US3518956A - Bubble hulls - Google Patents
Bubble hulls Download PDFInfo
- Publication number
- US3518956A US3518956A US729714A US3518956DA US3518956A US 3518956 A US3518956 A US 3518956A US 729714 A US729714 A US 729714A US 3518956D A US3518956D A US 3518956DA US 3518956 A US3518956 A US 3518956A
- Authority
- US
- United States
- Prior art keywords
- hull
- bubble
- compartments
- plane
- partitions
- 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
- B60V1/04—Air-cushion wherein the cushion is contained at least in part by walls
- B60V1/046—Air-cushion wherein the cushion is contained at least in part by walls the walls or a part of them being rigid
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/11—Stability or attitude control
- B60V1/12—Stability or attitude control by dividing the cushion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
- B63B1/32—Other means for varying the inherent hydrodynamic characteristics of hulls
- B63B1/34—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction
- B63B1/38—Other means for varying the inherent hydrodynamic characteristics of hulls by reducing surface friction using air bubbles or air layers gas filled volumes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T70/00—Maritime or waterways transport
- Y02T70/10—Measures concerning design or construction of watercraft hulls
Definitions
- the present invention has the object of obviating above mentioned disadvantages.
- the present invention is characterised in that the bottom part of the hull is divided into compartments; the compartments being open at the bottom in such manner as to give rise to the formation of at least four elementary captured air bubbles.
- the compartments are bounded by three longitudinal partitions, one of which is in the axis of symmetry of the hull, and by three transversal partitions.
- the bottom edges of all the partitions are preferably in a single plane which is substantially horizontal at rest.
- the above briefly described structure results in division of the bubble into four elementary bubbles and provides stability because in the case of a difference in level the bubbles of the portions which are immersed to a greater extent will be at a higher pressure than the bubbles of the portions which have emerged to a greater extent. Accordingly, the difference in pressure between the respective bubbles supplies the lifting couple.
- the front walls of the transversal partitions are convex cylindrical in shape.
- the axes of the cylinders are perpendicular to the plane of symmetry of the hull in the case of the front walls of the rearmost partitions, while the axis of the cylinders of the front walls of the front partition form an acute angle with said plane of symmetry.
- the front transversal partition taken as a whole and viewed in plan, has a V-shaped form, the point of the V forming the stem of the hull.
- the overall shape of the bow of the vessel viewed in plan will preferably be that of a W, the outer side branches of the W forming lateral aprons having the effect of containing the two branches of the central stem wave and of reducing, if not eliminating, their drag effect.
- Each bubble is preferably supplied continuously with air by an independent blower or, as an alternative, the bubbles are fed by a common blower delivering into a number of pipes equal to the number of compartments.
- each pipe has a loss of head suitably calculated to make the deliveries uniform, since otherwise they would be disturbed by the movements of the hull.
- the pressurised air is preferably introduced into each compartment through the bottom portion, tangentially to the bottom limit plane.
- FIG. 1 illustrates the hull, which is assumed to be in section through a horizontal plane immediately above the flat bottom and viewed from below, with nevertheless a slight effect of perspective.
- the hull may have any shape and structure in the invisible portion beyond the sectional plane.
- This flat bottom 1 constitutes on its lower side the upper plane delimiting the bubbles.
- FIG. 2 is a sectional side elevation view of a portion of the hull shown in FIG. 1, FIG. 2 depicting the preferred method of furnishing pressurised air to the bubbledefining hull compartments.
- the invention relates to the arrangement of the portion beneath said flat bottom.
- Two longitudinal partitions 6 and 7 bound the compartments laterally.
- the outer walls are extensions of the hull and the inner walls are flat and inclined towards the interior of the compartments.
- the middle partition 8 the edge of which is in a plane of symmetry of the hull, likewise has flat walls inclined towards the interior of the compartments.
- the transversal partitions have convex front walls 12 in the form of a cylinder having a horizontal axis perpendicular to the plane of symmetry of the hull. Along the edges 9 and these walls adjoin the bottom limit plane of the bubble.
- the rear walls 13 of these partitions are flat and vertical or inclined towards the interior of the compartments.
- the bow of the vessel has here the general shape of a W, the bottom edges of the outer branches of the W being designated by 14 and 15 and the bottom edges of the branches of the central V, defined by the forward transversal partition, being designated by 16 and 17.
- the walls 18 to 21 are convex cylindrical, the axes of the cylinders forming acute angles with the plane of symmetry of the hull. Their faces are joined along the edges 14 to 17 tangentially to the bottom limit plane of the bubble.
- the faces 18 and 20 are joined together, and the faces 19 and 21 are joined together, by cylindrical surfaces 22 and 23, the axis of the cylinders being perpendicular to the aforesaid plane of symmetry.
- the rear faces are preferably vertical.
- air will preferably be supplied to the compartments by means of nan-ow slots disposed along the rear faces of the transversal walls, preferably near the edge situated in the bottom limit plane of the bubbles.
- a hull for a vessel characterised in that the bottom portion of the hull is divided into a plurality of compartments, the compartments being opened at the bottom and giving rise to the formation of at least four elementary air bubbles, said compartments being defined in part by three rigid longitudinal partitions, one of said longitudinal partitions being aligned with the axis of symmetry of the hull, said compartments being further defined by at least three rigid transversal partitions, the bottom edges of all of said partitions lying in a single plane which is substantially horizontal with the vessel at rest.
- a bubble hull according to claim 1 characterised in that the front walls of the transversal partitions are of convex cylindrical shape, the axis of the cylinders being perpendicular to the plant of symmetry of the hull in the case of the front walls of the rearmost partitions, while the axis of the cylinders of the front walls of the front partition form an acute angle with said plane of symmetry.
- a bubble hull according to claim 2 characterised in that the front walls are terminated horizontally at their vanishing point and tangentially to the bottom limit plane of the bubble.
- a bubble hull according to claim 1 characterised in that the front transversal partition, as a whole and viewed in plan, has a V-shaped form, the point of the V forming the stem of the hull.
- a bubble hull according to claim 4 characterised in that the shape of the forward end of the hull including said front partition will be that of a W.
- a bubble hull according to claim 1 characterised in that the pressurised air is introduced into each compartment through the bottom portion and tangentially to the bottom limit plane.
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
Jul 7,1970 M. cs. H. GIRODIN BUBBLE HULLS 2 Sheets-Sheet 1 Filed May 16, 1968 July 7, 1970 M. G. H.-G|RODIN 3,513,956
' BUBBLE HULLS Filed May 16, 1968 2 Sheets-Sheet 2 United States Patent 3,518,956 BUBBLE HULLS Marius Georges Henri Girodin, 20 Place de la Madeleine, Paris, France Filed May 16, 1968, Ser. No. 729,714 Claims priority, applicago; France, May 26, 1967,
Int. Cl. Btssb 1/34 U.S. Cl. 114-67 6 Claims ABSTRACT OF THE DISCLOSURE A hull for a water vehicle of the captured air bubble type wherein the lower exterior surface area of the hull is divided into at least four symmetrically disposed compartments for capturing air bubbles.
BACKGROUND OF THE INVENTION SUMMARY OF THE DISCLOSURE The present invention has the object of obviating above mentioned disadvantages.
The present invention is characterised in that the bottom part of the hull is divided into compartments; the compartments being open at the bottom in such manner as to give rise to the formation of at least four elementary captured air bubbles. The compartments are bounded by three longitudinal partitions, one of which is in the axis of symmetry of the hull, and by three transversal partitions. The bottom edges of all the partitions are preferably in a single plane which is substantially horizontal at rest.
The above briefly described structure results in division of the bubble into four elementary bubbles and provides stability because in the case of a difference in level the bubbles of the portions which are immersed to a greater extent will be at a higher pressure than the bubbles of the portions which have emerged to a greater extent. Accordingly, the difference in pressure between the respective bubbles supplies the lifting couple.
According to another characteristic of the invention, the front walls of the transversal partitions are convex cylindrical in shape. The axes of the cylinders are perpendicular to the plane of symmetry of the hull in the case of the front walls of the rearmost partitions, while the axis of the cylinders of the front walls of the front partition form an acute angle with said plane of symmetry.
These front walls terminate horizontally at their vanishing point, that is to say tangentially to the bottom limit plane of the bubble.
In contrast to previous procedure, these walls are not provided to perform a lifting function, and the tangential connection avoids any downward acceleration of the liquid.
According to another characteristic of the invention the front transversal partition, taken as a whole and viewed in plan, has a V-shaped form, the point of the V forming the stem of the hull.
The overall shape of the bow of the vessel, viewed in plan will preferably be that of a W, the outer side branches of the W forming lateral aprons having the effect of containing the two branches of the central stem wave and of reducing, if not eliminating, their drag effect.
Each bubble is preferably supplied continuously with air by an independent blower or, as an alternative, the bubbles are fed by a common blower delivering into a number of pipes equal to the number of compartments. In the case of a single blower each pipe has a loss of head suitably calculated to make the deliveries uniform, since otherwise they would be disturbed by the movements of the hull.
The pressurised air is preferably introduced into each compartment through the bottom portion, tangentially to the bottom limit plane.
Other characteristics of the invention will be clear in the course of the following description, which is given solely by way of example of embodiment of the invention.
BRIEF DESCRIPTION OF THE DRAWING In the accompanying drawing, FIG. 1 illustrates the hull, which is assumed to be in section through a horizontal plane immediately above the flat bottom and viewed from below, with nevertheless a slight effect of perspective.
In this construction, the hull may have any shape and structure in the invisible portion beyond the sectional plane. This flat bottom 1 constitutes on its lower side the upper plane delimiting the bubbles.
FIG. 2 is a sectional side elevation view of a portion of the hull shown in FIG. 1, FIG. 2 depicting the preferred method of furnishing pressurised air to the bubbledefining hull compartments.
The invention relates to the arrangement of the portion beneath said flat bottom.
DESCRIPTION OF AN EMBODIMENT As can be seen from the drawings, four depressed compartments 2, 3, 4 and 5 are seen 'when the bottom is viewed from below, this resulting from the following method of partitioning:
Two longitudinal partitions 6 and 7 bound the compartments laterally. The outer walls are extensions of the hull and the inner walls are flat and inclined towards the interior of the compartments.
The middle partition 8, the edge of which is in a plane of symmetry of the hull, likewise has flat walls inclined towards the interior of the compartments.
The transversal partitions, the edges of which are designated by 9 and 10, have convex front walls 12 in the form of a cylinder having a horizontal axis perpendicular to the plane of symmetry of the hull. Along the edges 9 and these walls adjoin the bottom limit plane of the bubble. The rear walls 13 of these partitions are flat and vertical or inclined towards the interior of the compartments.
The bow of the vessel has here the general shape of a W, the bottom edges of the outer branches of the W being designated by 14 and 15 and the bottom edges of the branches of the central V, defined by the forward transversal partition, being designated by 16 and 17. The walls 18 to 21 are convex cylindrical, the axes of the cylinders forming acute angles with the plane of symmetry of the hull. Their faces are joined along the edges 14 to 17 tangentially to the bottom limit plane of the bubble.
The faces 18 and 20 are joined together, and the faces 19 and 21 are joined together, by cylindrical surfaces 22 and 23, the axis of the cylinders being perpendicular to the aforesaid plane of symmetry. The rear faces are preferably vertical.
As may clearly be seen from FIG. 2, air will preferably be supplied to the compartments by means of nan-ow slots disposed along the rear faces of the transversal walls, preferably near the edge situated in the bottom limit plane of the bubbles.
Consequently, in the event of the failure of the blower or blowers, air cushions will remain available which will provide support.
As the result of the form of partitioning which has been described above, four separate air bubbles are captured which are contained in four fluid-tight compartments of general prismatic shape.
I claim:
1. A hull for a vessel characterised in that the bottom portion of the hull is divided into a plurality of compartments, the compartments being opened at the bottom and giving rise to the formation of at least four elementary air bubbles, said compartments being defined in part by three rigid longitudinal partitions, one of said longitudinal partitions being aligned with the axis of symmetry of the hull, said compartments being further defined by at least three rigid transversal partitions, the bottom edges of all of said partitions lying in a single plane which is substantially horizontal with the vessel at rest.
2. A bubble hull according to claim 1, characterised in that the front walls of the transversal partitions are of convex cylindrical shape, the axis of the cylinders being perpendicular to the plant of symmetry of the hull in the case of the front walls of the rearmost partitions, while the axis of the cylinders of the front walls of the front partition form an acute angle with said plane of symmetry.
3. A bubble hull according to claim 2, characterised in that the front walls are terminated horizontally at their vanishing point and tangentially to the bottom limit plane of the bubble.
4. A bubble hull according to claim 1, characterised in that the front transversal partition, as a whole and viewed in plan, has a V-shaped form, the point of the V forming the stem of the hull.
5. A bubble hull according to claim 4 characterised in that the shape of the forward end of the hull including said front partition will be that of a W.
6. A bubble hull according to claim 1, characterised in that the pressurised air is introduced into each compartment through the bottom portion and tangentially to the bottom limit plane.
References Cited UNITED STATES PATENTS 3,362,499 1/1968 Tripp 180121 FOREIGN PATENTS 1,001,058 8/ 1965 Great Britain.
ANDREW H. FARRELL, Primary Examiner
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR107999A FR1537727A (en) | 1967-05-26 | 1967-05-26 | Confined air cushion shell |
Publications (1)
Publication Number | Publication Date |
---|---|
US3518956A true US3518956A (en) | 1970-07-07 |
Family
ID=8631703
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US729714A Expired - Lifetime US3518956A (en) | 1967-05-26 | 1968-05-16 | Bubble hulls |
Country Status (3)
Country | Link |
---|---|
US (1) | US3518956A (en) |
FR (1) | FR1537727A (en) |
GB (1) | GB1223713A (en) |
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3742888A (en) * | 1971-12-30 | 1973-07-03 | W Crowley | Stable multiple-chamber air cushion boat hull |
JPS5058791A (en) * | 1973-09-20 | 1975-05-21 | ||
US4090459A (en) * | 1977-03-25 | 1978-05-23 | Textron Inc. | Side lubricated seal device for a surface effect ship |
FR2387148A1 (en) * | 1977-04-15 | 1978-11-10 | Mattox Darryl | WATER SUPPORTED SIDE WALL AIR CUSHION VEHICLE |
US4393802A (en) * | 1980-05-16 | 1983-07-19 | Rizzo Salvatore A | Boat hull with underside channel |
US4739719A (en) * | 1976-11-01 | 1988-04-26 | Burg Donald E | Movable bow seal air ride boat hull |
US5000107A (en) * | 1976-11-01 | 1991-03-19 | Burg Donald E | Extended bow and multiple air cushion air ride boat hull |
WO1992013753A1 (en) * | 1988-04-19 | 1992-08-20 | Donald Earl Burg | Multiple cushion air ride boat hull |
DE3490269C2 (en) * | 1983-06-07 | 1995-08-31 | Sjoerd Meijer | Vessel with adjustable draught |
US5611294A (en) * | 1976-11-01 | 1997-03-18 | Paulette Renee Burg | Multihulled air cushioned marine vehicle |
US5626669A (en) * | 1976-11-01 | 1997-05-06 | Paulette Renee Burg | High efficiency marine vehicle |
US20040154514A1 (en) * | 1999-09-01 | 2004-08-12 | Burg Donald E. | Air lubricated ship |
US6957620B1 (en) | 2004-12-30 | 2005-10-25 | Wheeler Robert L | Self-generating air cushion vessel |
US6981460B1 (en) | 2003-12-23 | 2006-01-03 | Robert L Wheeler | Self-Generating Air Cushion Vessel |
CN101412435B (en) * | 2002-05-07 | 2011-10-05 | Dk集团荷属安的列斯群岛公司 | Air cavity vessel |
KR20150082697A (en) * | 2012-02-21 | 2015-07-15 | 실버스트림 테크놀러지스 비.브이. | Air lubrication system |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1361150A1 (en) * | 2002-05-07 | 2003-11-12 | DK Group N.A. N.V. | Air cavity vessel with wedge-shaped cavities, longitudinally offset cavities, and roll control means |
EP1361152A1 (en) * | 2002-05-07 | 2003-11-12 | DK Group N.A. N.V. | Air cavity vessel with wedge-shaped cavities, longitudinally offset cavities, and roll control means |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1001058A (en) * | 1910-05-31 | 1911-08-22 | Frederick Mayer | Wheel. |
US3362499A (en) * | 1964-01-30 | 1968-01-09 | Hovercraft Dev Ltd | Vehicles for travelling over a surface |
-
1967
- 1967-05-26 FR FR107999A patent/FR1537727A/en not_active Expired
-
1968
- 1968-05-16 US US729714A patent/US3518956A/en not_active Expired - Lifetime
- 1968-05-16 GB GB23421/68A patent/GB1223713A/en not_active Expired
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1001058A (en) * | 1910-05-31 | 1911-08-22 | Frederick Mayer | Wheel. |
US3362499A (en) * | 1964-01-30 | 1968-01-09 | Hovercraft Dev Ltd | Vehicles for travelling over a surface |
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3742888A (en) * | 1971-12-30 | 1973-07-03 | W Crowley | Stable multiple-chamber air cushion boat hull |
JPS5058791A (en) * | 1973-09-20 | 1975-05-21 | ||
US5626669A (en) * | 1976-11-01 | 1997-05-06 | Paulette Renee Burg | High efficiency marine vehicle |
US4739719A (en) * | 1976-11-01 | 1988-04-26 | Burg Donald E | Movable bow seal air ride boat hull |
US5000107A (en) * | 1976-11-01 | 1991-03-19 | Burg Donald E | Extended bow and multiple air cushion air ride boat hull |
US5611294A (en) * | 1976-11-01 | 1997-03-18 | Paulette Renee Burg | Multihulled air cushioned marine vehicle |
US4090459A (en) * | 1977-03-25 | 1978-05-23 | Textron Inc. | Side lubricated seal device for a surface effect ship |
FR2387148A1 (en) * | 1977-04-15 | 1978-11-10 | Mattox Darryl | WATER SUPPORTED SIDE WALL AIR CUSHION VEHICLE |
US4227475A (en) * | 1977-04-15 | 1980-10-14 | Mattox Darryl F | Waterborne sidewall air cushion vehicle |
US4393802A (en) * | 1980-05-16 | 1983-07-19 | Rizzo Salvatore A | Boat hull with underside channel |
DE3490269C2 (en) * | 1983-06-07 | 1995-08-31 | Sjoerd Meijer | Vessel with adjustable draught |
WO1992013753A1 (en) * | 1988-04-19 | 1992-08-20 | Donald Earl Burg | Multiple cushion air ride boat hull |
WO1998050270A1 (en) * | 1995-06-07 | 1998-11-12 | Burg Donald E | High efficiency marine vehicle |
US20040154514A1 (en) * | 1999-09-01 | 2004-08-12 | Burg Donald E. | Air lubricated ship |
CN101412435B (en) * | 2002-05-07 | 2011-10-05 | Dk集团荷属安的列斯群岛公司 | Air cavity vessel |
US6981460B1 (en) | 2003-12-23 | 2006-01-03 | Robert L Wheeler | Self-Generating Air Cushion Vessel |
US6957620B1 (en) | 2004-12-30 | 2005-10-25 | Wheeler Robert L | Self-generating air cushion vessel |
KR20150082697A (en) * | 2012-02-21 | 2015-07-15 | 실버스트림 테크놀러지스 비.브이. | Air lubrication system |
Also Published As
Publication number | Publication date |
---|---|
GB1223713A (en) | 1971-03-03 |
FR1537727A (en) | 1968-08-30 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3518956A (en) | Bubble hulls | |
CN100379645C (en) | Air cavity vessel with wedge-shaped cavities, longitudinally offset cavities, and roll control means and method for constructing the same | |
US4004542A (en) | Waterjet propelled planing hull | |
KR840002724A (en) | Pressure tank for liquid transportation and storage | |
US3399645A (en) | Tanker construction | |
SE8006524L (en) | DOUBLE-HULL VESSELS | |
ES322735A1 (en) | Boats | |
GB1180482A (en) | A Vessel Partly Supported by Water and Partly by Static Air | |
ES338762A1 (en) | Method for rebuilding the hull of a ship to increase its tonnage | |
GB1190621A (en) | Improvements in or relating to Ships and Boats. | |
KR20060057003A (en) | Container ship | |
US3083672A (en) | Stabilization system | |
US3083673A (en) | Passive stabilization system | |
US3511204A (en) | Method and apparatus for steering twin hulled vessels | |
KR960029193A (en) | Ship with fuel tank adjacent to hull and method of operation | |
US3382945A (en) | Devices supported by air cushions | |
GB1194510A (en) | Improvements in or relating to Ship Steering Devices | |
GB1052497A (en) | ||
GB1067201A (en) | Roll stabilization system for vessels | |
US3093843A (en) | Water bug boat | |
US2974624A (en) | Ship | |
US1776336A (en) | Float construction for hydroplanes | |
US2520645A (en) | Ship hull construction | |
RU210661U1 (en) | Inflatable motorboat with sponsons | |
US2918032A (en) | Tanker bulkhead and compartment construction |