CN220406038U - A integral type support for fin application - Google Patents
A integral type support for fin application Download PDFInfo
- Publication number
- CN220406038U CN220406038U CN202321898231.XU CN202321898231U CN220406038U CN 220406038 U CN220406038 U CN 220406038U CN 202321898231 U CN202321898231 U CN 202321898231U CN 220406038 U CN220406038 U CN 220406038U
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- mounting plate
- wing
- wing body
- body mounting
- bracket
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- 238000000576 coating method Methods 0.000 claims abstract description 11
- 239000011248 coating agent Substances 0.000 claims abstract description 10
- 238000010422 painting Methods 0.000 claims description 9
- 230000003014 reinforcing effect Effects 0.000 claims description 9
- 239000000565 sealant Substances 0.000 abstract description 3
- 229910000975 Carbon steel Inorganic materials 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 3
- 239000010962 carbon steel Substances 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 238000005507 spraying Methods 0.000 description 3
- 230000008901 benefit Effects 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000001962 electrophoresis Methods 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 239000003973 paint Substances 0.000 description 2
- 238000006467 substitution reaction Methods 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 1
- 238000005034 decoration Methods 0.000 description 1
- 239000003292 glue Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 239000013585 weight reducing agent Substances 0.000 description 1
Landscapes
- Body Structure For Vehicles (AREA)
Abstract
The utility model relates to the field of automobile coating technology, and discloses an integrated bracket for tail coating, which comprises the following components: the novel wing structure comprises a cross beam, a first upright post and a second upright post, wherein a first bracket hole and a second bracket hole are respectively formed in the left side and the right side of the cross beam, the first bracket hole and the second bracket hole extend vertically, a first wing body mounting plate is arranged on the first upright post, a first wing body hole is formed in the first wing body mounting plate, a second wing body mounting plate is arranged on the second upright post, and a second wing body hole is formed in the second wing body mounting plate. This an integral type support for fin application is convenient for squeeze into the sealant when fixed fin, and is firm to the support of wing body, and it is convenient to install the wing body.
Description
Technical Field
The utility model relates to the field of automobile coating processes, in particular to an integrated bracket for tail fin coating.
Background
In order to improve the stability of the vehicle during high-speed running and meet the special vehicle requirements of market clients, an electric tail wing is added to part of vehicle types in the market at present, and the electric tail wing is mounted on a trunk cover in a whole vehicle state. When the vehicle runs at a high speed, the angle of the tail wing is automatically adjusted through the electric device, and additional downward pressure is provided for the vehicle, so that the ground grabbing force of the rear wheel is improved, and the running stability is improved.
In order to ensure that the tail fin has enough strength and comprehensively consider the whole car cost, one of the alternatives of the electric tail fin material is carbon steel. The electric tail fin made of carbon steel needs to be pretreated.
Firstly, electrophoresis is needed to meet the anti-corrosion requirement of the whole vehicle; secondly, in order to prevent water from penetrating into the inner cavity at the buckling edge of the electric tail wing when the electric tail wing works in a whole vehicle state, the buckling edge of the electric tail wing needs to be sealed by extruding glue; thirdly, in order to improve the appearance of the electric tail wing in the whole car state, paint (with the same color as that of the car body) needs to be sprayed on the inner surface and the outer surface of the electric tail wing for decoration; fourth, in order to ensure the gap section difference between the electric tail wing and the trunk lid, the deformation amount generated by the electric tail wing in the painting manufacturing link should be small.
Based on the above, to the motorcycle type of using the electronic fin of carbon steel material, need design a reliable, easy loading and unloading's support, this support is in the application process, effectively satisfies pretreatment, electrophoresis, crowded seal gum, the normal operation of spraying paint link, and the deflection is little.
Disclosure of Invention
The present utility model aims to solve at least one of the technical problems existing in the background art.
The utility model provides an integrated bracket for tail wing coating, which comprises the following components: the novel wing structure comprises a cross beam, a first upright post and a second upright post, wherein a first bracket hole and a second bracket hole are respectively formed in the left side and the right side of the cross beam, the first bracket hole and the second bracket hole extend vertically, a first wing body mounting plate is arranged on the first upright post, a first wing body hole is formed in the first wing body mounting plate, a second wing body mounting plate is arranged on the second upright post, and a second wing body hole is formed in the second wing body mounting plate.
The utility model has the beneficial effects that: this an integral type support for fin application has set up crossbeam, first stand, the second stand, first wing body mounting panel and second wing body mounting panel, fix on automobile body frame through first support hole and second support hole, because first wing body mounting panel and second wing body mounting panel are set up by first stand and second stand respectively, be convenient for squeeze into the sealant when fixing the fin through first wing body mounting panel and second wing body mounting panel, in addition because first support hole and second support hole all follow vertical extension, it is comparatively convenient when fixing on the automobile body through first support hole and second support hole, in addition, both sides of wing body are fixed through first wing body hole and second wing body hole respectively, the both sides of wing body all obtain the support, the difficult torsional deformation that takes place for the wing body.
As some sub-schemes of the above technical scheme, a first vehicle body mounting plate is arranged on the left side of the cross beam, and the first bracket hole is formed in the first vehicle body mounting plate.
As some sub-aspects of the above technical solution, the first vehicle body mounting plate is provided with a first vehicle positioning pin, and the first vehicle positioning pin extends downward.
As some sub-schemes of the technical scheme, the first vehicle body mounting plate is L-shaped, the first vehicle body mounting plate comprises a transverse plate and a vertical plate which are connected together, the first bracket hole is formed in the transverse plate, and the vertical plate is connected with one side of the transverse plate.
As some sub-schemes of the above technical scheme, the first wing body mounting plate is provided with a wing body positioning pin, and the wing body positioning pin extends upwards.
As some sub-schemes of the above technical scheme, the number of the first wing body holes is two, and the two first wing body holes are respectively located at two sides of the wing body positioning pin.
As some sub-schemes of the above technical scheme, a reinforcing plate is further arranged between the first upright post and the cross beam.
As some sub-aspects of the above technical solution, the reinforcing plate is triangular.
As some sub-schemes of the above technical scheme, the beam is provided with a direction mark.
As some sub-aspects of the above technical solution, the beam is a hollow tube.
Drawings
The foregoing and/or additional aspects and advantages of the utility model will become apparent and may be better understood from the following description of embodiments taken in conjunction with the accompanying drawings in which:
FIG. 1 is an isometric view of an embodiment of an integrated bracket for tail coating;
FIG. 2 is a second perspective view of an embodiment of an integrated bracket for tail coating;
FIG. 3 is an isometric third view of an embodiment of an integrated bracket for tail coating;
FIG. 4 is a schematic view of the structure of an integrated bracket and tail assembly;
fig. 5 is an integrated bracket. A first schematic diagram of the assembly of the tail wing and the body frame;
fig. 6 is an integrated bracket. And a second schematic diagram of the assembly of the tail wing and the vehicle body frame.
In the accompanying drawings: 1-a cross beam; 11-a first bracket aperture; 12-a second bracket aperture; 13-direction identification;
2-a first upright; 21-a reinforcing plate;
3-a second upright;
4-a first wing mounting plate; 41-a first wing aperture; 42-wing body locating pins;
5-a second wing mounting plate; 51-a second wing aperture;
6-a first body mounting plate; 61-a first vehicle locating pin;
7-a second body mounting plate; 71-a second vehicle locating pin;
81-tail fin; 82-a body frame;
91-round washers; 92-kidney shaped gasket.
Detailed Description
Embodiments of the present utility model are described in detail below, examples of which are illustrated in the accompanying drawings, wherein like or similar reference numerals refer to like or similar elements or elements having like or similar functions throughout. The embodiments described below by referring to the drawings are illustrative only and are not to be construed as limiting the utility model.
In the description of the present utility model, it should be understood that references to orientation descriptions such as upper, lower, front, rear, left, right, etc. are based on the orientation or positional relationship shown in the drawings, are merely for convenience of description of the present utility model and to simplify the description, and do not indicate or imply that the apparatus or elements 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 utility model.
In the description of the present utility model, the meaning of a number is not quantitative, and the meaning of a number is two or more, and greater than, less than, exceeding, etc. are understood to exclude the present number, and the meaning of above, below, within, etc. are understood to include the present number. The description of the first and second is for the purpose of distinguishing between technical features only and should not be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated or implicitly indicating the precedence of the technical features indicated. Appear throughout and/or represent three parallel schemes, e.g., a and/or B represent a scheme that is met by a, a scheme that is met by B, or a scheme that is met by a and B simultaneously.
In the description of the utility model, there are phrases containing a plurality of parallel features, where the phrase defines a feature that is closest, for example: b, C provided on A, E connected with D, which means that B is provided on A, E connected with D, and C is not limited; but for the words representing the relationship between features, such as "spaced arrangement", "annular arrangement", etc., do not belong to this category. The phrase preceded by a "homonym" indicates that all features in the phrase are defined, e.g., B, C, D, all disposed on a, and B, C and D are disposed on a. The sentence of the subject is omitted, and the omitted subject is the subject of the previous sentence, namely, B is arranged on A and comprises C, B is arranged on A, and A comprises C.
In the description of the present utility model, unless explicitly defined otherwise, terms such as arrangement, installation, connection, etc. should be construed broadly and the specific meaning of the terms in the present utility model can be reasonably determined by a person skilled in the art in combination with the specific contents of the technical scheme.
Embodiments of the present utility model are described below with reference to fig. 1 to 6.
The present embodiment relates to an integral bracket for fin coating, so that before fin 81 is sprayed, fin 81 and body frame 82 are fixed together and enter a spraying line for spraying treatment, so as to obtain fin 81 and body frame 82 with consistent surface color.
An integral bracket for tail coating of the embodiment includes: the novel wing structure comprises a cross beam 1, a first upright 2 and a second upright 3, wherein a first bracket hole 11 and a second bracket hole 12 are respectively arranged on the left side and the right side of the cross beam 1, the first bracket hole 11 and the second bracket hole 12 extend vertically, a first wing body mounting plate 4 is arranged on the first upright 2, a first wing body hole 41 is arranged on the first wing body mounting plate 4, a second wing body mounting plate 5 is arranged on the second upright 3, and a second wing body hole 51 is arranged on the second wing body mounting plate 5.
When the integrated bracket is used, the tail wing 81 is fastened by penetrating bolts through the first wing body hole 41 and the second wing body hole 51, and then the tail wing 81 and the vehicle body frame 82 are transversely fastened to the vehicle body frame 82 through the first bracket hole 11 and the second bracket hole 12 by bolts, so that the installation and the fixation of the integrated bracket are completed, and the tail wing 81 and the vehicle body frame 82 are fixed together. Since the left and right sides of the tail wing 81 are fixedly supported through the first wing body hole 41 and the second wing body hole 51, respectively, both sides of the tail wing 81 are supported in the vertical direction, the tail wing 81 does not generate additional torque under the self weight, and the structural strength of the tail wing 81 is high.
In addition, this region that integral type support and fin 81 are connected is located the downside of fin 81, and fin 81 and vehicle are all difficult for being seen under the state of finished product assembly, can not produce visual outward appearance surface colour difference, and in addition first wing body mounting panel 4 and second wing body mounting panel 5 are put up by first stand 2 and second stand 3 respectively, are convenient for squeeze into the sealant when fixing fin 81 through first wing body mounting panel 4 and second wing body mounting panel 5.
Moreover, because the first bracket hole 11 and the second bracket hole 12 extend vertically, when the beam 1 is fixed on a vehicle body, the beam 1 is only required to be placed on the vehicle body frame 82 vertically, and then the beam 1 and the vehicle body frame 82 are locked together vertically, so that the operation is convenient.
The left side of the beam 1 is provided with a first vehicle body mounting plate 6, and the first bracket hole 11 is formed in the first vehicle body mounting plate 6. In this embodiment, the left side of the beam 1 is additionally provided with the first vehicle body mounting plate 6 and the first bracket hole 11 is formed on the first vehicle body mounting plate 6, so that the first bracket hole 11 is prevented from being formed on the beam 1, and the structural strength of the beam 1 can be ensured.
Further, the first vehicle body mounting plate 6 is provided with a first vehicle positioning pin 61, and the first vehicle positioning pin 61 protrudes downward. By providing the first vehicle positioning pin 61 protruding downward, the first vehicle body mounting plate 6 and the vehicle body frame 82 can be positioned by the first vehicle positioning pin 61 so as to quickly lock the first vehicle body mounting plate 6 by penetrating the bolt at the first bracket hole 11 when the integrated bracket is assembled with the vehicle body frame 82.
Further, the first vehicle body mounting plate 6 is in an L shape, the first vehicle body mounting plate 6 includes a cross plate and a vertical plate connected together, the first bracket hole 11 is formed on the cross plate, and the vertical plate is connected with one side of the cross beam 1.
In this embodiment, the beam 1 is a hollow tube. The beam 1 adopts a hollow tube, which is beneficial to weight reduction and has certain structural support strength. More specifically the cross beam 1 is a hollow metal tube. Specifically, the riser is welded with the terminal surface welded fastening of crossbeam 1 and seals the terminal surface of crossbeam 1, adopts the welded mode to have the nimble advantage in structure fixed position.
In the present embodiment, a second body mounting plate 7 is provided on the other side of the cross member 1. The second body mounting plate 7 has the same structure as the first body mounting plate 6, and the second body mounting plate 7 and the first body mounting plate 6 are in mirror-symmetrical relation to each other. The second body mounting plate 7 and the tail wing 81 are also fixed by bolts, and the second body mounting plate 7 is correspondingly provided with a second positioning pin 71.
The first wing body mounting plate 4 is provided with a wing body positioning pin 42, and the wing body positioning pin 42 extends upwards. By providing the wing positioning pins 42, the positioning of the tail wing 81 can be quickly achieved when the tail wing 81 is mounted with the first wing mounting plate 4.
The number of the first wing body holes 41 is two, and the two first wing body holes 41 are respectively positioned at two sides of the wing body positioning pin 42. The arrangement of two first wing holes 41 can improve the stability of mounting of the tail wing 81 and the first wing mounting plate 4.
A reinforcing plate 21 is also arranged between the first upright 2 and the cross beam 1. The reinforcement plate 21 is provided between the first column 2 and the cross member 1, so that the support strength of the first column 2 can be improved.
The reinforcing plate 21 has a triangular shape. The triangle has the characteristic of stable support, and the triangular structure of the reinforcing plate 21 is beneficial to improving the support capacity of the first upright 2.
In the present embodiment, the structures of the second upright 3 and the second wing mounting plate 5 are the same as those of the first wing mounting plate 4 and the second upright 3, and the second upright 3 is also correspondingly provided with a reinforcing plate 21 for supporting. Two second wing holes 51 are also provided in the second wing mounting plate 5. The second wing mounting plate 5 is also provided with a wing positioning pin 42.
The beam 1 is provided with a direction mark 13. The direction mark 13 is arranged on the cross beam 1, so that an operator can quickly and clearly distinguish the direction, and the risk of misloading is reduced.
In addition, a circular washer 91 is provided on the top surfaces of the first wing mounting plate 4 and the second wing mounting plate 5 to relieve pressure on the tail wing 81 when the tail wing 81 is fixed. Waist washers 92 are also provided on the underside of the first body mounting plate 6 and the underside of the second body mounting plate 7 to relieve pressure on the body frame 82.
While the preferred embodiment of the present utility model has been described in detail, the utility model is not limited to the embodiments, and various equivalent modifications and substitutions can be made by those skilled in the art without departing from the spirit of the utility model, and these equivalent modifications and substitutions are intended to be included in the scope of the utility model as defined in the appended claims.
Claims (10)
1. A integral type support for fin application, its characterized in that: comprising the following steps: the novel wing structure comprises a cross beam (1), a first upright (2) and a second upright (3), wherein a first bracket hole (11) and a second bracket hole (12) are respectively formed in the left side and the right side of the cross beam (1), the first bracket hole (11) and the second bracket hole (12) extend vertically, a first wing body mounting plate (4) is arranged on the first upright (2), a first wing body hole (41) is formed in the first wing body mounting plate (4), a second wing body mounting plate (5) is arranged on the second upright (3), and a second wing body hole (51) is formed in the second wing body mounting plate (5).
2. An integrated bracket for tail painting according to claim 1, characterized in that: the left side of the beam (1) is provided with a first vehicle body mounting plate (6), and the first bracket hole (11) is formed in the first vehicle body mounting plate (6).
3. An integrated bracket for tail painting according to claim 2, characterized in that: the first vehicle body mounting plate (6) is provided with a first vehicle positioning pin (61), and the first vehicle positioning pin (61) extends downwards.
4. An integrated bracket for tail painting according to claim 2, characterized in that: the first vehicle body mounting plate (6) is L-shaped, the first vehicle body mounting plate (6) comprises a transverse plate and a vertical plate which are connected together, the transverse plate is provided with a first bracket hole (11), and the vertical plate is connected with one side of the transverse beam (1).
5. An integrated bracket for tail painting according to claim 1, characterized in that: the first wing body mounting plate (4) is provided with a wing body positioning pin (42), and the wing body positioning pin (42) extends upwards.
6. An integrated bracket for tail coating as set forth in claim 5, wherein: the number of the first wing body holes (41) is two, and the two first wing body holes (41) are respectively positioned at two sides of the wing body positioning pin (42).
7. An integrated bracket for tail painting according to claim 1, characterized in that: a reinforcing plate (21) is further arranged between the first upright post (2) and the cross beam (1).
8. An integrated bracket for tail painting according to claim 7, characterized in that: the reinforcing plate (21) is triangular.
9. An integrated bracket for tail painting according to claim 1, characterized in that: the beam (1) is provided with a direction mark (13).
10. An integrated bracket for tail painting according to claim 1, characterized in that: the cross beam (1) is a hollow tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321898231.XU CN220406038U (en) | 2023-07-19 | 2023-07-19 | A integral type support for fin application |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321898231.XU CN220406038U (en) | 2023-07-19 | 2023-07-19 | A integral type support for fin application |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220406038U true CN220406038U (en) | 2024-01-30 |
Family
ID=89652856
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321898231.XU Active CN220406038U (en) | 2023-07-19 | 2023-07-19 | A integral type support for fin application |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220406038U (en) |
-
2023
- 2023-07-19 CN CN202321898231.XU patent/CN220406038U/en active Active
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| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |