US20050112964A1 - Extruded strut, fuselage and front wing assembly for towable hydrofoil - Google Patents
Extruded strut, fuselage and front wing assembly for towable hydrofoil Download PDFInfo
- Publication number
- US20050112964A1 US20050112964A1 US10/897,363 US89736304A US2005112964A1 US 20050112964 A1 US20050112964 A1 US 20050112964A1 US 89736304 A US89736304 A US 89736304A US 2005112964 A1 US2005112964 A1 US 2005112964A1
- Authority
- US
- United States
- Prior art keywords
- fuselage
- strut
- board
- water sports
- sports device
- 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.)
- Abandoned
Links
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 16
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910000838 Al alloy Inorganic materials 0.000 claims description 5
- 210000001217 buttock Anatomy 0.000 claims description 2
- 238000000034 method Methods 0.000 description 13
- 238000001125 extrusion Methods 0.000 description 8
- 238000004519 manufacturing process Methods 0.000 description 7
- 238000005266 casting Methods 0.000 description 6
- 238000007743 anodising Methods 0.000 description 5
- 229910045601 alloy Inorganic materials 0.000 description 4
- 239000000956 alloy Substances 0.000 description 4
- 230000008901 benefit Effects 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 238000003466 welding Methods 0.000 description 4
- AZDRQVAHHNSJOQ-UHFFFAOYSA-N alumane Chemical group [AlH3] AZDRQVAHHNSJOQ-UHFFFAOYSA-N 0.000 description 3
- 238000005260 corrosion Methods 0.000 description 3
- 230000007797 corrosion Effects 0.000 description 3
- 239000011888 foil Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 229910001882 dioxygen Inorganic materials 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 229910052500 inorganic mineral Inorganic materials 0.000 description 1
- 238000005304 joining Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000003801 milling Methods 0.000 description 1
- 239000011707 mineral Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 239000011253 protective coating Substances 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000004576 sand Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000013022 venting Methods 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B32/00—Water sports boards; Accessories therefor
- B63B32/60—Board appendages, e.g. fins, hydrofoils or centre boards
- B63B32/62—Board appendages, e.g. fins, hydrofoils or centre boards characterised by the material, e.g. laminated materials; characterised by their manufacturing process
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B34/00—Vessels specially adapted for water sports or leisure; Body-supporting devices specially adapted for water sports or leisure
- B63B34/60—Arrangements for towing, e.g. for use with water-skis or wakeboards
Definitions
- These towable water sports devices have a strut, fuselage and front and rear wings or blades which are made by casting a molten aluminum alloy.
- This process requires pouring molten aluminum into a sand or steel mold.
- the alloy used in this process is a 356A aluminum which is then heat-treated to T-6 hardness.
- the casting is then ground or sanded down to eliminate all entry gates, all venting gates and the receiving canals. This requires a lot of grinding, sanding and machining of the cast part after it has been taken out of the mold. Cutting and grounding a part from a rolled or pressed aluminum billet wastes material and requires a lot of machine time.
- Another disadvantage in manufacturing using the cast process is that the metal as it cures releases or gives off gases, resulting in the production of many small voids. This porosity in the part results in a poor finish.
- the primary disadvantage of a part cast from 356A aluminum is that it does not have the ability to flex which can result in a catastrophic failure or breakage of the part. There is a large rejection rate when casting an aluminum part due to the temperature of the mold, the outside temperature, and the amount of the metal as it is poured into the mold.
- the temperature of the mold has to be compatible with the heat of the material poured into the mold and this changes on a daily basis.
- the porosity of the cast part is present on the surface of the part.
- the surface porosity of the cast part adds drag to the foil assembly, which hinders the performance of the hydrofoil assembly.
- the porosity of the cast part also is not compatible with and does not accept the anodizing process.
- the anodizing is, however, desirable in that it offers a protective, maintenance free and corrosion-resistant finish.
- a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said
- the invention uses an extruded aluminum out of a AA6061 alloy heat-treated to T-6 in advance of the extrusion.
- the 6061 heat-treated aluminum is one of the alloys to be used, but it is not the only one suitable for use in this manufacturing process.
- suitable aluminum alloys include the M 6000 series which are disclosed in Park U.S. Pat. No. 4,589,932, and Wade et al U.S. Patent No. 5,503,690, the disclosures of which are expressly incorporated herein by reference. This eliminates the need to take the casting from the foundry to a separate location for the heat-treating process. Extrusion does not involve the pouring of metal. The metal is billet or rolled aluminum is pushed or pulled through a pre-cut die.
- This grain allows the running of the grain in the long dimension of the part for added strength.
- This process eliminates the porosity (that offers no strength) and gives the part more strength with completely different characteristics.
- the extruded part can bend or flex with a memory that allows it to retain its original shape.
- the extruded part is less brittle which avoids breakage while under stress in use and danger to the rider. Eliminating the porosity on the exterior surface of the part gives it: a)more visibly aesthetics; 2) polishes up nicely; 3) less drag due to little or no porosity; and 4) it is compatible with the anodizing protective coating.
- the surface anodizing of aluminum extrusions described, for example, in Fukagawa et al U.S. Pat. No. 5,911,845.
- extruded aluminum is applicable to the strut, fuselage, front and rear blade or wing comprising the foil assembly used in a towable hydrofoil.
- FIG. 1 is a perspective view of the water sport device of this invention with the rider seated and being towed through the water by a power boat (not shown).
- FIG. 2 shows at the left a top plan view of the fuselage and front and rear planing blades, and at the right, a side view of the strut, the parts being unassembled.
- FIG. 3 shows the strut being inserted into the opening provided in the fuselage, the fuselage and planing blades being shown in longitudinal section.
- FIG. 4 shows the strut fully in place in the fuselage and welded to the fuselage.
- FIG. 5 depicts a die through which aluminum alloy is extruded to make the parts from which the strut, fuselage and planing blades are ultimately formed.
- the water sports device of this invention has a seat 10 for the rider 11 which is affixed to the curved board 12 , the strut 14 projects downwardly from board 12 in a generally perpendicular fashion.
- the lower end of strut 14 is received in opening 16 of fuselage 18 .
- the fuselage 18 carries the front planing blade 20 and rear planing blade 22 .
- a further feature of this invention concerns the combination of parts.
- the castings for the foil assembly were three different parts: 1) a t-bar consisting of strut and fuselage as a single component; 2) front wing; and 3) rear wing.
- the new means of manufacturing includes four parts: 1) the rear wing 22 ; 2) front wing 20 ; 3) the strut 14 ; and 4) the fuselage 18 .
- the strut 14 and the fuselage 18 are heliarced (a means of welding aluminum) together to form the t-bar as shown in FIG. 4 .
- the extruded strut 14 fits into the fuselage slot 24 as shown in the drawings and heliarced 26 as depicted in the drawing.
- the extrusion process also provides the capability of including the front wing 20 and rear wing 22 within the extruded fuselage 18 as a single unit, thus reducing the number of parts to two.
- the fuselage 18 and front wing 20 and rear wing 22 can be cut to the desired shape from a single aluminum extrusion using a programmable milling machine which is available in the marketplace. This reduces assembly time since the wings do not have to be joined to the fuselage in separate operations.
- the extrusions are formed by drawing hot formable aluminum through a die such as die 28 .
- the extrusion is then quenched and heat treated.
- the strut can be extruded through a die of appropriate cross section, cut to length and used as such without further working. This process conforms generally to FIG. 1 of Wakabayashi U.S. Pat. No. 5,321,967.
- the slot 24 is cut into the fuselage.
- the fuselage, wings and strut in the desired configuration are polished smooth.
- the resultant surface is quite slick and well adapted to anodizing which provides an esthetically pleasing appearance which is highly resistant to corrosion.
- the avoidance of corrosion is an important benefit of this invention in that the strut, fuselage and blades or wings remain smooth and do not acquire or build up added drag in the water over time due to oxidation and mineral build-up.
- the heliarc process is an oxygen gas mix and can be used for the welding of the extruded parts and it represents one option to be used for welding aluminum parts, but is not the only one available for this method of manufacturing.
- Other techniques for welding or joining pre-formed aluminum parts are known to those skilled in the art.
- the benefits of this invention include a less expensive part, stronger part, more consistent part and a part with less drag, increased performance, and fewer warranty problems. Extrusion has been used in other industries such as screen doors, window frames and others.
- the present invention is a completely new concept in the manufacturing of hydrofoils for water sport devices and it provides results which are not manifested in prior extruded parts.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Forging (AREA)
Abstract
A towable water sports device having a hydrofoil assembly including a strut, fuselage and front and rear blades carried by the fuselage wherein said parts are extruded aluminum.
Description
- This patent application claims the benefit of Provisional Patent Application Ser. No. 60/524,657, filed Nov. 25, 2003.
- Towable hydrofoil water sports devices for supporting a human rider are described in U.S. Pat. No. 5,100,354, granted March 31, 1992, U.S. Pat. No. 5,249,998, granted Oct. 5, 1993, U.S. Pat. No. 6,179,676, Jan. 30, 2001, and U.S. Pat. No. 6,551,158, granted Apr. 22, 2003
- These towable water sports devices have a strut, fuselage and front and rear wings or blades which are made by casting a molten aluminum alloy. This process requires pouring molten aluminum into a sand or steel mold. The alloy used in this process is a 356A aluminum which is then heat-treated to T-6 hardness. The casting is then ground or sanded down to eliminate all entry gates, all venting gates and the receiving canals. This requires a lot of grinding, sanding and machining of the cast part after it has been taken out of the mold. Cutting and grounding a part from a rolled or pressed aluminum billet wastes material and requires a lot of machine time. Another disadvantage in manufacturing using the cast process is that the metal as it cures releases or gives off gases, resulting in the production of many small voids. This porosity in the part results in a poor finish. In addition as the casting comes out of the mold, there is shrinkage and the extent of the shrinkage is variable due to the nature of the alloy and weather conditions during the curing process. The primary disadvantage of a part cast from 356A aluminum is that it does not have the ability to flex which can result in a catastrophic failure or breakage of the part. There is a large rejection rate when casting an aluminum part due to the temperature of the mold, the outside temperature, and the amount of the metal as it is poured into the mold. The temperature of the mold has to be compatible with the heat of the material poured into the mold and this changes on a daily basis. There is a lack of overall consistency in the parts. The porosity of the cast part is present on the surface of the part. The surface porosity of the cast part adds drag to the foil assembly, which hinders the performance of the hydrofoil assembly. The porosity of the cast part also is not compatible with and does not accept the anodizing process. The anodizing is, however, desirable in that it offers a protective, maintenance free and corrosion-resistant finish.
- In a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said support, generally parallel to said board, wherein said rearward planing wing or blade has a generally flat upper face and a generally flat lower face;
-
- the improvement wherein at least said strut and fuselage are made of extruded aluminum alloy.
- The invention uses an extruded aluminum out of a AA6061 alloy heat-treated to T-6 in advance of the extrusion. The 6061 heat-treated aluminum is one of the alloys to be used, but it is not the only one suitable for use in this manufacturing process. For example, suitable aluminum alloys include the M 6000 series which are disclosed in Park U.S. Pat. No. 4,589,932, and Wade et al U.S. Patent No. 5,503,690, the disclosures of which are expressly incorporated herein by reference. This eliminates the need to take the casting from the foundry to a separate location for the heat-treating process. Extrusion does not involve the pouring of metal. The metal is billet or rolled aluminum is pushed or pulled through a pre-cut die. This gives the material a grain as opposed to a porosity as in a part made by the cast process. This grain allows the running of the grain in the long dimension of the part for added strength. This process eliminates the porosity (that offers no strength) and gives the part more strength with completely different characteristics. The extruded part can bend or flex with a memory that allows it to retain its original shape. The extruded part is less brittle which avoids breakage while under stress in use and danger to the rider. Eliminating the porosity on the exterior surface of the part gives it: a)more visibly aesthetics; 2) polishes up nicely; 3) less drag due to little or no porosity; and 4) it is compatible with the anodizing protective coating. The surface anodizing of aluminum extrusions described, for example, in Fukagawa et al U.S. Pat. No. 5,911,845.
- The advantages of extruded aluminum are applicable to the strut, fuselage, front and rear blade or wing comprising the foil assembly used in a towable hydrofoil.
- Turning to the drawings:
-
FIG. 1 is a perspective view of the water sport device of this invention with the rider seated and being towed through the water by a power boat (not shown). -
FIG. 2 shows at the left a top plan view of the fuselage and front and rear planing blades, and at the right, a side view of the strut, the parts being unassembled. -
FIG. 3 shows the strut being inserted into the opening provided in the fuselage, the fuselage and planing blades being shown in longitudinal section. -
FIG. 4 shows the strut fully in place in the fuselage and welded to the fuselage. -
FIG. 5 depicts a die through which aluminum alloy is extruded to make the parts from which the strut, fuselage and planing blades are ultimately formed. - Turning to the drawings in more detail, the water sports device of this invention has a
seat 10 for the rider 11 which is affixed to the curved board 12, thestrut 14 projects downwardly from board 12 in a generally perpendicular fashion. The lower end ofstrut 14 is received in opening 16 offuselage 18. Thefuselage 18 carries thefront planing blade 20 andrear planing blade 22. - A further feature of this invention concerns the combination of parts. In the past the castings for the foil assembly were three different parts: 1) a t-bar consisting of strut and fuselage as a single component; 2) front wing; and 3) rear wing. The new means of manufacturing includes four parts: 1) the
rear wing 22; 2)front wing 20; 3) thestrut 14; and 4) thefuselage 18. Thestrut 14 and thefuselage 18 are heliarced (a means of welding aluminum) together to form the t-bar as shown inFIG. 4 . Theextruded strut 14 fits into thefuselage slot 24 as shown in the drawings and heliarced 26 as depicted in the drawing. This process is completely new from the previous method of manufacturing in the past. The extrusion process also provides the capability of including thefront wing 20 andrear wing 22 within theextruded fuselage 18 as a single unit, thus reducing the number of parts to two. For example, thefuselage 18 andfront wing 20 andrear wing 22 can be cut to the desired shape from a single aluminum extrusion using a programmable milling machine which is available in the marketplace. This reduces assembly time since the wings do not have to be joined to the fuselage in separate operations. - The extrusions are formed by drawing hot formable aluminum through a die such as
die 28. The extrusion is then quenched and heat treated. The strut can be extruded through a die of appropriate cross section, cut to length and used as such without further working. This process conforms generally toFIG. 1 of Wakabayashi U.S. Pat. No. 5,321,967. Theslot 24 is cut into the fuselage. The fuselage, wings and strut in the desired configuration are polished smooth. The resultant surface is quite slick and well adapted to anodizing which provides an esthetically pleasing appearance which is highly resistant to corrosion. The avoidance of corrosion is an important benefit of this invention in that the strut, fuselage and blades or wings remain smooth and do not acquire or build up added drag in the water over time due to oxidation and mineral build-up. - The heliarc process is an oxygen gas mix and can be used for the welding of the extruded parts and it represents one option to be used for welding aluminum parts, but is not the only one available for this method of manufacturing. Other techniques for welding or joining pre-formed aluminum parts are known to those skilled in the art.
- The benefits of this invention include a less expensive part, stronger part, more consistent part and a part with less drag, increased performance, and fewer warranty problems. Extrusion has been used in other industries such as screen doors, window frames and others. The present invention is a completely new concept in the manufacturing of hydrofoils for water sport devices and it provides results which are not manifested in prior extruded parts.
Claims (7)
1. In a water sports device for supporting a seated human rider while said rider and device are towed behind a powered watercraft, comprising: an elongate board having a front end and a back end; a seat secured to said board for supporting the buttocks of a seated rider at a position spaced above said board; a holder spaced toward the front end of said board from said seat for securing at least one foot of said rider over the top of said board; an elongate strut perpendicular to and extending downward from said board; a fuselage having a forward end and a rearward end fixed at a point between its forward end and rearward end to said strut at a position spaced below said board; a forward planing wing or blade secured proximate the forward end of said support, generally parallel to said board, wherein said forward planing wing or blade has a generally flat upper face and a generally flat lower face; and a rear planing wing or blade secured proximate the rearward end of said support, generally parallel to said board, wherein said rearward planing wing or blade has a generally flat upper face and a generally flat lower face;
the improvement wherein at least said strut and fuselage are made of extruded aluminum alloy.
2. The water sports device of claim 1 wherein the strut, fuselage and front and rear planing wings are made of extruded aluminum.
3. The water sports device of claim 2 wherein the strut, fuselage and front rear planing wings are provided with an anodized surface.
4. The water sports device of claim 1 wherein the strut has a lower end which is received in an opening in the fuselage.
5. The water sports device of claim 4 wherein the strut is heliarc welded to the fuselage.
6. The water sports device of claim 1 wherein the extruded aluminum is an M 6000 series.
7. The water sports device of claim 6 wherein the extruded aluminum is M 6061.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/897,363 US20050112964A1 (en) | 2003-11-25 | 2004-07-21 | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
| US11/186,356 US7980191B2 (en) | 2003-11-25 | 2005-07-20 | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US52465703P | 2003-11-25 | 2003-11-25 | |
| US10/897,363 US20050112964A1 (en) | 2003-11-25 | 2004-07-21 | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
Related Child Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US11/186,356 Continuation-In-Part US7980191B2 (en) | 2003-11-25 | 2005-07-20 | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US20050112964A1 true US20050112964A1 (en) | 2005-05-26 |
Family
ID=34595160
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US10/897,363 Abandoned US20050112964A1 (en) | 2003-11-25 | 2004-07-21 | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US20050112964A1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7980191B2 (en) | 2003-11-25 | 2011-07-19 | Murphy Michael J | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US261022A (en) * | 1882-07-11 | Machine for making bolts and rivets | ||
| US4027614A (en) * | 1975-04-07 | 1977-06-07 | Jones Clyde B | Sailboat construction |
| US4615291A (en) * | 1982-08-16 | 1986-10-07 | Jones Clyde B | Hydrofoil boat |
| US5100354A (en) * | 1989-02-23 | 1992-03-31 | Woolley Robert C | Water sports device |
| US5211594A (en) * | 1992-07-02 | 1993-05-18 | Barrows Michael L | Water ski hydrofoil and process |
| US5249998A (en) * | 1989-02-23 | 1993-10-05 | Woolley Robert C | Water sports device |
| US6179676B1 (en) * | 1999-03-22 | 2001-01-30 | Jon D. Wilborn | Shock tower |
| US6386932B1 (en) * | 2000-06-27 | 2002-05-14 | Michael Murphy | Inflatable boat |
| US6551158B2 (en) * | 2001-02-20 | 2003-04-22 | Michael Murphy | Adjustable angled rear wing |
-
2004
- 2004-07-21 US US10/897,363 patent/US20050112964A1/en not_active Abandoned
Patent Citations (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US261022A (en) * | 1882-07-11 | Machine for making bolts and rivets | ||
| US4027614A (en) * | 1975-04-07 | 1977-06-07 | Jones Clyde B | Sailboat construction |
| US4615291A (en) * | 1982-08-16 | 1986-10-07 | Jones Clyde B | Hydrofoil boat |
| US5100354A (en) * | 1989-02-23 | 1992-03-31 | Woolley Robert C | Water sports device |
| US5249998A (en) * | 1989-02-23 | 1993-10-05 | Woolley Robert C | Water sports device |
| US5211594A (en) * | 1992-07-02 | 1993-05-18 | Barrows Michael L | Water ski hydrofoil and process |
| US6179676B1 (en) * | 1999-03-22 | 2001-01-30 | Jon D. Wilborn | Shock tower |
| US6386932B1 (en) * | 2000-06-27 | 2002-05-14 | Michael Murphy | Inflatable boat |
| US6551158B2 (en) * | 2001-02-20 | 2003-04-22 | Michael Murphy | Adjustable angled rear wing |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7980191B2 (en) | 2003-11-25 | 2011-07-19 | Murphy Michael J | Extruded strut, fuselage and front wing assembly for towable hydrofoil |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| STCB | Information on status: application discontinuation |
Free format text: EXPRESSLY ABANDONED -- DURING EXAMINATION |