CN204883498U - All -in -one computer - Google Patents
All -in -one computer Download PDFInfo
- Publication number
- CN204883498U CN204883498U CN201520557848.4U CN201520557848U CN204883498U CN 204883498 U CN204883498 U CN 204883498U CN 201520557848 U CN201520557848 U CN 201520557848U CN 204883498 U CN204883498 U CN 204883498U
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- CN
- China
- Prior art keywords
- center
- fuselage
- rotary shaft
- opening
- shaft rack
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Abstract
The utility model discloses an all -in -one computer, including the fuselage, pivot support and base are equipped with the center on the fuselage, center and backshell fixed connection, and the center includes the holding portion relative with the backshell to and connect the lateral wall of holding portion and center lateral part frame, the bottom that is close to the center on the lateral wall is equipped with the opening, enhancement panel beating on pivot support and the fuselage become a body structure set firmly in the opening part of center bottom. Having saved one like this and having strengthened the panel beating, the cost is reduced has strengthened the plastics center, has played the effect of pivot, and lies in the fuselage bottom, does not account for the space, and back lid detachable fixed connection in opening part, it is irrelevant whether the dismouting and the base of back lid are connected on the pivot support, when the computer is reprocessed, need not to pull down the base and just can pull down back lid, ten minutes convenience like this.
Description
Technical field
The utility model relates to computer technology field, relates to a kind of integrated computer in particular.
Background technology
Integrated computer of the prior art is all first be fixed on fuselage by rotary shaft rack, then by screw thread, bonnet is being fixedly connected on fuselage, finally base is fixedly connected on rotary shaft rack, when bonnet removes by needs, just need base of first dismantling like this, then just can pull down bonnet, seem very loaded down with trivial details, in addition, adopt above-mentioned installation method, just need to strengthen panel beating by rotary shaft rack fixed main body with one piece, cost is increased.
Utility model content
The utility model, in order to solve existing problem, provides a kind of integrated computer, by by into a single integrated structure for the reinforcement panel beating on rotary shaft rack and the fuselage opening part being fixedly arranged on middle frame bottom, thus reduces cost, conserve space.
The technical solution of the utility model is: a kind of integrated computer, comprise fuselage, rotary shaft rack and base, fuselage is provided with center, center is fixedly connected with back cover, and center comprises the holding part relative with back cover, and connects the sidewall of holding part and center side edge frame, sidewall is provided with opening near the bottom of center, the into a single integrated structure opening part being fixedly arranged on described middle frame bottom of reinforcement panel beating on described rotary shaft rack and fuselage.
Preferably, the opening part both sides of described middle frame bottom are provided with the bonnet with opening adaptation, and bonnet is dismountable is fixedly connected on opening both sides place.
Preferably, the bottom of described rotary shaft rack is provided with the relative brace of perpendicular two of outwards bending, and each described brace is flexibly connected with a connecting screw rod, and described connecting screw rod is provided with the threaded hole be connected with base.
Preferably, described rotary shaft rack is evenly distributed with threaded hole.
Preferably, the opening part of described middle frame bottom and the both sides being positioned at described rotary shaft rack are provided with heat sink, described heat sink is provided with louvre.
Preferably, be provided with the threaded post with its one in described holding part, in described threaded post, be provided with threaded hole.
A kind of integrated computer of the present utility model, by into a single integrated structure for the reinforcement panel beating on rotary shaft rack and the fuselage opening part being fixedly arranged on middle frame bottom, makes to save one piece and strengthens panel beating, reduce cost, strengthen plastic middle-frame, serve the effect of rotating shaft, and be positioned at fuselage bottom, conserve space.And bonnet is dismountable is fixedly connected on opening part, it is irrelevant whether the dismounting of bonnet and base are connected on rotary shaft rack, like this when computer is reprocessed, just can pull down bonnet without the need to pulling down base, very convenient.
Accompanying drawing explanation
Fig. 1 is the structural drawing of the new a kind of integrated computer of this practicality.
Fig. 2 is the enlarged drawing at A place in Fig. 1.
The structural drawing of Fig. 3 position the utility model shaft support.
Rotary shaft rack in the utility model of Fig. 4 position to be arranged on after on fuselage schematic diagram from the side.
Embodiment
As depicted in figs. 1 and 2, a kind of integrated computer, comprise fuselage, rotary shaft rack and base, fuselage is provided with center, center 10 is fixedly connected with by screw with back cover (not shown in FIG.), center 10 comprises the holding part 11 relative with back cover, and connect the sidewall 14 of holding part 11 and center 10 side edge frame, bottom near center 10 on sidewall 14 is provided with opening 13, this rotary shaft rack 12 and into a single integrated structure opening 13 place be fixedly arranged on bottom center 10 of reinforcement panel beating on fuselage, here opening 13 is that conveniently rotary shaft rack 12 is fixed on fuselage and facilitates rotary shaft rack 12 and base to be connected and fixed.
In the present embodiment, sidewall 14 comprises left side wall and right side wall, and connects the upper side wall of left side wall and right side wall, and whole like this sidewall 14 is arranged in inverted C type.
Both sides, opening 13 place bottom center 10 are provided with the bonnet 20 with opening 13 adaptation, bonnet 20 is dismountable is fixedly connected on opening 13 both sides place, because rotary shaft rack 12 is into a single integrated structure with the reinforcement panel beating on fuselage, such rotary shaft rack 12 can directly be fixedly connected with base, it is irrelevant whether the dismounting of bonnet and base are connected on rotary shaft rack, so when bonnet pulled down by needs, just do not need base first to pull down to pull down bonnet again, the dismounting of such bonnet is very convenient, saves time.
Rotary shaft rack 12 is evenly distributed with threaded hole 122, opening 13 place bottom the center 10 and both sides being positioned at rotary shaft rack 12 are provided with heat sink 30, heat sink 30 is provided with louvre 31.The threaded post 111 with its one is provided with in holding part 11, threaded hole is provided with in threaded post 111, the threaded hole of threaded post 111 is mainly used in being fixedly connected with by screw thread with back cover, in the present embodiment, threaded post 111 is randomly arranged at holding part 11, arrange according to the actual requirements, mainly in order to can be convenient with back cover connection.
As shown in Figure 3 and Figure 4, the bottom of rotary shaft rack 12 is provided with the relative brace 121 of perpendicular two of outwards bending, brace 121 and rotary shaft rack 12 are structure as a whole, and each brace 121 is flexibly connected with a connecting screw rod 15, and connecting screw rod 15 is provided with the threaded hole be connected with base.The present embodiment is flexibly connected with connecting screw rod 15 due to rotary shaft rack 12, and connecting screw rod 15 is fixedly connected with base, and such rotary shaft rack serves again the effect of rotating shaft, and strengthens plastic middle-frame.
Above specific embodiment is only in order to illustrate design of the present utility model, and those of ordinary skill in the art can make various deformation and change under design of the present utility model, and these distortion and change include within protection domain of the present utility model.
Claims (6)
1. an integrated computer, comprise fuselage, rotary shaft rack and base, fuselage is provided with center (10), center (10) is fixedly connected with back cover, center (10) comprises the holding part (11) relative with back cover, and connect the sidewall (14) of holding part (11) and center (10) side edge frame, the upper bottom near center (10) of sidewall (14) is provided with opening (13), it is characterized in that: described rotary shaft rack (12) opening (13) place that be fixedly arranged on described center (10) bottom into a single integrated structure with the reinforcement panel beating on fuselage.
2. a kind of integrated computer according to claim 1, it is characterized in that: opening (13) both sides, place of described center (10) bottom are provided with the bonnet (20) adaptive with opening (13), and bonnet (20) is dismountable is fixedly connected on opening (13) both sides place.
3. a kind of integrated computer according to claim 1, it is characterized in that: the bottom of described rotary shaft rack (12) is provided with the relative brace (121) of perpendicular two of outwards bending, each described brace (121) is flexibly connected with a connecting screw rod (15), and described connecting screw rod (15) is provided with the threaded hole be connected with base.
4. a kind of integrated computer according to claim 3, is characterized in that: described rotary shaft rack (12) is evenly distributed with threaded hole (122).
5. a kind of integrated computer according to claim 1, it is characterized in that: opening (13) place of described center (10) bottom and the both sides being positioned at described rotary shaft rack (12) are provided with heat sink (30), described heat sink (30) is provided with louvre (31).
6. a kind of integrated computer according to claim 1, is characterized in that: be provided with the threaded post (111) with its one in described holding part (11), be provided with threaded hole in described threaded post.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520557848.4U CN204883498U (en) | 2015-07-29 | 2015-07-29 | All -in -one computer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520557848.4U CN204883498U (en) | 2015-07-29 | 2015-07-29 | All -in -one computer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204883498U true CN204883498U (en) | 2015-12-16 |
Family
ID=54827854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520557848.4U Active CN204883498U (en) | 2015-07-29 | 2015-07-29 | All -in -one computer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204883498U (en) |
-
2015
- 2015-07-29 CN CN201520557848.4U patent/CN204883498U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address |
Address after: 518108 Fourth Floor of Building A, Xinhui Industrial Zone, Tangtou Third Industrial Park, Tangtou Community, Shiyan Street, Baoan District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Changxiang Vision Technology Co., Ltd. Address before: 518000 6th Floor, Building A, Xinhui Industrial Zone, Tangtou Third Industrial Park, Tangtou Community, Shiyan Street, Baoan District, Shenzhen City, Guangdong Province Patentee before: Free thought great achievement Science and Technology Ltd. of Shenzhen |
|
| CP03 | Change of name, title or address |