CN101165814A - Panel display bracket assembly - Google Patents
Panel display bracket assembly Download PDFInfo
- Publication number
- CN101165814A CN101165814A CNA2006100966703A CN200610096670A CN101165814A CN 101165814 A CN101165814 A CN 101165814A CN A2006100966703 A CNA2006100966703 A CN A2006100966703A CN 200610096670 A CN200610096670 A CN 200610096670A CN 101165814 A CN101165814 A CN 101165814A
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- supporting arm
- fuselage
- mentioned
- folding
- base
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Abstract
The invention can be used for freely adjusting the position of the display body; when making package or hanging it on the wall; the size of the display can be reduced to the minimum. It comprises: a base plate located on the table; a rotatable first support arm located at one side of the base plate; a rotatable second support arm located at the first arm; a back surface used for fixing the display body and located on the first arm and second arm.
Description
Technical field
The present invention relates to flat-panel monitor,, when packing or being hung on the wall, its volume can be reduced to the bracket component (stand assembly) of minimum flat-panel monitor especially about the fuselage position freely being regulated.
Background technology
As everyone knows, flat-panel monitor is not only the display of desktop computer, also is the necessary display device that comprises miniaturization and systems such as portable computers such as notebook computer, PDA or mobile phone.
As this flat-panel monitor, mainly contain LCD (LCD:LiquidCrystal Display Device) now, plasma display (PDP:Plasma DisplayPanel), and Field Emission Display are called for short FED (Field Emission Display) etc.
It is better that these flat-panel monitors and leonard's tube (CRT) are compared usability, and the average power consumption also CRT than identical image size is little, and thermal discharge is also little in addition.So obtain paying close attention to as display device of future generation such as mobile phone or computer monitor, TVs recently.
Below, with reference to accompanying drawing to the explanation simply in addition of the flat-panel monitor under the prior art.
Fig. 1 is the synoptic diagram according to the flat-panel monitor summary structure of prior art.
With reference to Fig. 1, the flat-panel monitor of prior art is made of the fuselage 1 of display image and the bracket component (stand assembly) of support fuselage 1.
Here, above-mentioned bracket component is divided into base 2 again; Supporting arm 3; Articulated elements 4.
Above-mentioned base 2 places on the desktop, support the weight of fuselage 1, and supporting arm 3 one ends combine with the upper surface of base 2, and the other end combines with fuselage 1 rear surface, and the load of fuselage 1 is sent to base 2.
Above-mentioned articulated elements 4 makes fuselage 1 can be connected obliquely up and down with supporting arm 3.
This articulated elements 4 is by hinge (not shown); A plurality of liners (washer) (not shown); And with respect to fuselage 1 sense of rotation, apply elastic force in the opposite direction, torsion (torsion) spring (not shown) that the torque (torque) that takes place because of deadweight with fuselage 1 offsets.
Thus, if apply external force,, be benchmark with sway brace 3 by articulated elements 4 to fuselage 1, static on the certain angle that the user requires when rotating up and down, keep the state of inclination.
But the bracket component of the flat-panel monitor under this prior art exists following problem.
At first, even by articulated elements, fuselage can rotate up and down, but the rotatable angle of fuselage has certain restriction, that is, because on the fuselage rotate path supporting arm is arranged, so the user can not rotate to an angle fuselage more than (about 90 °).
Secondly, supporting arm is fixed on base upper surface, and in the packing of product of wanting the cube minimum, the height of flat-panel monitor can not be reduced to below the supporting arm height.
Thus, the volume ratio of flat-panel monitor packing is bigger, may bring unnecessary expense in transportation and management.
Wall-hanging flat-panel display is is constantly researched and developed and is put goods on the market recently, considers this point, and the problems referred to above are badly in need of solving.
Summary of the invention
The present invention researches and develops for solving top problem.But its purpose is to provide a kind of free adjustment fuselage position, and when packing or being hung on the wall, volume can be reduced to the bracket component of minimum flat-panel monitor.
To achieve these goals, its formation of the bracket component of flat-panel monitor provided by the invention comprises as lower device: be arranged at the base on the desktop; Rotatably be combined in the 1st supporting arm of above-mentioned base one side; Rotatable the 2nd supporting arm that is combined in the upper end of the 1st supporting arm; And the fuselage back of being fixed in display image, form rotatable the 3rd supporting arm that combines with the 2nd supporting arm upper end.
In above-mentioned base one side, be formed with fuselage when folding, for folding the 1st opening portion of inserting of the 1st supporting arm.Be formed with fuselage on the 1st supporting arm top when folding, for folding the 2nd opening portion of inserting of the 2nd supporting arm.
In addition,, be formed with when the 3rd supporting arm rotates, be the 3rd opening portion that prevents to bump with the 2nd supporting arm on the top of the 2nd supporting arm.
In addition, above-mentioned the 2nd opening portion has the area that the 2nd supporting arm and the 3rd supporting arm are inserted simultaneously.
At this moment, above-mentioned the 1st, 2,3 supporting arms can have identical thickness with base.
On the other hand, the side of above-mentioned base is formed with the 1st fixed orifice.Be formed with in the side of the 1st supporting arm fuselage when folding with the 2nd fixed orifice of the 1st fixed orifice perforation.The side of above-mentioned the 2nd supporting arm is formed with fuselage when folding and the 3rd fixed orifice that is connected of the 1st, 2 fixed orifice.
In addition, be inserted with fuselage in above-mentioned the 1st, 2,3 fixed orifices when folding, be used for the 1st, 2 supporting arm is fixed on the fixed pin of base.
The bracket component of flat-panel monitor of the present invention has following effect.
At first, the present invention is equipped with three supporting arms, the fuselage freedom is rotated up and down and highly adjusting up and down, and can move horizontally.Thus, the user can more freely move to fuselage the angle and the position of requirement.
The second, each supporting arm of the present invention can be folded on the base fully, like this, for packing or hang fuselage when folding, can reduce the volume of flat-panel monitor to greatest extent.
Description of drawings
Fig. 1 is the flat-panel monitor synoptic diagram according to prior art;
Fig. 2 is the side schematic view of flat-panel monitor of the present invention;
Fig. 3 is the bracket component detailed maps of flat-panel monitor of the present invention;
Fig. 4 is by bracket component of the present invention, the state side schematic view that fuselage can rotate up and down;
Fig. 5 a and Fig. 5 b utilize bracket component of the present invention, the side schematic view that fuselage folds.
Accompanying drawing major part symbol description
10: 20: the 3 supporting arms of fuselage
31: the 3 fixed orifices of 30: the 2 supporting arms
40: the 1 supporting arms in 32: the 3 opening portions
42: the 2 opening portions of 41: the 2 fixed orifices
50: 51: the 1 fixed orifices of base
60: the 3 articulated elements in 52: the 1 opening portions
80: the 1 articulated elements of 70: the 2 articulated elements
90: fixed pin
Embodiment
Below, with reference to accompanying drawing desirable embodiment of the present invention is described.In the process of explanation embodiment, use identical title and symbol for identical formation, no longer apply and state.
Fig. 2 is the side schematic view according to flat-panel monitor of the present invention; Fig. 3 is the bracket component synoptic diagram according to flat-panel monitor of the present invention.
With reference to Fig. 2 and Fig. 3, its formation of the bracket component of flat-panel monitor of the present invention comprises: base 50, the 1 supporting arms 40, the 2 supporting arms 30, and the 3rd supporting arm 20.
Above-mentioned base 50 is arranged at desktop, supports the weight of the fuselage 10 that is used for display image.
At this moment, above-mentioned base 50 is made of the metal material with certain intensity and weight in order stably to support fuselage 10.In addition, above-mentioned base 50 has enough contacts area with desktop, and fuselage 10 is in external force or under conducting oneself with dignity about not meeting or rock back and forth like this.
In addition, though not shown, below base 50, be formed with the padded coaming of a plurality of elastic materials.Above-mentioned padded coaming is for the damage of 50 pairs of desktops of base of preventing metal material.Also disperseed simultaneously the fuselage weight that applies to desktop.Sort buffer material 50 is formed by rubber (rubber), in connecting below by fixed pin of base 50.
Above-mentioned the 1st supporting arm 40 rotatably is combined in base 50 1 ends, is provided with the 1st articulated elements 80 in the joint portion of above-mentioned the 1st supporting arm 40 and above-mentioned base 50.
Above-mentioned the 1st articulated elements 80 is by hinge (not shown); A plurality of liners (washer) (not shown); And, apply elastic force in the opposite direction with respect to fuselage 1 sense of rotation, offset torsion (torsion) spring (not shown) of the torque (torque) that fuselage 1 deadweight produces.
Thus, if the 1st above-mentioned supporting arm 40 is applied with external force, be that the center rotates up and down with the 1st articulated elements 80, when removing external force, can keep static state according to torque spring, the user can rotate to desired angle with the 1st supporting arm 40 by the 1st articulated elements 80.
Certainly, the structure of above-mentioned the 1st articulated elements 80 is not limited to the foregoing description.Above-mentioned the 1st articulated elements 80 its formations also comprise following form: a plurality of liners (washer); Generate friction, when removing external force, fuselage 10 is maintained the disc type spring (disk spring) (not shown) of halted state.
Above-mentioned the 2nd supporting arm 30 rotatably is combined in the upper end of the 1st supporting arm 40, for this reason, in the binding site of above-mentioned the 2nd supporting arm 30 and the 1st supporting arm 40, is provided with the 2nd articulated elements 70 with the 1st articulated elements 80 same structures.
Thus, when when the 2nd supporting arm 30 applies external force, be that the center rotates up and down with above-mentioned the 2nd articulated elements 70, when removing external force, keep static state by torque spring.
Above-mentioned the 3rd supporting arm 20 is fixed on fuselage 10 back, and rotatably combines with the upper end of the 2nd supporting arm 30.
That is, be formed with fixed projection 21, be formed with the 3rd articulated elements 60 at the binding site of above-mentioned the 3rd supporting arm 20 and the 2nd supporting arm 30 at the front surface of the 3rd supporting arm 20.
The rear surface that above-mentioned fixed projection 21 inserts fuselage 10 is fixed on the 3rd supporting arm 20 on the fuselage 10.Certainly, above-mentioned the 3rd supporting arm 20 also can be fixed on the back of fuselage 10 by screw.
And above-mentioned the 3rd articulated elements 60 has and above-mentioned the 1st, 2 articulated elements 80,70 identical construction, also has identical effect.That is, when applying external force, the 3rd supporting arm 20 is that the center rotates up and down with the 3rd articulated elements 60, and when removing external force, keeps static state by torque spring.
At this moment, when the 3rd supporting arm 20 rotated up and down, the fuselage 10 that is fixed on above-mentioned the 3rd supporting arm 20 was also with 20 rotations of the 3rd supporting arm.As a result, the rotation up and down of above-mentioned fuselage 10 is that the center rotates and finishes by the 3rd supporting arm 20 with the 3rd articulated elements 60.
On the other hand, when a side of above-mentioned base 50 is formed with folding (folding) fuselage 10, for the 1st supporting arm 40 folding the 1st opening portions 52 of inserting.
The folding of fuselage 10 refers to, and when packing or wall hanging use, for farthest reducing the volume of flat-panel monitor, fuselage 10 can be layered on top (with reference to Fig. 5 b) of base 50 abreast.
When fuselage 10 folded, above-mentioned the 1st supporting arm 40 was that the center is rotated with the 1st articulated elements 80, and folding above base 50, and at this moment, above-mentioned the 1st supporting arm 40 is inserted in the 1st opening portion 52.
In addition, on the top of the 1st supporting arm 40, be formed with fuselage 10 when folding, for the 2nd supporting arm 30 folding the 2nd opening portions 42 of inserting.
That is, when fuselage 10 was folding, the 2nd supporting arm 30 was be that the center is rotated with the 2nd articulated elements 70, and at this moment, the 2nd supporting arm 30 folds to the 1st supporting arm 40 directions, and is inserted in the 2nd opening portion 42.
Like this, when fuselage 10 folded, the 1st supporting arm 40 inserted the 1st opening portion 52, the 2 supporting arms 30 and inserts the 2nd opening portion 42.
When fuselage 10 folding finishing, the 1st, 2 supporting arm 40,30 all is arranged in the 1st opening portion 52, promptly in 52 outsides, the 1st opening portion the 1st supporting arm 40 is arranged, and there is the 2nd supporting arm 30 its inboard.
In addition, be formed with on the top of the 2nd supporting arm 30 when 20 rotations of the 3rd supporting arm, be used to prevent the 3rd opening portion 32 that collides with the 2nd supporting arm 30.
Above-mentioned the 3rd opening portion 32 has certain area, and 20 rotations of the 3rd supporting arm are passed through, and can make the rotation up and down freely of the 3rd supporting arm 20.
Specifically, above-mentioned the 3rd supporting arm 20 is an axle with the 3rd articulated elements 60, can carry out 180 ° of rotations, and thus, fuselage 10 also can carry out 180 ° of rotations.
On the other hand, when fuselage 10 folded, the 3rd supporting arm 20 also together inserted the 2nd opening portion 42 with the 2nd supporting arm 30.For this reason, the 2nd opening portion 42 has the area that the 2nd supporting arm 30 and the 3rd supporting arm 20 are inserted simultaneously.
When fuselage 10 folds, be formed with the 1st opening portion 52 in the base 50, can allow all folding insertion of the 1st, 2,3 supporting arms 40,30,20 wherein.
Here, the 1st, 2,3 supporting arms 40,30,20 preferably have identical thickness with base 50.Like this, after fuselage 10 was folding, the flat-panel monitor integral thickness was the thickness (with reference to Fig. 5 b) of the thickness addition of the thickness of fuselage 10 and base 50.
That is, above-mentioned the 1st, 2,3 supporting arms 40,30,20 are because be inserted into the 1st opening portion 52 that is formed in the base 50, so when seeing from the side, the outstanding any supporting arm in base 50 tops.
On the other hand, the user packs or is hung on wall after fuselage 50 is folded, mobile display, at this moment, because the deadweight of fuselage 10 or the mobile middle impact that produces, the 1st, 2 supporting arms 40,30 might occur and launch, perhaps the untenable situation of fuselage 10 folded states.Like this, after fuselage 10 folds, be necessary the 1st, 2 supporting arms 40,30 more firmly are fixed on the base 50.
For this reason, in the side of base 50, be formed with the 1st fixed orifice 51, and in the side of the 1st supporting arm 40, be formed with when fuselage 10 folds the 2nd fixed orifice 41 that is connected with the 1st fixed orifice 51.
In addition, in the 2nd supporting arm 30 sides, be formed with when fuselage 10 is folding and the 3rd fixed orifice 31 that the 1st, 2 fixed orifices 51,41 are connected.
In addition, in above-mentioned the 1st, 2,3 fixed orifices 51,41,31, when fuselage 10 is folding, is inserted with and makes the 1st, 2 supporting arm 40,30 be fixed on fixed pin 90 on the base 50.Thus, just can be securely fixed on the base 50 by fixed pin 90 the 1st, 2 supporting arms 40,30.
Certainly, in the 3rd supporting arm 20, can also be formed with the fixed orifice that is used to insert fixed pin 90.In addition, each fixed orifice also can form one respectively on the two sides of base 50 or the 1st, 2 supporting arm 40,30.
With reference to accompanying drawing, the fuselage in the bracket component of the present invention 10 is rotated up and down and fuselage 10 folding processes carry out schematic illustration.
Fig. 4 is according to bracket component of the present invention, the state side schematic view that fuselage rotates up and down.
With reference to Fig. 4, the user pushes away the upside of fuselage 10, and the 3rd supporting arm 20 that is fixed on fuselage 10 back is that the center is rotated in the direction of the clock with the 3rd articulated elements 60, and thus, fuselage 10 also together is rotated in the direction of the clock with the 3rd supporting arm 20.
At this moment, above-mentioned the 3rd supporting arm 20 can carry out 180 ° rotation, so shown in Fig. 4 dotted line, the people who is sitting in position, user opposite also can rotate fuselage 10, watches the image that shows in the fuselage 10.
Afterwards, by the angle of user's requirement, fuselage 10 rotations, when removal was applied to the applied external force of fuselage 10, fuselage 10 passed through the torque spring of formation the 3rd articulated elements 60 etc., keeps stationary state.
Fig. 5 a and Fig. 5 b utilize bracket component of the present invention, the process side schematic view that fuselage is folded.
With reference to Fig. 5 a, the user rotates the 3rd supporting arm 20 for folding fuselage 10, make fuselage 10 and base 50 keep horizontalitys after, fuselage 10 is pushed away downwards.
At this moment, above-mentioned the 1st supporting arm 40 is that the center is rotated counterclockwise with the 1st articulated elements 80, and folding to base 50.Above-mentioned the 2nd supporting arm 30 is that the center turns clockwise with the 2nd articulated elements 70, and is folding to the 1st supporting arm 40.
In this state, if continue to apply external force to fuselage 10, the 1st supporting arm 40 inserts the 1st opening portion 52 that is formed in the base 50, and above-mentioned the 2nd supporting arm 30 inserts the 2nd opening portion 42 that is formed in the 1st supporting arm 40.At this moment, above-mentioned the 3rd supporting arm 20 also together inserts the 2nd opening portion 42 with the 2nd supporting arm 30.
Thus, shown in Fig. 5 b, above-mentioned the 1st, 2,3 supporting arms 40,30,20 and base 50 are folding fully, and the fuselage 10 folding flat-panel monitors of finishing have the height that equates with base 50 and fuselage 10 thickness.
When fuselage 10 folding finishing, the flat-panel monitor overall volume can reduce widely.
In addition, during fuselage 10 folding finishing, the user inserts the 1st fixed orifice 51 with fixed pin 90.At this moment, the 2nd, 3 fixed orifice 41,31 that is formed in the 1st, 2 supporting arms 40,30 is kept the state that is connected with the 1st fixed orifice 51, so fixed pin 90 connects the 1st, 2 fixed orifices 41,31, and is inserted into the 3rd fixed orifice 31.
Like this, the 1st, 2 supporting arms 40,30 securely are fixed on the base 50 by said fixing pin 90, and when needing mobile flat-panel monitor in order to pack or be hung on wall, fuselage 10 self or outside impact can not cause removing the folding situation of fuselage 10.
On the other hand, use bracket component of the present invention, also can carry out fuselage 10 adjusting of height up and down.Fuselage 10 highly regulate up and down by the user with fuselage 10 downwards by or catch fuselage 10 upwards to draw and finish.
At first, in the time of reducing the height of fuselage 10, the user presses fuselage 10 downwards, and the 1st, 2 supporting arms 40,30 were rotated and folded along clockwise direction or counterclockwise by the effect of external force this moment.
Thus, the height of the 1st, 2 supporting arms 40,30 can reduce, and then has reduced the height of fuselage 10.
In addition, by above-mentioned the 1st, 2 supporting arms 40,30, also can carry out fuselage 10 front and back and move horizontally.That is, the user to pusher or draw forward, 40,30 rotations of the 1st, 2 supporting arms are flatly moved fuselage 10 front and back with fuselage 10.
The front and back of this fuselage 10 move horizontally with above-mentioned fuselage 10 up and down the height adjustment process similar, so no longer describe.
By above-mentioned description, relevant speciality personnel can carry out various change and modification fully in the scope that does not depart from the technology of the present invention thought.Therefore, technical scope of the present invention is not limited to the content on the instructions, must determine its technical scope according to interest field.
Claims (8)
1. the bracket component of a flat-panel monitor is characterized in that, comprising:
Be arranged at the base on the desktop;
Rotatable the 1st supporting arm that is combined in above-mentioned base one side;
Rotatable the 2nd supporting arm that is combined in above-mentioned the 1st supporting arm upper end; And
Be fixed in the fuselage rear surface of display image, rotatable the 3rd supporting arm that is combined in above-mentioned the 2nd supporting arm upper end.
2. the bracket component of flat-panel monitor according to claim 1 is characterized in that:
Be formed with in above-mentioned base one side, when fuselage is folding, for folding the 1st opening portion of inserting of above-mentioned the 1st supporting arm.
3. as the bracket component of flat-panel monitor as described in the claim 2, it is characterized in that:
Be formed with on above-mentioned the 1st supporting arm top, when fuselage is folding, for folding the 2nd opening portion of inserting of the 2nd supporting arm.
4. as the bracket component of flat-panel monitor as described in the claim 3, it is characterized in that:
Top at above-mentioned the 2nd supporting arm is formed with, and when the 3rd supporting arm rotates, prevents the 3rd opening portion that itself and the 2nd supporting arm bump.
5. as the bracket component of flat-panel monitor as described in the claim 4, it is characterized in that:
Above-mentioned the 2nd opening portion has the area that the 2nd supporting arm and the 3rd supporting arm are inserted simultaneously.
6. as the bracket component of flat-panel monitor as described in the claim 5, it is characterized in that:
Above-mentioned the 1st, 2,3 supporting arms have identical thickness with base.
7. as the bracket component of flat-panel monitor as described in the claim 2, it is characterized in that:
The side of above-mentioned base is formed with the 1st fixed orifice;
Side at the 1st supporting arm is formed with, the 2nd fixed orifice that is communicated with the 1st fixed orifice when fuselage is folding;
The side of above-mentioned the 2nd supporting arm is formed with, the 3rd fixed orifice that fuselage is connected with above-mentioned the 1st, 2 fixed orifices when folding.
8. as the bracket component of flat-panel monitor as described in the claim 7, it is characterized in that:
Be inserted with in above-mentioned the 1st, 2,3 fixed orifices, fuselage is used for the 1st, 2 supporting arms are fixed on the fixed pin of base when folding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2006100966703A CN101165814A (en) | 2006-10-17 | 2006-10-17 | Panel display bracket assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNA2006100966703A CN101165814A (en) | 2006-10-17 | 2006-10-17 | Panel display bracket assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN101165814A true CN101165814A (en) | 2008-04-23 |
Family
ID=39334457
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNA2006100966703A Pending CN101165814A (en) | 2006-10-17 | 2006-10-17 | Panel display bracket assembly |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101165814A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009135366A1 (en) * | 2008-05-08 | 2009-11-12 | 东莞宜安电器制品有限公司 | A folding stand |
| CN104913165A (en) * | 2014-03-10 | 2015-09-16 | 联想(北京)有限公司 | Electronic device |
| CN104932610A (en) * | 2014-03-17 | 2015-09-23 | 联想(北京)有限公司 | Electronic device |
| CN114370575A (en) * | 2022-01-19 | 2022-04-19 | 北京博瑞翔伦科技发展有限公司 | Position-adjustable positioning support for underground wireless AP |
-
2006
- 2006-10-17 CN CNA2006100966703A patent/CN101165814A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009135366A1 (en) * | 2008-05-08 | 2009-11-12 | 东莞宜安电器制品有限公司 | A folding stand |
| CN104913165A (en) * | 2014-03-10 | 2015-09-16 | 联想(北京)有限公司 | Electronic device |
| CN104932610A (en) * | 2014-03-17 | 2015-09-23 | 联想(北京)有限公司 | Electronic device |
| CN114370575A (en) * | 2022-01-19 | 2022-04-19 | 北京博瑞翔伦科技发展有限公司 | Position-adjustable positioning support for underground wireless AP |
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Open date: 20080423 |