intake 10. As FIG. 5 shows, the up stream section 13 of the duct 9 is provided with lateral extensions 13a cooperating in sealed manner with the substantially parallel walls 9b, whatever the position of the moving section 13.
It should be noted that it is possible to control the position of the moving section 13 in order to provide a pick-up duct whose section is convergent upstream of the joint 14 and divergent downstream of said joint.
It will be apparent that the embodiments above described are purely examples and are open to modification in various ways without departing from the scope of the invention as defined by the appended claims.
We claim:
1. In a surface effect machine movable along a bearing surface with the interposition of a pressure fluid cushion system, a cushion fluid delivery device comprising a source of pressure fluid, a plenum manifold generally coextensive with said cushion system and into which said source discharges a flow of pressure fluid, and a succession of closely juxtaposed scoops having each: an inlet end projecting into said plenum manifold to tap pressure fluid therefrom and facing in an upstream direction with respect to said flow to recover the dynamic pressure thereof, an outlet end opening into said cushion system, and a divergent section intermediate said inlet and outlet ends.
2. A device according to claim 1, wherein said scoops have opposite planar wall portions which are substantially parallel to each other, with wall portions of adjacent scoops being contiguous.
3. A device according to claim 2, wherein said scoops are of substantially rectangular cross-section and said inlet ends thereof are of substantially rectangular shape.
4. A device according to claim 11, wherein said rectangular inlet ends extend in planes spaced longitudinally and generally normal to said flow.
5. A device according to claim 3, wherein said rectangular inlet ends are of variable area.
6. A device according to claim 5, wherein said variable area rectangular inlet ends comprise each a generally planar pivotal wall element hinged about an axis substantially perpendicular to said flow, and an opposite, generally planar, stationary wall.
7. A device according to claim 6, wherein said pivotal wall is on the inward side of said stationary wall with respect to said plenum manifold.
8. A device according to claim 7, wherein said pivotal wall is adjustable to an inlet end closure position in which it extends substantially parallel to said flow.

Claims (8)

1. In a surface effect machine movable along a bearing surface with the interposition of a pressure fluid cushion system, a cushion fluid delivery device comprising a source of pressure fluid, a plenum manifold generally coextensive with said cushion system and into which said source discharges a flow of pressure fluid, and a succession of closely juxtaposed scoops having each: an inlet end projecting into said plenum manifold to tap pressure fluid therefrom and facing in an upstream direction with respect to said flow to recover the dynamic pressure thereof, an outlet end opening into said cushion system, and a divergent section intermediate said inlet and outlet ends.
2. A device according to claim 1, wherein said scoops have opposite planar wall portions which are substantially parallel to each other, with wall portions of adjacent scoops being contiguous.
3. A device according to claim 2, wherein said scoops are of substantially rectangular cross-section and said inlet ends thereof are of substantially rectangular shape.
4. A device according to claim 11, wherein said rectangular inlet ends extend in planes spaced longitudinally and generally normal to said flow.
5. A device according to claim 3, wherein said rectangular inlet ends are of variable area.
6. A device according to claim 5, wherein said variable area rectangular inlet ends comprise each a generally planar pivotal wall element hinged about an axis substantially perpendicular to said flow, and an opposite, generally planar, stationary wall.
7. A device according to claim 6, wherein said pivotal wall is on the inward side of said stationary wall with respect to said plenum manifold.
8. A device according to claim 7, wherein said pivotal wall is adjustable to an inlet end closure position in which it extends substantially parallel to said flow.
US75474A 1969-09-26 1970-09-25 Devices for supplying the pressurized fluid cushions of a ground-effect vehicle Expired - Lifetime US3695382A (en)

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FR696932898A FR2063112B1 (en) 1969-09-26 1969-09-26

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BE (1) BE756628A (en)
CH (1) CH528396A (en)
DE (1) DE2047243C3 (en)
FR (1) FR2063112B1 (en)
GB (1) GB1318539A (en)
LU (1) LU61745A1 (en)
NL (1) NL7014121A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5542357A (en) * 1994-03-18 1996-08-06 Northrop Grumman Corporation Linear turbine propulsion system
US5876825A (en) * 1997-01-28 1999-03-02 Pacific Foam Technologies Customized cushioned floor mat and method of producing same

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3099449B1 (en) 2019-07-29 2021-08-20 Spacetrain Fluid regulating device of at least one fluid pad for a fluid pad vehicle

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US936395A (en) * 1908-11-09 1909-10-12 Charles Worthington Transportation system.
US3388766A (en) * 1962-01-11 1968-06-18 Bertin & Cie Fluid cushion device for ground effect vehicles and the like
US3439772A (en) * 1965-12-29 1969-04-22 Bertin & Cie Surface effect devices with fluid amplifier stabilizing means
US3559758A (en) * 1967-08-22 1971-02-02 Bertin & Cie Fluid cushion confining device
US3575116A (en) * 1967-08-03 1971-04-13 Hovercraft Dev Ltd Gas-cushion load-supporting apparatus
US3583323A (en) * 1968-02-14 1971-06-08 Aerotrain Gas-cushion vehicle

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1550267A (en) * 1967-10-19 1968-12-20

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US936395A (en) * 1908-11-09 1909-10-12 Charles Worthington Transportation system.
US3388766A (en) * 1962-01-11 1968-06-18 Bertin & Cie Fluid cushion device for ground effect vehicles and the like
US3439772A (en) * 1965-12-29 1969-04-22 Bertin & Cie Surface effect devices with fluid amplifier stabilizing means
US3575116A (en) * 1967-08-03 1971-04-13 Hovercraft Dev Ltd Gas-cushion load-supporting apparatus
US3559758A (en) * 1967-08-22 1971-02-02 Bertin & Cie Fluid cushion confining device
US3583323A (en) * 1968-02-14 1971-06-08 Aerotrain Gas-cushion vehicle

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5542357A (en) * 1994-03-18 1996-08-06 Northrop Grumman Corporation Linear turbine propulsion system
US5669308A (en) * 1994-03-18 1997-09-23 Northrop Grumman Corporation Linear turbine propulsion system
US5876825A (en) * 1997-01-28 1999-03-02 Pacific Foam Technologies Customized cushioned floor mat and method of producing same

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DE2047243A1 (en) 1971-04-01
FR2063112A1 (en) 1971-07-09
DE2047243B2 (en) 1979-06-21
FR2063112B1 (en) 1973-04-06
NL7014121A (en) 1971-03-30
DE2047243C3 (en) 1980-02-21
BE756628A (en) 1971-03-25
CH528396A (en) 1972-09-30
LU61745A1 (en) 1971-01-18
GB1318539A (en) 1973-05-31

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