US3750978A - Skyboat - Google Patents
Skyboat Download PDFInfo
- Publication number
- US3750978A US3750978A US00174653A US3750978DA US3750978A US 3750978 A US3750978 A US 3750978A US 00174653 A US00174653 A US 00174653A US 3750978D A US3750978D A US 3750978DA US 3750978 A US3750978 A US 3750978A
- Authority
- US
- United States
- Prior art keywords
- skyboat
- ski
- craft
- fuselage
- water
- 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
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 17
- 230000010006 flight Effects 0.000 claims description 2
- 241000218645 Cedrus Species 0.000 description 1
- 230000004308 accommodation Effects 0.000 description 1
- 230000033001 locomotion Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Images
Classifications
-
- 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
- B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
- B63B1/18—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydroplane type
- B63B1/22—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydroplane type with adjustable planing surfaces
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/22—Air-cushion provided with hydrofoils
-
- 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
- B63B1/322—Other means for varying the inherent hydrodynamic characteristics of hulls using aerodynamic elements, e.g. aerofoils producing a lifting force
-
- 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
- ABSTRACT A skyboat is provided which consists of an airplane-like structure having limited lift wings and a trailing ski which is ordinarily in contact with water. A high speed, efficient, safe craft for the transportation of people and cargo is thus provided.
- the present invention relates to a skyboat which combines some of the best features of the airplane and the boat. It is much more efficient than either a hydrofoil, which requires a substantial amount of energy to overcome water friction, or air cushion vehicles which require a large amount of energy to keep them supported.
- the craft of the present invention is much faster than conventional boats since it moves almost entirely through the air.
- it is much safer than the conventional airplane since it almost always maintains contact with water.
- it can be operated under conditions of low ceiling and poor visibility which would preclude the use of an airplane. Since it operates close to the water, it can be piloted by a much less skilled pilot than would be necessary for an airplane.
- the objects of the invention areobtained by providing an airplane-like structure with limited lift wings which has a ski which trails in the water on a small keel.
- the elevator is located at the front of the plane rather than the rear as is the case in conventional airplanes.
- FIG. 1 is a plan view of a skyboat embodying the present invention.
- FIG. 2 is a side elevation of the skyboat shown in FIG. 1.
- FIG. 3 is a front elevation of the skyboat of FIG. 1.
- a ski mounteded under the fuselage 7 is a ski generally designated 33 which is provided with a locking hinge 35 and a spring structure 37 which tends to push the ski downwardly and maintain it in the position generally shown in solid lines of FIG. 2.
- Hinge 35 is locked in the down position when the skyboat is in a moving position which will help raise boat to an operating position and maintain that position in flight.
- the hinge is unlocked, permitting the spring and keel to conform to the hull of the boat in the closed position.
- the bottom end of the ski is provided with a small keel section 39 and may include also a small horizontal section 41 which helps support the plane although the ski is not primarily for support purposes.
- FIG. 5 The action of the skyboat can be seen in FIG. 5 wherein a skyboat is shown in various positions at the trough and crests of a wave. It will be seen that the center view shows the craft entirely unsupported by water but the two end views show the craft supported on the crests of the wave. Thus, although the skyboat will not normally fly with its ski out of contact with the water,
- FIG. 4 is an enlarged perspective view of the end of the ski which is employed with the skyboat.
- FIG. 5 is a diagrammatic view showing how the skyboat stays level in the presence of high wave action.
- FIG. 6 is a side view of a large skyboat suitable for long range commercial service.
- the skyboat includes a hull or fuselage generally designated 7 to which is attached a tail section 9, a wing section 11 and an elevator section 13.
- a propulsion section 15 is attached at the center of the wing and includes a conventional propeller 17. Although the device could be jet propelled, the operating speed is such that it would be normal to employ propeller propulsion and particularly turbo-propeller propulsion.
- the fuselage 7 is provided with a passenger compartment 19 and a windshield 21 for the accommodation of a pilot and/or one or more passengers.
- the wing 11 includes a main wing portion 23 which is provided with the conventional ailerons 25 at the trailing edge.
- the wing sections 23 are relatively small compared with those of a usual airplane and might be described as limited lift wings which will barely support the skyboat at maximum speed.
- the tail section 9 is conventional except that it includes only the rudder 27 and does not include the elevator which is common with airplane tails.
- the elevator 13 is mounted near the front of the craft and includes the main elevator section 29 which in turn is supplied with small ailerons or elevators 31. It will be underpletely airborne.
- FIG. 5 a much larger craft of the commercial type is shown but it will be seen that essentially it has the same parts as were previously described. Thus, it has a large cabin portion 43, propulsion section 45, wing 47, a forward elevator 49 and ski 51. Again the rudder 53 does not include the elevator of the conventional airplane.
- the elevators normally found in the tail of an airplane are provided up forward to give more lift to the front end of the skyboat. However, it is possible to em ploy elevators at the rear although this is a less preferred method.
- the propeller has been shown as a pusher and it is obvious that this is merely for convenience and it might be of the more conventional forward configuration. Also it has been assumed that a jet prop engine would be used but a reciprocating engine might be used with the propeller or a pure jet propulsion system might be employed. In some instances it might be desirable to provide a guard around the pro peller for the protection of personnel.
- the limited lift wings are relatively short which will prevent the craft from lifting completely out of the water under normalconditions.
- the skyboat normally travels under a semi-stall position and it might be compared with an airplane in its landing position. Nevertheless, there are some conditions, such as shown in FIG. 5, wherein the craft could be airborne for short periods of time so that wave action is effectively damped out.
- the ski When the craft lands, the ski folds up under the action of the spring to the position shown in dot dash lines in FIG. 2 and is waterborne in the same manner as a conventional hydroplane.
- a specific configuration of spring is shown, this is not necessary and the shaft itself of the ski could provide the necessary springing.
- the keel-like section 39 is very helpful in preventing the plane from skidding sideways, particularly in turns.
- the ski is provided for both lift and guiding and it also provides support for the plane in motion.
- the springiness of the ski 33 is sufficient so that it will absorb shocks, especially when traveling under high speed conditions over choppy water and in landing.
- FIGS. 1 through 5 Although the skyboat described in FIGS. 1 through 5 is obviously a very small vehicle, it can be made enlarged configuration for commercial purposes as is shown in FIG. 6.
- An airplane-like craft or skyboat adapted for over water flights having in combination:
- a fuselage adapted to float on water and fly through the air
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Ocean & Marine Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Toys (AREA)
Abstract
A skyboat is provided which consists of an airplane-like structure having limited lift wings and a trailing ski which is ordinarily in contact with water. A high speed, efficient, safe craft for the transportation of people and cargo is thus provided.
Description
United States Patent 11 1 Cunningham Aug. 7, 1973 [54] SKYBOAT 2,693,325 11/1954 Lippisch 244 45 R x [76] Inventor: Byron H. Cunningham, 1013 Cedar 3 fi Santa Cruz, (3314- 95060 2,692,096 10/1954 Pierce 244/2 x Filed: Aug. 25, 1971 App]. No.: l74,653
U.S. Cl. 244/2 Int. Cl. B64c 37/00 Field of Search 244/2, 41, 45, 46,
References Cited UNITED STATES PATENTS 3/1972 Eickmann 244/2 X 3/1973 Cardwell et al 244/2 Primary ExaminerMilton Buchler Assistant ExaminerCarl A. Rutledge Attorney-Carl Hoppe, Robert G, Slick et al.
[57] ABSTRACT A skyboat is provided which consists of an airplane-like structure having limited lift wings and a trailing ski which is ordinarily in contact with water. A high speed, efficient, safe craft for the transportation of people and cargo is thus provided.
2 Claims, 6 Drawing Figures 2) H 335 I7 9 27 I3 29 51/97 PAIENIED M 3. 750.978
sum 2 or 2 I N VENTOR.
BV/ZON H. CUNNINGHAM SKYBOAT SUMMARY OF THE INVENTION The present invention relates to a skyboat which combines some of the best features of the airplane and the boat. It is much more efficient than either a hydrofoil, which requires a substantial amount of energy to overcome water friction, or air cushion vehicles which require a large amount of energy to keep them supported. The craft of the present invention is much faster than conventional boats since it moves almost entirely through the air. On the other hand, it is much safer than the conventional airplane since it almost always maintains contact with water. Naturally it can be operated under conditions of low ceiling and poor visibility which would preclude the use of an airplane. Since it operates close to the water, it can be piloted by a much less skilled pilot than would be necessary for an airplane.
In general the objects of the invention areobtained by providing an airplane-like structure with limited lift wings which has a ski which trails in the water on a small keel. In a preferred embodiment of the invention the elevator is located at the front of the plane rather than the rear as is the case in conventional airplanes.
Other features of the invention will be brought out in the detailed specification which follows.
BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a plan view of a skyboat embodying the present invention.
FIG. 2 is a side elevation of the skyboat shown in FIG. 1.
FIG. 3 is a front elevation of the skyboat of FIG. 1.
stood that in a conventional airplane the elevators are at the rear and tend to push the plane down as the power pulls the plane up. However, in the present invention, by providing elevators at the front of the structure the nose is pulled up by the elevator action to maintain the craft on an even keel.
Mounted under the fuselage 7 is a ski generally designated 33 which is provided with a locking hinge 35 and a spring structure 37 which tends to push the ski downwardly and maintain it in the position generally shown in solid lines of FIG. 2. Hinge 35 is locked in the down position when the skyboat is in a moving position which will help raise boat to an operating position and maintain that position in flight. When landing the boat on the water surface, the hinge is unlocked, permitting the spring and keel to conform to the hull of the boat in the closed position. The bottom end of the ski is provided with a small keel section 39 and may include also a small horizontal section 41 which helps support the plane although the ski is not primarily for support purposes.
The action of the skyboat can be seen in FIG. 5 wherein a skyboat is shown in various positions at the trough and crests of a wave. It will be seen that the center view shows the craft entirely unsupported by water but the two end views show the craft supported on the crests of the wave. Thus, although the skyboat will not normally fly with its ski out of contact with the water,
wave action may be such that temporarily it is com FIG. 4 is an enlarged perspective view of the end of the ski which is employed with the skyboat.
FIG. 5 is a diagrammatic view showing how the skyboat stays level in the presence of high wave action.
FIG. 6 is a side view of a large skyboat suitable for long range commercial service.
DESCRIPTION OF THE PREFERRED EMBODIMENTS Referring to the drawings by reference characters and particularly FIGS. 1 through 5, the skyboat includes a hull or fuselage generally designated 7 to which is attached a tail section 9, a wing section 11 and an elevator section 13. A propulsion section 15 is attached at the center of the wing and includes a conventional propeller 17. Although the device could be jet propelled, the operating speed is such that it would be normal to employ propeller propulsion and particularly turbo-propeller propulsion. The fuselage 7 is provided with a passenger compartment 19 and a windshield 21 for the accommodation of a pilot and/or one or more passengers. The wing 11 includes a main wing portion 23 which is provided with the conventional ailerons 25 at the trailing edge. The wing sections 23 are relatively small compared with those of a usual airplane and might be described as limited lift wings which will barely support the skyboat at maximum speed.
The tail section 9 is conventional except that it includes only the rudder 27 and does not include the elevator which is common with airplane tails. The elevator 13 is mounted near the front of the craft and includes the main elevator section 29 which in turn is supplied with small ailerons or elevators 31. It will be underpletely airborne.
In FIG. 5 a much larger craft of the commercial type is shown but it will be seen that essentially it has the same parts as were previously described. Thus, it has a large cabin portion 43, propulsion section 45, wing 47, a forward elevator 49 and ski 51. Again the rudder 53 does not include the elevator of the conventional airplane.
,It is believed apparent from the foregoing that I have provided a skyboat which combines certain of the advantages of conventional boat with those of an airplane without involving the disadvantages of the hydrofoil or the air cushion vehicle. The device is capable of traveling at high speed in inclement weather and with a relatively unskilled pilot. a
The elevators normally found in the tail of an airplane are provided up forward to give more lift to the front end of the skyboat. However, it is possible to em ploy elevators at the rear although this is a less preferred method.
In the drawings the propeller has been shown as a pusher and it is obvious that this is merely for convenience and it might be of the more conventional forward configuration. Also it has been assumed that a jet prop engine would be used but a reciprocating engine might be used with the propeller or a pure jet propulsion system might be employed. In some instances it might be desirable to provide a guard around the pro peller for the protection of personnel.
The limited lift wings are relatively short which will prevent the craft from lifting completely out of the water under normalconditions. Thus the skyboat normally travels under a semi-stall position and it might be compared with an airplane in its landing position. Nevertheless, there are some conditions, such as shown in FIG. 5, wherein the craft could be airborne for short periods of time so that wave action is effectively damped out.
When the craft lands, the ski folds up under the action of the spring to the position shown in dot dash lines in FIG. 2 and is waterborne in the same manner as a conventional hydroplane. Although a specific configuration of spring is shown, this is not necessary and the shaft itself of the ski could provide the necessary springing. The keel-like section 39 is very helpful in preventing the plane from skidding sideways, particularly in turns. The ski is provided for both lift and guiding and it also provides support for the plane in motion. The springiness of the ski 33 is sufficient so that it will absorb shocks, especially when traveling under high speed conditions over choppy water and in landing.
Although the skyboat described in FIGS. 1 through 5 is obviously a very small vehicle, it can be made enlarged configuration for commercial purposes as is shown in FIG. 6.
It is obvious that many departures can be made from the exact structure shown without departing from the spirit of this invention.
1 claim:
1. An airplane-like craft or skyboat adapted for over water flights having in combination:
a. a fuselage adapted to float on water and fly through the air,
b. means for propelling said fuselage through the air,
c. wings mounted on said skyboat, said wings being adapted to support said craft as it moves forward through the air, said wings being of relatively small size and having a to lift 40 prevent the skyboat from becoming completely airborne under normal conditions,
d. a ski hingedly mounted on a stiff arm near the front of said fuselage and extending to the rear, said hinge permitting said ski to extend downwardly and rearwardly of the hinge point into contact with the water when said skyboat is airborne and to fold along the bottom of said fuselage when said craft is waterborne,
e. locking means whereby said hinge can be locked in the down position, and
f. spring means normally urging said ski downwardly whereby the ski tends to support the skyboat.
2. The structure of claim 1 wherein the skyboat has an elevator mounted ahead of the wing.
Claims (2)
1. An airplane-like craft or skyboat adapted for over water flights having in combination: a. a fuselage adapted to float on water and fly through the air, b. means for propelling said fuselage through the air, c. wings mounted on said skyboat, said wings being adapted to support said craft as it moves forward through the air, said wings being of relatively small size and having a to lift 4o prevent the skyboat from becoming completely airborne under normal conditions, d. a ski hingedly mounted on a stiff arm near the front of said fuselage and extending to the rear, said hinge permitting said ski to extend downwardly and rearwardly of the hinge point into contact with the water when said skyboat is airborne and to fold along the bottom of said fuselage when said craft is waterborne, e. locking means whereby said hinge can be locked in the down position, and f. spring means normally urging said ski downwardly whereby the ski tends to support the skyboat.
2. The structure of claim 1 wherein the skyboat has an elevator mounted ahead of the wing.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US17465371A | 1971-08-25 | 1971-08-25 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US3750978A true US3750978A (en) | 1973-08-07 |
Family
ID=22636981
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US00174653A Expired - Lifetime US3750978A (en) | 1971-08-25 | 1971-08-25 | Skyboat |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US3750978A (en) |
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3960103A (en) * | 1973-06-04 | 1976-06-01 | Herbert Rey | Marine skimmer craft |
| JPS5272300U (en) * | 1975-11-25 | 1977-05-30 | ||
| US5267626A (en) * | 1991-08-29 | 1993-12-07 | Tanfield Jr Theodore W | Near surface vehicle |
| EP1524181A1 (en) * | 2003-10-13 | 2005-04-20 | Mongkol Jesadanont | Hydroplane boat with outboard propulsion |
| US20050230535A1 (en) * | 2004-04-13 | 2005-10-20 | Lockheed Martin Corporation | Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea |
| GB2493789A (en) * | 2011-07-09 | 2013-02-20 | Colin Hilton | Ground effect planing watercraft with a stabilizing hydro-ski |
| AT516822A1 (en) * | 2015-01-19 | 2016-08-15 | Steinkogler Peter | sailboat |
| US9487269B1 (en) * | 2015-11-25 | 2016-11-08 | Richard Chutter | Aerodynamically buoyant vehicle |
| US20230062717A1 (en) * | 2021-02-11 | 2023-03-02 | REGENT Craft Inc. | Wing-In-Ground Effect Vehicle |
| USD1090401S1 (en) | 2022-01-06 | 2025-08-26 | REGENT Craft Inc. | Winged vehicle, toy, and/or replica model thereof |
| US12420924B2 (en) | 2022-08-10 | 2025-09-23 | Regent Craft, Inc. | Hydrofoil takeoff and landing with multiple hydrofoils |
| US12420940B2 (en) | 2023-09-06 | 2025-09-23 | Regent Craft, Inc. | Hybrid propulsion for airborne craft |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2430793A (en) * | 1944-07-07 | 1947-11-11 | Curtiss Wright Corp | Aircraft elevator construction |
| US2692096A (en) * | 1951-08-06 | 1954-10-19 | All American Eng Co | Apparatus for transporting personnel and equipment |
| US2693325A (en) * | 1951-02-23 | 1954-11-02 | Collins Radio Co | Aerodynamic stabilizing and controlling means for delta wing aircraft |
| US3082975A (en) * | 1961-09-11 | 1963-03-26 | Cardwell Dick | Under-sea and heavier-than-air craft or the like |
| US3503574A (en) * | 1966-05-27 | 1970-03-31 | Karl Eickmann | Fluid power operated vehicle groups |
| US3614024A (en) * | 1970-04-06 | 1971-10-19 | Rohr Corp | Combined water surface and air craft |
-
1971
- 1971-08-25 US US00174653A patent/US3750978A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2430793A (en) * | 1944-07-07 | 1947-11-11 | Curtiss Wright Corp | Aircraft elevator construction |
| US2693325A (en) * | 1951-02-23 | 1954-11-02 | Collins Radio Co | Aerodynamic stabilizing and controlling means for delta wing aircraft |
| US2692096A (en) * | 1951-08-06 | 1954-10-19 | All American Eng Co | Apparatus for transporting personnel and equipment |
| US3082975A (en) * | 1961-09-11 | 1963-03-26 | Cardwell Dick | Under-sea and heavier-than-air craft or the like |
| US3503574A (en) * | 1966-05-27 | 1970-03-31 | Karl Eickmann | Fluid power operated vehicle groups |
| US3614024A (en) * | 1970-04-06 | 1971-10-19 | Rohr Corp | Combined water surface and air craft |
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3960103A (en) * | 1973-06-04 | 1976-06-01 | Herbert Rey | Marine skimmer craft |
| JPS5272300U (en) * | 1975-11-25 | 1977-05-30 | ||
| US5267626A (en) * | 1991-08-29 | 1993-12-07 | Tanfield Jr Theodore W | Near surface vehicle |
| EP1524181A1 (en) * | 2003-10-13 | 2005-04-20 | Mongkol Jesadanont | Hydroplane boat with outboard propulsion |
| US20050230535A1 (en) * | 2004-04-13 | 2005-10-20 | Lockheed Martin Corporation | Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea |
| US7097136B2 (en) * | 2004-04-13 | 2006-08-29 | Lockheed Martin Corporation | Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea |
| GB2493789A (en) * | 2011-07-09 | 2013-02-20 | Colin Hilton | Ground effect planing watercraft with a stabilizing hydro-ski |
| GB2493789B (en) * | 2011-07-09 | 2018-03-07 | Hilton Colin | Self-stabilising seaplane |
| AT516822A1 (en) * | 2015-01-19 | 2016-08-15 | Steinkogler Peter | sailboat |
| US9487269B1 (en) * | 2015-11-25 | 2016-11-08 | Richard Chutter | Aerodynamically buoyant vehicle |
| US20230062717A1 (en) * | 2021-02-11 | 2023-03-02 | REGENT Craft Inc. | Wing-In-Ground Effect Vehicle |
| USD1090401S1 (en) | 2022-01-06 | 2025-08-26 | REGENT Craft Inc. | Winged vehicle, toy, and/or replica model thereof |
| US12420924B2 (en) | 2022-08-10 | 2025-09-23 | Regent Craft, Inc. | Hydrofoil takeoff and landing with multiple hydrofoils |
| US12420940B2 (en) | 2023-09-06 | 2025-09-23 | Regent Craft, Inc. | Hybrid propulsion for airborne craft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3627235A (en) | Wing arrangement | |
| US4080922A (en) | Flyable hydrofoil vessel | |
| US3190582A (en) | Ground effects utilizing and transition aircraft | |
| US4691881A (en) | High performance amphibious airplane | |
| US5697468A (en) | Spoiler system for ground effect vehicles | |
| JPH08192798A (en) | Hydro-airship | |
| US3750978A (en) | Skyboat | |
| US7040574B2 (en) | Aircraft and watercraft adapted to float on main wing | |
| US5335742A (en) | Ground effect vehicle | |
| US3854679A (en) | Water-based airplane especially designed for adaptation to stol | |
| US6164591A (en) | Ground-effect flying boats also applicable to aircraft, drones, and spacecraft | |
| US3614024A (en) | Combined water surface and air craft | |
| RU2668000C1 (en) | Amphibious aircraft of "flying wing" scheme | |
| US7631609B1 (en) | Versatile watercraft | |
| US5913493A (en) | Seaplane hull | |
| US3191566A (en) | Water-borne take-off and landing craft for aircraft | |
| US2068618A (en) | Sea gyroplane | |
| US3136505A (en) | Amphibious airplane | |
| US3522785A (en) | Semiairborne vehicle | |
| RU112154U1 (en) | MULTI-PURPOSE PLANE | |
| US3636906A (en) | Hydroglyder | |
| RU2111896C1 (en) | Polyfuselage seaplane | |
| US2499350A (en) | Floating wing airplane | |
| US3253809A (en) | Ultra low speed aircraft | |
| RU2764036C1 (en) | Air transport system |