CN220326064U - High-performance aluminum alloy tail cabin shell - Google Patents
High-performance aluminum alloy tail cabin shell Download PDFInfo
- Publication number
- CN220326064U CN220326064U CN202321758027.8U CN202321758027U CN220326064U CN 220326064 U CN220326064 U CN 220326064U CN 202321758027 U CN202321758027 U CN 202321758027U CN 220326064 U CN220326064 U CN 220326064U
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- China
- Prior art keywords
- aluminum alloy
- fixedly connected
- tail cabin
- high performance
- cabin shell
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- 229910000838 Al alloy Inorganic materials 0.000 title claims abstract description 49
- 238000009434 installation Methods 0.000 claims description 15
- 238000005192 partition Methods 0.000 claims description 4
- 239000007779 soft material Substances 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000017525 heat dissipation Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 239000011435 rock Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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- Body Structure For Vehicles (AREA)
Abstract
The utility model relates to a high-performance aluminum alloy tail cabin shell, which comprises an aluminum alloy tail cabin shell, wherein both sides of the inner wall of the aluminum alloy tail cabin shell are fixedly connected with a mounting box, the inside of the mounting box is provided with a fixing mechanism, the fixing mechanism comprises a sliding groove, a fixing rod, two L-shaped plates, a spring, a clamping plate, a lug and a groove, the inside of the mounting box is provided with the sliding groove, the inside of the sliding groove is fixedly connected with the fixing rod, and the outside of the fixing rod is slidably connected with the two L-shaped plates. The utility model has the advantages that larger components such as a CPU can be placed in the corresponding mounting box, the corresponding L-shaped plate can be driven to move by the elasticity of the spring, and meanwhile, the clamping plate can be driven to move, so that the convex blocks are clamped with the corresponding grooves, thereby playing an important role in fixing the components, avoiding damage caused by shaking of the components in the mounting box, and further prolonging the service life of the components in the aluminum alloy tail cabin shell.
Description
Technical Field
The utility model relates to the technical field of aluminum alloy, in particular to a high-performance aluminum alloy tail cabin shell.
Background
The aluminum alloy is the most widely used nonferrous metal structural material in industry, is widely used in aviation, aerospace, automobile, mechanical manufacturing, ship and chemical industry, has rapid development of industrial economy, has increasingly increased demands on aluminum alloy welding structural members, enables the welding research of the aluminum alloy to be deep, is the most widely used alloy at present, has low density but higher strength, is close to or exceeds high-quality steel, has good plasticity, can be processed into various sectional materials, has excellent electrical conductivity, thermal conductivity and corrosion resistance, is widely used in industry, has the use amount which is only inferior to steel, and is mostly made of aluminum when the current tail cabin shell is used.
When the existing high-performance aluminum alloy tail cabin shell is used, circuit main boards with different thicknesses cannot be fixed inside, so that when the existing high-performance aluminum alloy tail cabin shell moves, a CPU is easy to wear with the inside of the aluminum alloy tail cabin shell, the service life of the CPU is further shortened, and practical application and popularization are not facilitated.
Disclosure of Invention
In view of the foregoing problems of the prior art, a primary object of the present utility model is to provide a high performance aluminum alloy tailgate housing.
The technical scheme of the utility model is as follows: the utility model provides a high performance aluminum alloy tailstock casing, includes aluminum alloy tailstock casing, the equal fixedly connected with install bin in both sides of aluminum alloy tailstock shells inner wall, the inside of install bin all is provided with fixed establishment, fixed establishment includes spout, dead lever, two L shaped plates, spring, grip block, lug and recess, the spout has all been seted up to the inside of install bin, the equal fixedly connected with dead lever in inside of spout, the outside sliding connection of dead lever has two L shaped plates, L shaped plate all with dead lever sliding connection, L shaped plate all with the inner wall sliding connection of spout, the both sides of dead lever all overlap the spring, the equal fixedly connected with grip block in top of L shaped plate, one of them the outside fixedly connected with lug of L shaped plate, another the inside of L shaped plate is seted up flutedly, the lug all with recess looks joint.
As a preferred embodiment, fixed establishment still includes apron, joint spare, fixed plate, buckle and chock, the top of installation case all is provided with the apron, the equal fixedly connected with joint spare in both sides of apron, the equal fixedly connected with fixed plate in both sides of installation case, the top of fixed plate all is connected with the buckle through torsion spring rotation, the buckle all with joint spare looks joint, the bottom fixedly connected with chock of apron.
As a preferred implementation mode, radiating holes are formed in the installation box at equal intervals, and two radiating fins are fixedly installed on the periphery of the aluminum alloy tail cabin shell.
As a preferred embodiment, the top of each buckle is fixedly connected with a spanner.
As a preferred embodiment, the partition plates are fixedly connected to the inner wall of the aluminum alloy tail cabin shell and positioned between the two mounting boxes.
As a preferred embodiment, the outer side of the aluminum alloy tail cabin shell is fixedly provided with a mounting groove.
Compared with the prior art, the utility model has the advantages and positive effects that,
according to the utility model, larger components (such as a CPU) can be placed in the corresponding mounting boxes, the corresponding L-shaped plates can be driven to move through the elasticity of the springs, and meanwhile, the clamping plates can be driven to move, so that the convex blocks are clamped with the corresponding grooves, an important fixing effect on the components can be achieved, the damage caused by shaking of the components in the mounting boxes is avoided, and the service life of the components in the aluminum alloy tail cabin shell is further prolonged; after the bottom of components and parts is fixed, can cover the apron and install on the case to with torsion spring's setting, accessible buckle carries out the joint with the joint spare that corresponds, and then can plug in the top of components and parts through the chock of soft material, avoids components and parts to take place the condition of moving about in the installation case.
Drawings
FIG. 1 is a perspective view of a high performance aluminum alloy nacelle housing according to the utility model;
FIG. 2 is a front cross-sectional view of a high performance aluminum alloy nacelle housing according to the utility model;
FIG. 3 is a side cross-sectional view of a high performance aluminum alloy nacelle housing according to the utility model;
FIG. 4 is an enlarged view of the high performance aluminum alloy nacelle housing of FIG. 2 at A in accordance with the utility model;
fig. 5 is an enlarged view of the high performance aluminum alloy nacelle housing of fig. 3 at B.
Legend description: 1. an aluminum alloy tail cabin shell; 2. a mounting box; 3. a heat radiation hole; 4. a heat radiation fin; 5. a chute; 6. an L-shaped plate; 7. a fixed rod; 8. a spring; 9. a clamping plate; 10. a bump; 11. a groove; 12. a cover plate; 13. a clamping piece; 14. a wrench; 15. a buckle; 16. a partition plate; 17. a fixing plate; 18. a chock; 19. and a mounting groove.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. The components of the embodiments of the present utility model generally described and illustrated in the figures herein may be arranged and designed in a wide variety of different configurations. Thus, the following detailed description of the embodiments of the utility model, as presented in the figures, is not intended to limit the scope of the utility model, as claimed, but is merely representative of selected embodiments of the utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
The utility model will be further described with reference to the drawings and the specific embodiments
Examples
As shown in fig. 1, 2, 3, 4 and 5, the present utility model provides a technical solution: the aluminum alloy tail cabin comprises an aluminum alloy tail cabin shell body 1, wherein the two sides of the inner wall of the aluminum alloy tail cabin shell body 1 are fixedly connected with a mounting box 2, the inside of the mounting box 2 is provided with a fixing mechanism, the fixing mechanism comprises a sliding chute 5, a fixing rod 7, two L-shaped plates 6, a spring 8, a clamping plate 9, a lug 10 and a groove 11, the inside of the mounting box 2 is provided with the sliding chute 5, the inside of the sliding chute 5 is fixedly connected with the fixing rod 7, the outer side of the fixing rod 7 is slidably connected with the two L-shaped plates 6, the L-shaped plates 6 are slidably connected with the fixing rod 7, the two sides of the fixing rod 7 are sleeved with the spring 8, the top of the L-shaped plates 6 are fixedly connected with the clamping plate 9, the outer side of one L-shaped plate 6 is fixedly connected with the lug 10, the inside of the other L-shaped plate 6 is provided with the groove 11, and the lug 10 is clamped with the groove 11;
through above-mentioned technical scheme, can put into the installation case 2 that corresponds with great components and parts (like CPU), through the elasticity of spring 8, can drive the L shaped plate 6 that corresponds and remove, can drive the removal of grip block 9 simultaneously, and then can cause lug 10 and the recess 11 looks joint that corresponds to can play important fixed action to components and parts, avoid the components and parts to appear rocking in installation case 2 and cause the damage, further improved the life of components and parts in the aluminum alloy tailstock casing 1.
The fixing mechanism further comprises a cover plate 12, clamping pieces 13, fixing plates 17, buckles 15 and plugs 18, wherein the cover plate 12 is arranged at the top of the mounting box 2, the clamping pieces 13 are fixedly connected to the two sides of the cover plate 12, the fixing plates 17 are fixedly connected to the two sides of the mounting box 2, the buckles 15 are rotatably connected to the top of the fixing plates 17 through torsion springs, the buckles 15 are clamped with the clamping pieces 13, and the plugs 18 are fixedly connected to the bottom of the cover plate 12;
through above-mentioned technical scheme, after fixing the bottom of components and parts, can cover the apron 12 on the mounting box 2 to with torsion spring's setting, accessible buckle 15 carries out the joint with the joint piece 13 that corresponds, and then can be through the chock 18 of soft material with the top of components and parts packing in, avoid the components and parts to take place the condition of moving in the mounting box 2.
Wherein, the inside of the installation box 2 is provided with radiating holes 3 at equal intervals, and two radiating fins 4 are fixedly arranged on the periphery of the aluminum alloy tail cabin shell 1;
through the setting of louvre 3, can be with the heat transmission that the components and parts give off outside the aluminum alloy tailstock casing 1 to through radiating fin 4 quickening radiating efficiency, avoid thermal piling up.
The top of each buckle 15 is fixedly connected with a spanner 14;
by means of the arrangement of the wrench 14, the unlocking operation of the cover plate 12 is facilitated.
Wherein, the inner wall of the aluminum alloy tail cabin shell 1 is fixedly connected with a baffle 16 between the two mounting boxes 2;
by separating the positions of the components and by providing the partition plate 16, the interference (electromagnetic interference) between the high-power components, which may occur due to the close mounting, can be avoided.
Wherein, the outside of the aluminum alloy tail cabin shell 1 is fixedly provided with a mounting groove 19;
by means of the arrangement of the mounting groove 19, a quick mounting thereof is facilitated.
Working principle:
as shown in fig. 1, fig. 2, fig. 3, fig. 4 and fig. 5, firstly, put into the installation case 2 that corresponds with great components and parts (such as CPU), elasticity through spring 8 can drive the L shaped plate 6 that corresponds and remove, can drive the removal of grip block 9 simultaneously, and then can cause lug 10 and the looks joint of corresponding recess 11, thereby can play important fixed action to components and parts, avoid the components and parts to appear rocking and cause the damage in installation case 2, further improved the life of components and parts in the aluminum alloy tailstock casing 1, after fixing the bottom of components and parts, can cover the apron 12 on the installation case 2, and with torsion spring's setting, accessible buckle 15 and the joint piece 13 that corresponds, and then can be through the top of soft material's chock 18 with components and parts, avoid the components and parts to take place the condition of moving in disorder in the installation case 2, through the setting of louvre 3, can be with the heat transmission that components and parts give off outside aluminum alloy tailstock casing 1, and through the radiating fin appearance and rock and cause the damage, further improved the life of components and parts in the installation place to parts and parts can be close to each other because of the interference can be avoided between the setting up through the heat dissipation fin 16.
Finally, it should be noted that: the embodiments described above are only for illustrating the technical solution of the present utility model, and are not limiting; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some or all of the technical features thereof can be replaced with equivalents; such modifications and substitutions do not depart from the spirit of the utility model.
Claims (6)
1. The utility model provides a high performance aluminum alloy tail cabin casing, includes aluminum alloy tail cabin casing (1), its characterized in that: the utility model provides an aluminum alloy tailstock casing (1) inner wall's both sides equal fixedly connected with install bin (2), the inside of install bin (2) all is provided with fixed establishment, fixed establishment includes spout (5), dead lever (7), two L shaped plates (6), spring (8), grip block (9), lug (10) and recess (11), spout (5) have all been seted up to the inside of install bin (2), the equal fixedly connected with dead lever (7) of inside of spout (5), the outside sliding connection of dead lever (7) has two L shaped plates (6), L shaped plate (6) all with dead lever (7) sliding connection, the inner wall sliding connection of L shaped plate (6) all with spout (5), the both sides of dead lever (7) all overlap spring (8), the equal fixedly connected with grip block (9) in top of L shaped plate (6), one of them outside fixedly connected with lug (10) has been seted up in the inside of L shaped plate (6), lug (10) all connect with recess (11).
2. A high performance aluminum alloy boot shell as recited in claim 1, wherein: the fixing mechanism further comprises a cover plate (12), a clamping piece (13), a fixing plate (17), a buckle (15) and a plug block (18), the top of the installation box (2) is provided with the cover plate (12), the two sides of the cover plate (12) are fixedly connected with the clamping piece (13), the two sides of the installation box (2) are fixedly connected with the fixing plate (17), the top of the fixing plate (17) is fixedly connected with the buckle (15) through torsion springs in a rotating mode, the buckle (15) is fixedly connected with the clamping piece (13) in a clamping mode, and the bottom of the cover plate (12) is fixedly connected with the plug block (18).
3. A high performance aluminum alloy boot shell as recited in claim 1, wherein: the inside of the installation box (2) is provided with radiating holes (3) at equal intervals, and two radiating fins (4) are fixedly installed around the aluminum alloy tail cabin shell (1).
4. A high performance aluminum alloy boot shell as recited in claim 2, wherein: the top of buckle (15) all fixedly connected with spanner (14).
5. A high performance aluminum alloy boot shell as recited in claim 1, wherein: the inner wall of the aluminum alloy tail cabin shell (1) is fixedly connected with a partition plate (16) between the two mounting boxes (2).
6. A high performance aluminum alloy boot shell as recited in claim 1, wherein: the outside of the aluminum alloy tail cabin shell (1) is fixedly provided with a mounting groove (19).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321758027.8U CN220326064U (en) | 2023-07-06 | 2023-07-06 | High-performance aluminum alloy tail cabin shell |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202321758027.8U CN220326064U (en) | 2023-07-06 | 2023-07-06 | High-performance aluminum alloy tail cabin shell |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220326064U true CN220326064U (en) | 2024-01-09 |
Family
ID=89417395
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202321758027.8U Active CN220326064U (en) | 2023-07-06 | 2023-07-06 | High-performance aluminum alloy tail cabin shell |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220326064U (en) |
-
2023
- 2023-07-06 CN CN202321758027.8U patent/CN220326064U/en active Active
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