CN211844829U - Split hydrofoil - Google Patents
Split hydrofoil Download PDFInfo
- Publication number
- CN211844829U CN211844829U CN202020105892.2U CN202020105892U CN211844829U CN 211844829 U CN211844829 U CN 211844829U CN 202020105892 U CN202020105892 U CN 202020105892U CN 211844829 U CN211844829 U CN 211844829U
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- wing plate
- sliding rod
- screw hole
- split
- inner groove
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Abstract
The utility model discloses a split hydrofoil, which comprises a structure main body, wherein the structure main body comprises a support rod, a fixed external member is arranged on the support rod, a sliding rod is arranged in the fixed external member in an alternate mode, a front wing plate is arranged at the front end of the sliding rod, a rear wing plate is arranged at the rear end of the sliding rod, two sides of the front wing plate bend to one side away from the support rod and are in an arc shape, and two sides of the rear wing plate bend to one side close to the support rod and are in an arc shape; the utility model is a split structure, can be disassembled and assembled to replace accessories of different types, is used for meeting different requirements of different clients in different periods, and is convenient to operate in an embedded disassembly and assembly mode; the utility model is made of all carbon fiber material, has light weight and high ascending speed, and is firm and durable.
Description
Technical Field
The utility model relates to a water sports product technical field, concretely relates to components of a whole that can function independently hydrofoil.
Background
The traditional water surfboard mainly depends on sea waves to realize surfing, and if the sea surface is calm, the surfing can not be carried out.
The prior water surfboard has the hydrofoil to assist the surfboard to advance so as to realize surfing on the sealess sea, but the prior hydrofoil on the market has the advantages of fixed structure, small use flexibility, heavier weight, slow rising speed and poor use experience.
SUMMERY OF THE UTILITY MODEL
The utility model aims at providing a components of a whole that can function independently hydrofoil in order to solve above-mentioned problem.
The utility model discloses a following technical scheme realizes above-mentioned purpose, a components of a whole that can function independently hydrofoil, including a main structure body, main structure body includes the bracing piece, be equipped with fixed external member on the bracing piece, alternate formula is equipped with the slide bar in the fixed external member, the slide bar front end is equipped with preceding pterygoid lamina, the slide bar rear end is equipped with the back pterygoid lamina, preceding pterygoid lamina both sides side direction is kept away from bracing piece one side bending and is the arc form, back pterygoid lamina both sides direction is close to bracing piece one side bending and is the arc form.
Preferably, a first inner groove is formed in the connecting end of the front wing plate and the sliding rod, the first inner groove is of a conical polygonal structure, and the connecting end of the sliding rod and the front wing plate is inserted into the first inner groove.
Preferably, a first screw hole is formed in the first inner groove, a second screw hole is formed in the connecting end of the sliding rod and the front wing plate, the first screw hole corresponds to the second screw hole, and the sliding rod is fixedly connected with the front wing plate through screws.
Preferably, a third screw hole is formed in the fixing sleeve, a fourth screw hole is formed in the joint of the sliding rod and the fixing sleeve, the third screw hole corresponds to the fourth screw hole, and the sliding rod is fixedly connected with the fixing sleeve through a screw.
Preferably, a second inner groove is formed in the connecting end of the rear wing plate and the sliding rod, the second inner groove is of a conical structure, and the connecting end of the sliding rod and the rear wing plate is inserted into the second inner groove.
Preferably, a fifth screw hole is formed in the second inner groove, a sixth screw hole is formed in the connecting end of the sliding rod and the front wing plate, the fifth screw hole corresponds to the sixth screw hole, and the sliding rod is fixedly connected with the rear wing plate through screws.
Preferably, a gasket is arranged at the joint of the sliding rod and the rear wing plate, the gasket is connected with the sliding rod in a clamping mode and fixed on the sliding rod through screws, and the gasket is made of TTF titanium alloy materials.
Preferably, one end of the fixing sleeve, which is close to the front wing plate, is of a polygonal structure, and one end of the fixing sleeve, which is close to the rear wing plate, is of a circular structure.
Preferably, the connecting end of the sliding rod and the front wing plate is in a tapered polygonal structure, and the connecting end of the sliding rod and the rear wing plate is in a tapered structure.
The utility model has the advantages that: the utility model is a split structure, can be disassembled and assembled to replace accessories of different types, is used for meeting different requirements of different clients in different periods, and is convenient to operate in an embedded disassembly and assembly mode; the utility model is made of all carbon fiber material, has light weight, high rising speed and firmness and durability; the gasket is of a detachable structure, different types of gaskets are replaced according to use requirements, the tilting angle of the rear wing plate can be adjusted, and the gasket is a titanium alloy gasket, so that the gasket has the advantages of corrosion resistance, light weight and good hardness; through setting up slide bar and pterygoid lamina and fixed external member link to toper polygon structure, connect fixedly through polygon grafting structure, control equipment equilibrium degree and precision that can be better have guaranteed the performance of product, make its performance exert to the utmost point.
Drawings
FIG. 1 is a schematic view of the overall structure of the present invention;
FIG. 2 is a schematic view of another structure of the present invention;
FIG. 3 is an exploded view of the present invention;
FIG. 4 is a schematic view of the structure of the slide bar of the present invention;
FIG. 5 is a schematic view of the fixing kit according to the present invention;
FIG. 6 is a schematic view of the gasket structure of the present invention;
in the figure: 1. a front wing panel; 2. a fixation kit; 3. a slide bar; 4. a rear wing panel; 5. a support bar; 6. a first screw hole; 7. a first inner groove; 8. a third screw hole; 9. a second screw hole; 10. a fourth screw hole; 11. a sixth screw hole; 12. a second inner groove; 13. a fifth screw hole; 14. a gasket; 15. close to one end of the rear wing plate; 16. near one end of the front wing plate.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
As shown in fig. 1-3, a split hydrofoil comprises a structural body, the structural body comprises a support rod 5, a fixing sleeve 2 is arranged on the support rod 5, a sliding rod 3 is arranged in the fixing sleeve 2 in an interpenetration manner, a front wing plate 1 is arranged at the front end of the sliding rod 3, a rear wing plate 4 is arranged at the rear end of the sliding rod 3, two sides of the front wing plate 1 are bent towards one side far away from the support rod 5 to form an arc shape, and two sides of the rear wing plate 4 are bent towards one side close to the support rod 5 to form an arc shape.
A first inner groove 7 is formed in the connecting end of the front wing plate 1 and the sliding rod 3, the first inner groove 7 is of a conical polygonal structure, and the connecting end of the sliding rod 3 and the front wing plate 1 is inserted into the first inner groove 7; a first screw hole 6 is formed in the first inner groove 7, a second screw hole 9 is formed in the connecting end of the sliding rod 3 and the front wing plate 1, the first screw hole 6 corresponds to the second screw hole 9, and the sliding rod 3 is fixedly connected with the front wing plate 1 through screws; a third screw hole 8 is formed in the fixing sleeve 2, a fourth screw hole 10 is formed in the joint of the sliding rod 3 and the fixing sleeve 2, the third screw hole 8 corresponds to the fourth screw hole 10, and the sliding rod 3 is fixedly connected with the fixing sleeve 2 through screws; a second inner groove 12 is formed in the connecting end of the rear wing plate 4 and the sliding rod 3, the second inner groove 12 is of a conical structure, and the connecting end of the sliding rod 3 and the rear wing plate 4 is inserted into the second inner groove 12; a fifth screw hole 13 is formed in the second inner groove 12, a sixth screw hole 11 is formed in the connecting end of the sliding rod 3 and the front wing plate 1, the fifth screw hole 13 corresponds to the sixth screw hole 11, and the sliding rod 3 is fixedly connected with the rear wing plate 4 through screws; the connecting end of the sliding rod 3 and the front wing plate 1 is of a conical polygonal structure, and the connecting end of the sliding rod 3 and the rear wing plate 4 is of a conical structure.
It should be noted that the structural body is made of an all-carbon fiber material.
The shape of the connection end of the slide rod 3 and the front wing plate 1 is the same as the shape of the first inner groove 7, and the shape of the connection end of the slide rod 3 and the rear wing plate 4 is the same as the shape of the second inner groove 12.
It should be noted that, one end of the sliding rod 3 connected to the front wing plate 1 is a tapered polygonal structure, and one of the tapered polygonal structures is a tapered hexagon.
As shown in fig. 4, the slide rod 3 is composed of a first section and a second section, the first section is connected to the front wing plate 1, the second section is connected to the rear wing plate 4, a connecting end of the first section and the second section is a polygonal structure, a connecting end of the second section and the first section is a cylindrical structure, and the fixing sleeve 2 is sleeved at a connecting position of the first section and the second section.
As shown in fig. 5, one end 16 of the fixing sleeve 2 close to the front wing plate is of a polygonal structure, and one end 15 of the fixing sleeve 2 close to the rear wing plate is of a circular structure.
As shown in fig. 6, a gasket 14 is arranged at the joint of the sliding rod 3 and the rear wing plate 4, the gasket 14 is connected with the sliding rod 3 in a clamping manner and fixed on the sliding rod 3 through screws, and the gasket 14 is made of a TTF titanium alloy material.
The utility model relates to a split type hydrofoil adopts split type connection structure, can the dismouting change the accessory of different models, is used for reaching the different demands of different customers different periods, and embedded dismouting mode is convenient for operate simultaneously, and the adjustable angle that is different of gasket 14 can realize different functions, lets the speed of sliding faster, and is balanced better, and bracing piece 5 can just trade the bracing piece of different length for different surfing scenes.
The utility model discloses according to the dynamic design that the fluid rises, the imitative aircraft principle of taking off adopts streamlined design to reduce the resistance, has improved the speed of sliding.
It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.
Furthermore, it should be understood that although the present description refers to embodiments, not every embodiment may contain only a single embodiment, and such description is for clarity only, and those skilled in the art should integrate the description, and the embodiments may be combined as appropriate to form other embodiments understood by those skilled in the art.
Claims (9)
1. The utility model provides a components of a whole that can function independently hydrofoil, its characterized in that, includes a structure main part, structure main part includes bracing piece (5), be equipped with fixed external member (2) on bracing piece (5), alternate formula is equipped with in fixed external member (2) and slides pole (3), it is equipped with preceding pterygoid lamina (1) to slide pole (3) front end, it is equipped with back pterygoid lamina (4) to slide pole (3) rear end, preceding pterygoid lamina (1) both sides are the arc form to keeping away from bracing piece (5) one side bending, back pterygoid lamina (4) both sides are the arc form to being close to bracing piece (5) one side bending.
2. The split hydrofoil according to claim 1, wherein: the front wing plate (1) and the sliding rod (3) are connected through a first inner groove (7), the first inner groove (7) is of a conical polygonal structure, and the sliding rod (3) and the front wing plate (1) are connected through a connecting end in the first inner groove (7) in an inserting mode.
3. The split hydrofoil according to claim 2, wherein: be equipped with first screw (6) on first inner grove (7), slide pole (3) with preceding pterygoid lamina (1) link is equipped with second screw (9), first screw (6) with second screw (9) correspond, slide pole (3) with preceding pterygoid lamina (1) pass through screw fixed connection.
4. The split hydrofoil according to claim 1, wherein: the sliding rod is characterized in that a third screw hole (8) is formed in the fixed sleeve (2), a fourth screw hole (10) is formed in the joint of the sliding rod (3) and the fixed sleeve (2), the third screw hole (8) corresponds to the fourth screw hole (10), and the sliding rod (3) is fixedly connected with the fixed sleeve (2) through a screw.
5. The split hydrofoil according to claim 1, wherein: the rear wing plate (4) and the connecting end of the sliding rod (3) are provided with a second inner groove (12), the second inner groove (12) is of a conical structure, and the connecting end of the sliding rod (3) and the rear wing plate (4) is inserted into the second inner groove (12).
6. The split hydrofoil according to claim 5, wherein: the novel sliding wing plate is characterized in that a fifth screw hole (13) is formed in the second inner groove (12), a sixth screw hole (11) is formed in the connecting end of the sliding rod (3) and the front wing plate (1), the fifth screw hole (13) corresponds to the sixth screw hole (11), and the sliding rod (3) is fixedly connected with the rear wing plate (4) through screws.
7. The split hydrofoil according to claim 1, wherein: slide pole (3) with back pterygoid lamina (4) junction is equipped with gasket (14), gasket (14) with slide pole (3) joint formula is connected to through the screw fixation in slide pole (3) are last, gasket (14) are made by TTF titanium alloy material.
8. The split hydrofoil according to claim 1, wherein: one end (16) of the fixed sleeve (2) close to the front wing plate is of a polygonal structure, and one end (15) of the fixed sleeve (2) close to the rear wing plate is of a circular structure.
9. The split hydrofoil according to claim 1, wherein: the connecting end of the sliding rod (3) and the front wing plate (1) is of a conical polygonal structure, and the connecting end of the sliding rod (3) and the rear wing plate (4) is of a conical structure.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202020105892.2U CN211844829U (en) | 2020-01-17 | 2020-01-17 | Split hydrofoil |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202020105892.2U CN211844829U (en) | 2020-01-17 | 2020-01-17 | Split hydrofoil |
Publications (1)
Publication Number | Publication Date |
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CN211844829U true CN211844829U (en) | 2020-11-03 |
Family
ID=73232168
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
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CN202020105892.2U Active CN211844829U (en) | 2020-01-17 | 2020-01-17 | Split hydrofoil |
Country Status (1)
Country | Link |
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CN (1) | CN211844829U (en) |
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2020
- 2020-01-17 CN CN202020105892.2U patent/CN211844829U/en active Active
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