US3590764A - Gas-cushion vehicles - Google Patents

Gas-cushion vehicles Download PDF

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Publication number
US3590764A
US3590764A US788232A US3590764DA US3590764A US 3590764 A US3590764 A US 3590764A US 788232 A US788232 A US 788232A US 3590764D A US3590764D A US 3590764DA US 3590764 A US3590764 A US 3590764A
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cushion
gas
hull
skirt
water
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US788232A
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Rowland D Hunt
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Vosper Ltd
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Vosper Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion

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  • the invention relates to gas-cushion vehicles, and more par ticularly to gas-cushion vehicles of the type provided with water reaction propulsion mechanism such as pumps for producing water jets, or water screws.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Vehicle Body Suspensions (AREA)
  • Wind Motors (AREA)

Abstract

A water reaction propulsion mechanism for the vehicle is housed within a skeg or keellike member located within the gas-cushion space of the vehicle and is retractable to prevent damage to the propulsion mechanism when the vehicle is temporarily on land or in very shallow water. Auxiliary propulsion means are provided for use when said member is retracted.

Description

United States Patent [72] Inventor Rowland D. Hunt Fareharn. England [21] Appl. No 788.232
[22] Filed Dee.31,l968
I45) Patented July 6, i971 [73) Assignee Vesper Llmited [32] Priority Jan. II, 1968 [33] Great Britain [S4] GAS-CUSHION VEHICLES 10 Claims, 5 Drawing Figs.
[52] U.S. Cl 114/67, l l4/l4l [5 I Int. Cl .t B63!) 1/38 [50] Field of Search 114/671, I41
[56] References Cited UNITED STATES PATENTS 93 L159 8/1909 Stribling ll4/l4l 3,384,!98 5/1968 Jones et al. .4 l14/67 Primary Examiner-Andrew H. Farrell Attorney-Norris and Bateman ABSTRACT: A water reaction propulsion mechanism for the vehicle is housed within a skeg 0t keellike member located within the gascushion space of the vehicle and is retractable to prevent damage to the propulsion mechanism when the vehicle is temporarily on land or in very shallow water. Auxiliary propulsion means are provided for use when said member is retracted.
PATENIEU JUL slan 3,590,764
INVBN'IOR ROWLAND DE LVI LLE HUNT PATENTEI] JUL 6 l9?! SHEET 2 UF 2 INVENTOR ROWLAND mLvgLLE HUNT GAS-CUSHION VEHICLES BACKGROUND OF INVENTION The invention relates to gas-cushion vehicles, and more par ticularly to gas-cushion vehicles of the type provided with water reaction propulsion mechanism such as pumps for producing water jets, or water screws.
It has hitherto been envisaged that a gas-cushion vehicle of the type referred to should operate from a pier or floating dock with sufficient depth of water at low tide to keep the dock afloat and enable the vehicle to maneuver. This requirement calls for an expensive terminal structure.
SUMMARY OF INVENTION The object of the invention is to eliminate the need for such a vehicle to operate from a pier or floating dock.
According to the invention, a gas-cushion vehicle is provided with at least one means housing water reaction propulsion mechanism, the whole or a part of the or each means being a retractable member.
BRIEF DESCRIPTION OF DRAWINGS Four embodiments of the invention will now described by way of example only, with reference to the accompanying diagrammatic drawings of which:
FIG. 1 is a sectional side view of part of an air-cushion vehicle showing a preferred embodiment of the invention;
FIG. 2 is a sectional view on the line 2-2 in FIG. I;
FIG. 3 is a sectional view on the line 3-3 in FIG. I;
FIG. 4 is a sectional side view of an air-cushion vehicle showing another embodiment ofthe invention; and
FIG. 5 is a sectional end view of part of an air-cushion vehicle showing a further embodiment of the invention.
DESCRIPTION OF PREFERRED EMBODIMENTS In the preferred embodiment of the invention, see FIGS. 1, 2, and 3 an aircushion vehicle has a hull 11 carrying a full flexible skirt I2 and a power unit 13 driving at least one fan for supplying air under pressure to the space enclosed by the skirt 12 to provide an air-cushion for supporting the vehicle. Water reaction propulsion mechanism for the vehicle comprises two axial flow pumps 14 each driven, via shafts 41, 42 and 43 and bevel gear units 44 and 45, by a power unit IS. The pumps 14 are housed within the lower parts 17 of respective laterally spaced parallel skegs or keellike members I6, the upper parts of the skegs 16 being above the waterline I9 when the vehicle is supported by its air-cushion. The lower part I7 of each skeg I6 is pivotable relative to the upper part thereof about a longitudinal hinge l8, coaxial with the shaft 43, by power operated means (not shown). The inlet 20 of each pump 14 is formed in associated lower part 17 and the outlet 46 thereof opens from said part into the cushion space. A flap 47 can be moved between an inoperative position (not shown) and an operative position shown in full lines in FIG. 1 to obstruct the normal outlet 46 of each pump 14 whereupon the water is expelled through vanes 48 for reverse thrust. Two laterally spaced high power/weight ratio gas-turbine jet engines or rocket motors 21 are provided at the stern of the vehi cle as auxiliary propulsion means, and two laterally spaced docking supports 22 project from the underside of the hull I1 near its forward end.
When travelling over water, the vehicle is supported by the air-cushion and propelled by water ejected at high velocity from the pump outlets 46. In order to turn the vehicle the pumps I4 are operated individually or at relatively different speeds, or the thrust of them is reversed by means of its flap 47. For reverse travel of the vehicle, both of the flaps 47 are moved into their operative positions. When it is desired to operate temporarily in extremely shallow water or on land, the In drive to the pumps 14 is discontinued and the lower parts 1 of the skegs I6 are swung upwardly by the power-operated 75 means. When proceeding directly on to a beach or the like, the momentum of the vehicle may be large enough to carry it sufficiently clear of the water to enable any cargo to be unloaded or loaded without the need of specially constructed docking facilities. Upon reaching a suitable position for transferring cargo the supply of air under pressure to the cushion space is cut off and the vehicle comes to rest on the supports 22 and the upper parts of the skegs I6. Return to the water may be possible by reinstating the air-cushion and allowing the vehicle simply to slide down the beach. When the vehicle has returned to relatively deep water the lower parts 17 of the skegs 16 are swung back into operative position by the poweroperated means and the vehicle is once again propelled by the pumps 14. In extremely shallow water, and in difficult conditions on land, for example where the slope of the beach is adverse or the vehicle has insufficient momentum, or possibly where there are very strong winds, the engines 2! are employed to propel the vehicle temporarily when the lower parts l7 of the skegs 16 are retracted and the pumps 14 are inoperative. The engines 21 are operated together to propel the vehicle forwards and individually or at relatively different speeds to turn the vehicle.
In another embodiment of the invention (see FIG. 4 in which parts corresponding to equivalent parts in FIGS. 1, 2 and 3 are identified by the same numbers), the water reaction propulsion mechanism in each of two laterally spaced skegs 16 is a vertical stack of individual pumps 14 which are connected in parallel, housed in the upper part of the skeg, and mounted on a common drive shaft projecting vertically downwards from the associated engine 15. The lower part I7 of the skeg 16 contains the pump inlet 20 and is pivotable about a longitudinal hinge I8.
In a further embodiment of the invention, see FIG. 5, the drive to a stack of pumps 14 is via bevel gearing 23, 24 and the major part 25 of a skeg contains said pumps and is pivotable about a longitudinal hinge coaxial with the driving gear 23.
lclaim:
1. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a pump assembly for producing a waterjet, characterized in that at least that part of said member which extends below the waterline is retractable and contains the inlet of said assembly.
2. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a water reaction propulsion mechanism, characterized in that at least that part of said member which extends below the waterline is retractable by pivotal movement about an axis extends longitudinally of the vehicle.
3. A gas-cushion vehicle according to claim 2, 2 further characterized in that only part of said keellike member is retractable and is hinged for displacement relative to the remainder of said member about said axis.
4. A gas-cushion vehicle according to claim 2, 2 further characterized in that auxiliary propulsion means other than of water reaction type are provided.
5. A gas-cushion vehicle according to claim 4, 4 further characterized in that said auxiliary propulsion means are of air reaction type.
6. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a pump assembly for producing a water jet, characterized in that part of said member which extends below the waterline is retractable and contains the inlet of said assembly, the retractable part is hinged for displacement relative to the remainder of said member about an axis which extends longitudinally of the vehicle, and auxiliary propulsion means other than of water reaction type are provided.
7. A gas-cushion vessel adapted for water travel comprising a hull having a depending full flexible skirt and power driven means supplying air under pressure within said skirt, laterally spaced keellike members depending from said hull within the skirt. each of said members comprising a lower portion hinged about a longitudinal axis, and longitudinal water passages in each of said members containing independently operable power driven pump means.
8. [n the vessel defined in claim 7, each of said pump means comprising a pump having its axis substantially coincident with said hinge axis.
9. A gas-cushion vessel adapted for water travel comprising a hull having a depending full skirt and power driven means supplying air under pressure within said skirt, at least one keellike member depending from said hull within the skirt. said member having a lower portion that projects below the waterline and is retractable about a longitudinal axis, and propulsion means comprising a stack of power driven pumps mounted in the upper portion of said member and disposed in water passage means extending mainly longitudinally through said member.
10. A gas-cushion vessel adapted for water travel comprising a hull having a depending full skirt and power driven means supplying air under pressure within said skirt, at least one keellike member depending from said hull within the skirt, said member having a lower portion that projects below the waterline and is retractable about a longitudinal axis, propulsion means comprising a stack of power driven pumps mounted in said lower portion of said member and disposed in water passage means extending through said member, and drive means connecting said propulsion means to a source of power carried by said hull.

Claims (10)

1. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a pump assembly for producing a water jet, characterized in that at least that part of said member which extends below the waterline is retractable and contains the inlet of said assembly.
2. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a water reaction propulsion mechanism, characterized in that at least that part of said member which extends below the waterline is retractable by pivotal movement about an axis extends longitudinally of the vehicle.
3. A gas-cushion vehicle according to claim 2, 2 further characterized in that only part of said keellike member is retractable and is hinged for displacement relative to the remainder of said member about said axis.
4. A gas-cushion vehicle according to claim 2, 2 further characterized in that auxiliary propulsion means other than of water reaction type are provided.
5. A gas-cushion vehicle according to claim 4, 4 further characterized in that said auxiliary propulsion means are of air reaction type.
6. A gas-cushion vehicle having a keellike member within its cushion space which extends downwardly from its hull to a point below the waterline and houses a pump assembly for producing a water jet, characterized in that part of said member which extends below the waterline is retractable and contains the inlet of said assembly, the retractable part is hinged for displacement relative to the remainder of said member about an axis which extends longitudinally of the vehicle, and auxiliary propulsion means other than of water reaction type are provided.
7. A gas-cushion vessel adapted for water travel comprising a hull having a depending full flexible skirt and power driven means supplying air under pressure within said skirt, laterally spaced keellike members depending from said hull within the skirt, each of said members comprising a lower portion hinged about a longitudinal axis, and longitudinal water passages in each of said members containing independently operable power driven pump means.
8. In the vessel defined in claim 7, each of said pump means comprising a pump having its axis substantially coincident with said hinge axis.
9. A gas-cushion vessel adapted for water travel comprising a hull having a depending full skirt and power driven means supplying air under pressure within said skirt, at least one keellike member depending from said hull within the skirt, said member having a lower portion that projects below the waterline and is retractable about a longitudinal axis, and propulsion means comprising a stack of power driven pumps mounted in the upper portion of said member and disposed in water passage means extending mainly longitudinally through said member.
10. A gas-cushion vessel adapted for water travel comprising a hull having a depending full skirt and power driven means supplying air under pressure within said skirt, at least one keellike member depending from said hull within the skirt, said member having a lower portion that projects below the waterline and is retractable about a longitudinal axis, propulsion means comprising a stack of power driven pumps mounted in said lower portion of said member and disposed in water passage means extending through said member, and drive means connecting said propulsion means to a source of power carried by said hull.
US788232A 1968-01-11 1968-12-31 Gas-cushion vehicles Expired - Lifetime US3590764A (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6062922A (en) * 1998-10-30 2000-05-16 Yamaha Hatsudoki Kabushiki Kaisha Watercraft propulsion system

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2241213A (en) * 1989-10-02 1991-08-28 John Graham Walker Directional control of air cushion vehicles

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US931159A (en) * 1908-07-03 1909-08-17 Franklin E Stribling Drop-propeller for boats.
US3384198A (en) * 1964-11-18 1968-05-21 Westland Aircraft Ltd Ground effect vehicles

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US931159A (en) * 1908-07-03 1909-08-17 Franklin E Stribling Drop-propeller for boats.
US3384198A (en) * 1964-11-18 1968-05-21 Westland Aircraft Ltd Ground effect vehicles

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6062922A (en) * 1998-10-30 2000-05-16 Yamaha Hatsudoki Kabushiki Kaisha Watercraft propulsion system

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FR1600968A (en) 1970-08-03
GB1237882A (en) 1971-06-30

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