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US20050005835A1 - Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water - Google Patents

Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water Download PDF

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Publication number
US20050005835A1
US20050005835A1 US10/886,820 US88682004A US2005005835A1 US 20050005835 A1 US20050005835 A1 US 20050005835A1 US 88682004 A US88682004 A US 88682004A US 2005005835 A1 US2005005835 A1 US 2005005835A1
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United States
Prior art keywords
hydrofoil
ground
wing
water
passenger
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Abandoned
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US10/886,820
Inventor
Dwight Brass
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Individual
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Individual
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Priority to US10/886,820 priority Critical patent/US20050005835A1/en
Publication of US20050005835A1 publication Critical patent/US20050005835A1/en
Priority to US11/264,602 priority patent/US7275493B1/en
Abandoned legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60VAIR-CUSHION VEHICLES
    • B60V1/00Air-cushion
    • B60V1/08Air-cushion wherein the cushion is created during forward movement of the vehicle by ram effect

Definitions

  • Hydrofoil designs typically allow higher speed travel over water and include somewhat complicated designs to maintain level and controlled motion. Although some also use adjustable foils, this design overcomes the limitations in required draft with a flush-retractible “V” design. This configuration also provides automatic leveling since the left, or right, segment of the “V” is immersed deeper, or shallower, depending on the lean of the vessel. As the segment is immersed deeper, it provides more lift, and thus automatically levels the vessel.
  • the object of this invention is to provide rapid, safe, comfortable, and economical transportation over water.
  • the Hybrid WIG design operates in three modes, displacement, hydrofoil, and “ground-effect”, depending on speed.
  • the hydrofoil “V” wing is completely retracted flush with the bottom of the vessel. This allows operation in close proximity to shoreline, and allows the vessel to be “beached” if desired.
  • the wing can be gradually extended, depending on water depth and speed. As the vessel increases in speed the lift from the wing increases, and eventually provides 100% of the required lift. The vessel hull then lifts clear of the water and is now operating in hydrofoil mode. As speed further increases, lift from the hull shape (airfoil) increases lifting the vessel further above the water. This process continues until the airfoil is providing 100% of the lift, and the wing is then retracted for wing-in-ground mode. High speeds are then possible with a highly streamlined vessel, propelled by twin aircraft engines/propellers. Studies have shown that lift from wing-in-ground operation is approximately double that obtained by a similar airfoil operating above the ground-effect zone.
  • FIG. 1 Perspective view of craft with hidden lines removed for clarity.
  • FIG. 2 Top view of vessel, showing twin aircraft engines and propellers ( 1 ) and side cabin access door ( 2 ).
  • FIG. 3 Front view of vessel showing airfoil cabin ( 3 ) and hydrofoil wing in fully deployed, or extended, position. Location of Section AA is also shown.
  • FIG. 4 Side view of vessel showing engines and propellers ( 1 ), cabin access door ( 2 ), airfoil shaped cabin ( 3 ) and hydrofoil in fully deployed, or extended, position.
  • FIG. 5 Front view of hydrofoil in retracted position. Cabin is shown in phantom. Also, hydrofoil is shown in phantom as extended.
  • FIG. 6 Section AA of the hydrofoil wing showing foil shape creating lift.
  • the hybrid hydrofoil vessel hull is constructed using standard reinforced fiberglass techniques, with reinforced frame for rigid attachment of engines and hydrofoil wing.
  • the adjustment of the foil is accomplished with a vertical sliding arm that extends downward for deployment and receeds into the cabin for retraction. When fully retracted the wing is flush with the underside of the airfoil shaped cabin allowing a streamlined shape for very low drag.
  • Aircraft propellers are used of the “constant velocity” type with reversable thrust capability. Each motor and prop are individually controllable and are used for directional control, including reverse maneuvering at slow speeds. In addition, elevator surfaces are located at the rear of the vessel providing angle-of-attack trim at moderate and high speeds.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)

Abstract

This design is for a passenger watercraft that can operate in three modes, displacement, hydrofoil, and ground-effect (wing-in-ground, WIG), over a wide range of speeds up to 150 MPH. It also has the capability of approach and land on a beach due to the unique retractable wing design and reversable propellers for “backing out”.

Description

    CROSS-REFERENCE TO RELATED APPLICATIONS
  • This application follows Provisional Application No. 60/486,152, with filing date of Jul. 10, 2003 which is claimed for this application.
  • Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water. Craft lift provided by displacement at low speeds and when not moving. At moderate speeds lift is provided by a retractable “v” hydrofoil. At high speed, the hydrofoil wing is retracted into the hull and lift comes entirely from the ground effect, a high pressure area is formed between the rapidly moving hull and the water surface beneath. The ship hull is in the form of an airfoil (wing). Propulsion is provided by two aircraft engines fitted with reversible pitch propellers. Directional control is provided by elevators and rudder.
    Name of inventor: Dwight S. Brass
    Citizenship: United States of America
    Residence of inventor: 400 East Richardson Springs Road
    Edgerton, Wisconsin 53534 USA
    Ph 608-884-6289
  • STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
  • Not applicable
  • REFERENCE TO SEQUENCE LISTING, A TABLE, OR A COMPUTER PROGRAM LISTING COMPACT DISK APPENDIX
  • Not applicable
  • BACKGROUND OF THE INVENTION
  • Hydrofoil typical designs
  • Hydrofoil designs typically allow higher speed travel over water and include somewhat complicated designs to maintain level and controlled motion. Although some also use adjustable foils, this design overcomes the limitations in required draft with a flush-retractible “V” design. This configuration also provides automatic leveling since the left, or right, segment of the “V” is immersed deeper, or shallower, depending on the lean of the vessel. As the segment is immersed deeper, it provides more lift, and thus automatically levels the vessel.
  • Patents on Hydrofoil or Wing-In-Ground Vessels
  • All patents discovered involved relatively complex control features designed to overcome typical designs described above. All hydrofoil, or ground-effect designs also used propulsion with propellers underwater. This design uses dual aircraft engines and propellers operating in air. During high speed operation, no part of the vessel is in water, thus eliminating the possibility of striking floating debris.
  • The following hydrofoil or wing-in-ground patents were identified
    Patent Nbr Date Inventor Classification
    4,151,893 May 1979 Mantle 180/116
    5,950,559 Sep 1999 Klem 114/272
    6,230,835 May 2001 Fisher 180/117
    4,660,670 Apr 1987 Mattox 180/117
    6,719,079 Apr 2004 Jones 180/126
    6,318,489 Nov 2001 McGill 180/164
    6,216,599 Apr 2001 Cavanagh 104/23.2
    RE28,955 Jul 1975 Stanberry 114/55.55
    5,860,383 Jan 1999 Whitener 114/271
    5,794,558 Aug 1998 Loui 114/274
    5,544,607 Aug 1996 Rorabaugh 114/123
    6,325,011 Dec 2001 Klen 114/272
    6,732,672 May 2004 Shin 114/272
  • Specific Problems With Current Hydrofoil Designs
  • Current designs have operational limitations, reliability issues, and cost factors that are greatly improved upon by this design. Most current designs have significant draft requirements limiting their ability to operate in very shallow water. Also, unless they have a retractible wing and can transition to a wing-in-ground mode, they are vulnerable to damage from floating debris, especially at high speed. Hydrofoil designs also have significant speed limitations due to violent cavitation at higher speeds. The literature identifies only experimental craft that can reach speeds of about 80 MPH. This hybrid WIG (wing-in-ground, or ground-effect) design allows speeds of approximately 150 MPH, with no danger of hitting floating debris. Since all components of the design are entirely out of the water, design is much simpler, and maintainance is drastically reduced.
  • BRIEF SUMMARY OF THE INVENTION
  • The object of this invention is to provide rapid, safe, comfortable, and economical transportation over water. The Hybrid WIG design operates in three modes, displacement, hydrofoil, and “ground-effect”, depending on speed.
  • Operation
  • At dockside and/or in shallow water, the hydrofoil “V” wing is completely retracted flush with the bottom of the vessel. This allows operation in close proximity to shoreline, and allows the vessel to be “beached” if desired. Once the vessel is underway, and speed is increased, the wing can be gradually extended, depending on water depth and speed. As the vessel increases in speed the lift from the wing increases, and eventually provides 100% of the required lift. The vessel hull then lifts clear of the water and is now operating in hydrofoil mode. As speed further increases, lift from the hull shape (airfoil) increases lifting the vessel further above the water. This process continues until the airfoil is providing 100% of the lift, and the wing is then retracted for wing-in-ground mode. High speeds are then possible with a highly streamlined vessel, propelled by twin aircraft engines/propellers. Studies have shown that lift from wing-in-ground operation is approximately double that obtained by a similar airfoil operating above the ground-effect zone.
  • BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING
  • FIG. 1 Perspective view of craft with hidden lines removed for clarity.
  • FIG. 2 Top view of vessel, showing twin aircraft engines and propellers (1) and side cabin access door (2).
  • FIG. 3 Front view of vessel showing airfoil cabin (3) and hydrofoil wing in fully deployed, or extended, position. Location of Section AA is also shown.
  • FIG. 4 Side view of vessel showing engines and propellers (1), cabin access door (2), airfoil shaped cabin (3) and hydrofoil in fully deployed, or extended, position.
  • FIG. 5 Front view of hydrofoil in retracted position. Cabin is shown in phantom. Also, hydrofoil is shown in phantom as extended.
  • FIG. 6 Section AA of the hydrofoil wing showing foil shape creating lift.
  • DETAILED DESCRIPTION OF THE INVENTION
  • The hybrid hydrofoil vessel hull is constructed using standard reinforced fiberglass techniques, with reinforced frame for rigid attachment of engines and hydrofoil wing. A jointed double wing, V shaped, with a pivot in the center and at each end allow retraction and deployment of the wing. The adjustment of the foil is accomplished with a vertical sliding arm that extends downward for deployment and receeds into the cabin for retraction. When fully retracted the wing is flush with the underside of the airfoil shaped cabin allowing a streamlined shape for very low drag.
  • Aircraft propellers are used of the “constant velocity” type with reversable thrust capability. Each motor and prop are individually controllable and are used for directional control, including reverse maneuvering at slow speeds. In addition, elevator surfaces are located at the rear of the vessel providing angle-of-attack trim at moderate and high speeds.

Claims (5)

1. What I claim as my invention is the filly adjustable V-shaped hydrofoil watercraft wing that is fully retractable into the vessel hull.
2. What I claim as my invention is a geometry configuration for the retractable hydrofoil wing that eliminates the necessity for any high speed bearings, cables, motors, or other equipment that must be exposed to the water. Only two (2) pivot bearings are submerged and only during slow speed operation (displacement mode, and hydrofoil mode). During high speed operation, that would normally involve risk of collision and wear and tear on components, all movable segments of the design are out of the water.
3. What I claim as my invention is a passenger hybrid hydrofoil vessel that is capable of operating in three modes, displacement, hydrofoil, and ground-effect.
4. What I claim as my invention is a passenger hybrid hydrofoil vessel with fully retractable foil design allowing operation in shallow water at low speeds.
5. What I claim as my invention is a passenger hybrid hydrofoil vessel that utilizes aircraft-style engines with propulsion entirely from propellers operating in air, not water. This greatly reduces initial cost of manufacture, as well as avoiding high maintainence due to water immersion
US10/886,820 2003-07-10 2004-07-08 Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water Abandoned US20050005835A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US10/886,820 US20050005835A1 (en) 2003-07-10 2004-07-08 Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water
US11/264,602 US7275493B1 (en) 2004-07-08 2005-11-01 Hydrofoil watercraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US48615203P 2003-07-10 2003-07-10
US10/886,820 US20050005835A1 (en) 2003-07-10 2004-07-08 Passenger watercraft using three methods of lift; displacement, hydrofoil, and ground-effect (wing-in-ground) operating over water

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US11/264,602 Continuation-In-Part US7275493B1 (en) 2004-07-08 2005-11-01 Hydrofoil watercraft

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US20050005835A1 true US20050005835A1 (en) 2005-01-13

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105235817A (en) * 2015-10-26 2016-01-13 陈俞任 Airship

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991747A (en) * 1959-05-29 1961-07-11 Bader John Hydrofoil retraction and steering mechanism
US3139059A (en) * 1961-12-11 1964-06-30 Fairchild Stratos Corp Winged hydrofoil watercraft
US3150626A (en) * 1962-10-23 1964-09-29 Outboard Marine Corp Hydrofoil attachment for boats
US3762355A (en) * 1970-07-27 1973-10-02 Rohr Corp Water craft with aerodynamic lift
US3785319A (en) * 1971-06-11 1974-01-15 Markus R Hydrofoil vessel
US4080922A (en) * 1975-09-08 1978-03-28 Brubaker Curtis M Flyable hydrofoil vessel

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991747A (en) * 1959-05-29 1961-07-11 Bader John Hydrofoil retraction and steering mechanism
US3139059A (en) * 1961-12-11 1964-06-30 Fairchild Stratos Corp Winged hydrofoil watercraft
US3150626A (en) * 1962-10-23 1964-09-29 Outboard Marine Corp Hydrofoil attachment for boats
US3762355A (en) * 1970-07-27 1973-10-02 Rohr Corp Water craft with aerodynamic lift
US3785319A (en) * 1971-06-11 1974-01-15 Markus R Hydrofoil vessel
US4080922A (en) * 1975-09-08 1978-03-28 Brubaker Curtis M Flyable hydrofoil vessel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105235817A (en) * 2015-10-26 2016-01-13 陈俞任 Airship

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