CN108298038B

CN108298038B - Carbon fiber balance wing structure

Info

Publication number: CN108298038B
Application number: CN201711447699.6A
Authority: CN
Inventors: 陆振辉
Original assignee: Suli Composite Material Technology Huizhou Co ltd
Current assignee: Suli Composite Materials Hubei Co ltd
Priority date: 2017-12-27
Filing date: 2017-12-27
Publication date: 2020-07-14
Anticipated expiration: 2037-12-27
Also published as: CN108298038A

Abstract

The invention discloses a carbon fiber balance wing structure. The ABS rubber ring comprises a core body, an ABS rubber ring, a carbon fiber rod, a protection block, a clamping groove, a protrusion, a centering groove, a first fixing block, a second fixing block, a fixing hole and a fixing pin. The method has the following beneficial effects: this balanced wing structure, regard as the core with the epoxy foaming, the outside sets up carbon fiber pole through hot briquetting, and changed the product when the mould design outer along forming omega form, crashproof ABS rubber circle is inlayed again to final finished product, set up the protection piece in fashioned core both sides and strengthen the protection, make this product have light weight high strength and crashworthiness performance, center department through at the core sets up the arch, set up the centering groove in the arch, balanced wing structure centering connection can be convenient for, guarantee the centering nature of the connection of this structure, the balance of both sides, the stationarity of increase device, set up symmetrical first fixed block and second fixed block in the both sides of core, be used for balanced wing and device be connected.

Description

Carbon fiber balance wing structure

Technical Field

The invention relates to the technical field of surfing appliances, in particular to a carbon fiber balance wing structure.

Background

Surfing is extreme motion taking sea waves as power, a surfer can take a prone posture or sit on a surfboard to wait in a place where sea waves are suitable, when the suitable sea waves are close to each other gradually, the surfer adjusts the direction of the board head, the surfer can take the prone posture to water on the surfboard along the direction of the sea waves, the surfboard is kept in front of the sea waves at a sufficient speed, when the sea waves push the surfboard to slide, the surfer stands up, the two legs stand forwards and backwards naturally, the two knees bend slightly, and the body gravity, the shoulders and the back legs are used for controlling the trend of the surfboard. Surfing can lead people to forget trouble, and experience the pleasure of fighting with sea waves and galloping on the sea waves for one time. This is why many people find the most perfect surfing place around the world every day, just to complete one perfect pursuit with the waves. In the surfing process, the stability in the surfing process needs to be improved by using a balance wing structure, the controllability of the surfing tool is improved, and the operation is more convenient.

However, the existing balance wing structure still has certain defects when in use, and the existing traditional balance wing is formed by carbon fiber/glass fiber pre-impregnated cloth in a stacking and hot-pressing mode, and has the defects of heavy volume, thin edge and easy damage.

Disclosure of Invention

The invention aims to solve the problems of heavy volume, thin edge and easy collision and damage in the prior art, and provides a carbon fiber balance wing structure.

In order to achieve the purpose, the invention adopts the following technical scheme:

carbon fiber balance wing structure, including core, ABS rubber circle and carbon fiber pole, the ABS rubber circle is connected to the periphery of core, the ABS rubber circles and sets up the joint groove, the ABS rubber circles and sets up the protection piece, the core is connected with the carbon fiber pole, the top of core is equipped with the arch, protruding middle part position sets up the middle groove, set up first fixed block and second fixed block on the core, all set up the fixed orifices on first fixed block and the second fixed block, first fixed block and second fixed block and fixed pin connection.

Preferably, the core body is arc-shaped, and two ends of the core body are arc-shaped.

Preferably, the periphery of the core body is provided with a groove clamped with the carbon fiber rod, and the carbon fiber rod is fixedly connected with the core body.

Preferably, symmetrical protective blocks are arranged at the joints of the ABS rubber ring and the two ends of the core body.

Preferably, a groove matched with the carbon fiber rod is arranged in the ABS rubber ring.

Preferably, the first fixing block and the second fixing block are arranged correspondingly, and the fixing pin is movably connected with the first fixing block and the second fixing block.

Compared with the prior art, the invention provides the carbon fiber balance wing structure, which has the following beneficial effects:

1. this balance wing structure is with epoxy foaming as the core, and the outside sets up carbon fiber pole through hot briquetting to having changed the outer omega form of edge formation of product when the mould design, final finished product is inlayed crashproof ABS rubber circle again, sets up the protection piece in fashioned core both sides and strengthens the protection, makes this product have light weight high strength and crashproof performance.

2. This balanced wing structure sets up the arch through the center department at the core, sets up the centering groove in the arch, can be convenient for balanced wing structure centering connection, guarantees the centering nature of the connection of this structure, and the balance of both sides increases the stationarity of device, sets up symmetrical first fixed block and second fixed block in the both sides of core for balanced wing is connected with the device, connects firmly.

The parts which are not involved in the device are the same as or can be realized by adopting the prior art, and the device has the advantages of simple structure and convenient operation.

Drawings

FIG. 1 is a schematic structural diagram of a carbon fiber balance wing structure according to the present invention;

fig. 2 is a schematic top view of a carbon fiber balance wing structure according to the present invention.

Fig. 3 is a schematic structural view of an ABS rubber ring of a carbon fiber balanced wing structure according to the present invention.

Fig. 4 is an enlarged detail view of a region a in the structure diagram 1 of the carbon fiber balance wing according to the present invention.

Fig. 5 is an enlarged detail view of the area B in the structure diagram 1 of the carbon fiber balance wing according to the present invention.

In the figure: 1. a core body; 2. an ABS rubber ring; 3. a carbon fiber rod; 4. a protection block; 5. a clamping groove; 6. a protrusion; 7. centering the groove; 8. a first fixed block; 9. a second fixed block; 10. a fixing hole; 11. and fixing the pin.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments.

In the description of the present invention, it is to be understood that the terms "upper", "lower", "front", "rear", "left", "right", "top", "bottom", "inner", "outer", and the like, indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, are merely for convenience in describing the present invention and simplifying the description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention.

Example 1

Referring to fig. 1-5, a carbon fiber balance wing structure comprises a core body 1, an ABS rubber ring 2 and a carbon fiber rod 3, wherein the periphery of the core body 1 is connected with the ABS rubber ring 2, the ABS rubber ring 2 provides all-directional protection for the core body 1, soft contact is performed during collision of the core body 1 to avoid collision damage of the core body 1, the ABS rubber ring 2 is provided with a clamping groove 5, the clamping groove 5 is matched with the carbon fiber rod 3, the ABS rubber ring 2 and the carbon fiber rod 3 are clamped with each other, the ABS rubber ring 2 is provided with a protection block 4, the protection blocks 4 are arranged at two ends of the core body 1, the collision probability at two ends of the core body 1 is maximum, the two ends of the core body 1 are mainly protected, a protrusion 6 is arranged above the core body 1, a centering groove 7 is arranged at the middle position of the protrusion 6, the protrusion 6 is arranged at the center position of the core body 1, the centering groove 7 is convenient for centering connection of a balance wing to balance the, first fixed block 8 and second fixed block 9 are the symmetry setting on core 1, all set up fixed orifices 10 on first fixed block 8 and the second fixed block 9, and the fixed orifices is used for the connection of fixed pin, and first fixed block 8 and second fixed block 9 are connected with fixed pin 11, and fixed pin 11 is swing joint, the balanced wing's of being convenient for dismantlement installation.

Example 2

In addition, please refer to fig. 1-5, which are different from embodiment 1 in that: the core body 1 is arc-shaped, two ends of the core body 1 are arc-shaped, the core body 1 is more in line with dynamic streamline, resistance in the sliding process is reduced, grooves clamped with the carbon fiber rods 3 are formed in the periphery of the core body 1, the carbon fiber rods 3 are fixedly connected with the core body 1, the carbon fiber rods 3 can increase toughness and strength of the core body 1, meanwhile, the weight of the device is reduced, symmetrical protective blocks 4 are arranged at the joints of the ABS rubber ring 2 and the two ends of the core body 1, the protective blocks 4 are arranged at the two ends with the maximum collision probability of the core body 1 to increase protection and avoid collision damage, grooves matched with the carbon fiber rods 3 are formed in the ABS rubber ring 2 to facilitate clamping of the ABS rubber ring 2 and facilitate connection and installation, the first fixed block 8 and the second fixed block 9 are correspondingly arranged, the fixed pin 11 is movably connected with the first fixed block 8 and the second fixed block 9 to facilitate installation and connection, the first fixed block 8 and the second fixed block 9 that core 1 both sides symmetry set up increase joint strength, make to connect more firm.

During the use, connect assorted carbon fiber pole 3 with it around core 1, carbon fiber pole 3 can increase the toughness and the intensity of balanced wing, ABS rubber circle 2 provides the protection for balanced wing, avoid damaging in the collision, set up centering groove 7 in the centre of core 1, the centering installation of the device of being convenient for, set up symmetrical first fixed block 8 and second fixed block 9 on core 1, can let the device connect firmly, the fixed pin 11 of activity is convenient for the erection joint of device simultaneously, balanced wing excellent in use effect.

In this document, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising an … …" does not exclude the presence of other identical elements in a process, method, article, or apparatus that comprises the element.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

The above description is only for the preferred embodiment of the present invention, but the scope of the present invention is not limited thereto, and any person skilled in the art should be considered to be within the technical scope of the present invention, and the technical solutions and the inventive concepts thereof according to the present invention should be equivalent or changed within the scope of the present invention.

Claims

1. Carbon fiber balance wing structure, including core (1), ABS rubber circle (2) and carbon fiber pole (3), its characterized in that, ABS rubber circle (2) is connected to the periphery of core (1), set up joint groove (5) on ABS rubber circle (2), joint groove (5) and carbon fiber pole (3) phase-match, set up protection piece (4) on ABS rubber circle (2), core (1) is connected with carbon fiber pole (3), the top of core (1) is equipped with arch (6), arch (6) middle part position sets up middle groove (7), set up first fixed block (8) and second fixed block (9) on core (1), all set up fixed orifices (10) on first fixed block (8) and second fixed block (9), first fixed block (8) and second fixed block (9) are connected with fixed pin (11), the core (1) is arc-shaped, the two ends of the core (1) are arc-shaped, the periphery of the core (1) is provided with a groove connected with the carbon fiber rod (3) in a clamped mode, and the carbon fiber rod (3) is fixedly connected with the core (1).

2. The carbon fiber balance wing structure according to claim 1, characterized in that symmetrical protective blocks (4) are arranged at the joints of the ABS rubber ring (2) and the two ends of the core body (1).

3. The carbon fiber balance wing structure according to claim 1, wherein the first fixing block (8) and the second fixing block (9) are correspondingly arranged, and the fixing pin (11) is movably connected with the first fixing block (8) and the second fixing block (9).