Fiber composite material empennage base bonding tool

Abstract

The utility model discloses a fiber composite material empennage base bonding tool which comprises a base, and a plurality of profiling blocks are distributed on the base at intervals and used for loading empennage workpieces. Two sets of lifting mechanisms are symmetrically arranged on one side of the base, and the base workpiece is transferred to the empennage workpiece through the lifting mechanisms to be bonded. According to the fiber composite material empennage base bonding tool, the air cylinder is arranged to conduct die assembly in a pneumatic mode, the manual operation requirement is greatly reduced, single-person empennage bonding is achieved, the tool is simple in structure and convenient and fast to operate, the safety coefficient and the product bonding consistency are improved, and meanwhile the bonding efficiency is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of fiber composite material tail wing bonding design, in particular to a fiber composite material tail wing base bonding tool. Background Art

[0002] With the development of new energy vehicles, automobiles pay more and more attention to the development of lightweight. Carbon fiber composite materials are widely used in various parts of automobiles due to their light weight and high strength.

[0003] Among carbon fiber products, the rear wing is one of the most popular automotive parts and is mass-produced. In this process, the rear wing body and base must be formed first, and then the two are connected together with structural adhesive. Currently, most of them are bonded manually by closing the upper and lower molds. The bonding operation cannot be completed by one person, and the bonding efficiency is low and the operation is inconvenient. Utility Model Content

[0004] The utility model aims to provide a fiber composite material tail wing base bonding tool, aiming to solve the problems of low manual bonding efficiency and inconvenient operation.

[0005] In order to solve the above technical problems, the utility model provides a fiber composite material tail wing base bonding tool, comprising a base,

[0006] A plurality of contour blocks are arranged at intervals on the base for loading the tail wing parts;

[0007] Two sets of lifting mechanisms are symmetrically arranged on one side of the base, and the base component is transferred to the tail wing component for bonding through the lifting mechanisms.

[0008] Preferably, the lifting mechanism comprises a cylinder, a lifting guide rail and an adsorption seat, and the adsorption seat with the base component placed thereon moves downward along the lifting guide rail under the action of the cylinder piston rod, so that the base component fits in contact with the bonding position on the tail component.

[0009] Preferably, a contoured groove is provided in the adsorption seat for placing the base component; and a plurality of negative pressure suction cups are provided in the contoured groove for adsorbing and fixing the base component.

[0010] Preferably, there are four profiling blocks, namely a first profiling block, a second profiling block, a third profiling block and a fourth profiling block; the first profiling block and the fourth profiling block are respectively used to support the two ends of the tail wing component, while the second profiling block and the third profiling block are respectively located directly below the two sets of lifting mechanisms to provide support for the bonding of the base component.

[0011] Preferably, two buffer rubber columns are provided on the base, and the two buffer rubber columns correspond to two sets of lifting mechanisms respectively, so as to provide buffering for the descent of the adsorption seat.

[0012] Preferably, two limit blocks are provided on the base, and the two limit blocks correspond to two sets of lifting mechanisms respectively, providing limit for the descent of the adsorption seat.

[0013] Preferably, three pneumatic switches are also provided on the base, two of which respectively control the negative pressure suction cups in the adsorption seat, and the third pneumatic switch is used to control the synchronous lifting and lowering of the two sets of lifting mechanisms.

[0014] Compared with the prior art, the beneficial effects of the utility model are:

[0015] The fiber composite material tail wing base bonding tool adopts pneumatic mold closing by setting up a cylinder, which greatly reduces the manual operation requirements and realizes single-person tail wing bonding. The tool has a simple structure and is easy to operate, which not only improves the safety factor and product bonding consistency, but also improves the bonding efficiency. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a structural schematic diagram of a fiber composite material tail wing base bonding tool provided by the utility model;

[0017] Figure 2 It is a structural schematic diagram of the bonding tool provided by the utility model bonding the fiber composite material tail wing base;

[0018] Figure 3 It is a structural schematic diagram of the adsorption seat provided by the utility model.

[0019] In the figure: 1, base; 2, cylinder; 3, lifting guide rail; 4, adsorption seat; 401, profiling groove; 5, first profiling block; 6, second profiling block; 7, third profiling block; 8, fourth profiling block; 9, buffer rubber column; 10, limit block; 11, pneumatic switch; 100, tail wing component; 200, base component. DETAILED DESCRIPTION

[0020] The following is a further detailed description of the present invention in conjunction with the accompanying drawings and specific embodiments. The advantages and features of the present invention will become more apparent from the following description and claims. It should be noted that the drawings are in very simplified form and in non-precise proportions, and are only used to conveniently and clearly assist in explaining the purpose of the embodiments of the present invention.

[0021] In the description of the present utility model, it should be understood that the terms "center", "longitudinal", "lateral", "up", "down", "front", "back", "left", "right", "vertical", "horizontal", "top", "bottom", "inside", "outside" and the like indicate positions or positional relationships based on the positions or positional relationships shown in the accompanying drawings, and are only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be understood as a limitation on the present utility model. In addition, the terms "first", "second", etc. are only used for descriptive purposes, and cannot be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Therefore, features defined as "first", "second", etc. may explicitly or implicitly include one or more of the features. In the description of the present utility model, unless otherwise specified, "multiple" means two or more.

[0022] In the description of the present invention, it should be noted that, unless otherwise clearly specified and limited, the terms "installation", "connection" and "connection" should be understood in a broad sense, for example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be a direct connection, or it can be an indirect connection through an intermediate medium, or it can be the internal communication of two components. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood by specific circumstances. Example

[0023] The utility model provides a fiber composite material tail wing base bonding tool, please refer to Figure 1 and Figure 2 , including a base 1, on which a plurality of contour blocks are arranged at intervals for loading a tail wing component 100; two sets of lifting mechanisms are symmetrically arranged on one side of the base 1, through which the base component 200 is transferred to the tail wing component 100 for bonding.

[0024] Specifically, the lifting mechanism includes a cylinder 2, a lifting guide rail 3 and an adsorption seat 4. The adsorption seat 4 with the base component 200 placed thereon moves downward along the lifting guide rail 3 under the action of the piston rod of the cylinder 2, so that the base component 200 is in contact with the bonding position on the tail component 100.

[0025] And, if Figure 3 As shown, a contoured groove 401 is provided in the adsorption seat 4 for placing the base component 200 ; and a plurality of negative pressure suction cups are provided in the contoured groove 401 for adsorbing and fixing the base component 200 .

[0026] Specifically, there are four profiling blocks, namely a first profiling block 5, a second profiling block 6, a third profiling block 7 and a fourth profiling block 8; the first profiling block 5 and the fourth profiling block 8 are respectively used to support the two ends of the tail wing component 100, while the second profiling block 6 and the third profiling block 7 are respectively located directly below the two sets of lifting mechanisms to provide support for the bonding of the base component 200.

[0027] In some embodiments, two buffer rubber columns 9 are provided on the base 1 , and the two buffer rubber columns 9 correspond to two sets of lifting mechanisms respectively, so as to provide buffering for the descent of the adsorption seat 4 .

[0028] In some embodiments, two limit blocks 10 are provided on the base 1 , and the two limit blocks 10 correspond to two sets of lifting mechanisms respectively, providing limit for the descent of the adsorption seat 4 .

[0029] Furthermore, three pneumatic switches 11 are provided on the base 1, wherein two pneumatic switches 11 respectively control the negative pressure suction cups in the adsorption seat 4, and the third pneumatic switch 11 is used to control the synchronous lifting of the two lifting mechanisms.

[0030] The specific working method is as follows: the tail wing component 100 is placed on the contour fixing block of the base 1, so that the tail wing component 100 fits with the inner surfaces of the first contour block 5, the second contour block 6, the third contour block 7 and the fourth contour block 8; then the pneumatic switch 11 of the negative pressure suction cup in the two adsorption seats 4 is turned on, and the base component 200 is adsorbed in the contour groove 401, and the contour groove 401 fits with the base component 200 around; finally, after applying glue to the bonding position of the tail wing component 100, the pneumatic switch 11 is operated to make the two adsorption seats 4 descend along the lifting guide rail 3 to the position of the limit block 10, and the bonding of the base component 200 and the tail wing component 100 is completed.

[0031] The above description is only a description of the preferred embodiment of the utility model, and is not any limitation on the scope of the utility model. Any changes and modifications made by ordinary technicians in the field of the utility model based on the above disclosure shall fall within the scope of protection of the claims.

Claims

1. A fiber composite material tail wing base bonding tool, characterized in that: Including base (1), A plurality of contour blocks are arranged at intervals on the base (1) for loading the tail wing component (100); Two sets of lifting mechanisms are symmetrically arranged on one side of the base (1), and the base component (200) is transferred to the tail wing component (100) for bonding via the lifting mechanisms.

2. A fiber composite material tail wing base bonding tool as claimed in claim 1, characterized in that: The lifting mechanism comprises a cylinder (2), a lifting guide rail (3) and an adsorption seat (4); the adsorption seat (4) on which the base component (200) is placed moves downward along the lifting guide rail (3) under the action of the piston rod of the cylinder (2), so that the base component (200) fits in contact with the bonding position on the tail component (100).

3. A fiber composite material tail wing base bonding tool as claimed in claim 2, characterized in that: The adsorption seat (4) is provided with a contoured groove (401) for placing the base component (200); and a plurality of negative pressure suction cups are provided in the contoured groove (401) for adsorbing and fixing the base component (200).

4. A fiber composite material tail wing base bonding tool as claimed in claim 1, characterized in that: There are four profiling blocks, namely a first profiling block (5), a second profiling block (6), a third profiling block (7) and a fourth profiling block (8); the first profiling block (5) and the fourth profiling block (8) are respectively used to support the two ends of the tail wing component (100), while the second profiling block (6) and the third profiling block (7) are respectively located directly below the two sets of lifting mechanisms to provide support for the bonding of the base component (200).

5. The fiber composite material tail wing base bonding tool as claimed in claim 2, characterized in that: Two buffer rubber columns (9) are provided on the base (1), and the two buffer rubber columns (9) correspond to two sets of lifting mechanisms respectively, so as to provide buffering for the descent of the adsorption seat (4).

6. A fiber composite material tail wing base bonding tool as claimed in claim 2, characterized in that: Two limit blocks (10) are provided on the base (1), and the two limit blocks (10) correspond to two sets of lifting mechanisms respectively, providing limit for the descent of the adsorption seat (4).

7. A fiber composite material tail wing base bonding tool as claimed in claim 2, characterized in that: The base (1) is also provided with three pneumatic switches (11), two of which are used to control the negative pressure suction cups in the adsorption seat (4), respectively, and the third pneumatic switch (11) is used to control the synchronous lifting of the two lifting mechanisms.

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