Backplane

Abstract

The present disclosure discloses a backplane comprises a backplane main body and a stiffener assembly disposed on the surface of the backplane main body, the stiffener assembly comprises a first inclined rib extending from each corner of the backplane main body toward the center and a second inclined rib surrounding triangle areas with every corners; wherein, the first inclined rib sets up a cross relative to the nearest second inclined rib. The surface of the backplane main body comprises a stiffener assembly with a plurality of stiffener ribs, a first inclined rib extending from each corner toward the center, and a second inclined rib disposed at every corners.

Description

BACKGROUND OF THE INVENTION

1. Field of the Invention

The invention relates to display technology field, in particular to a backplane.

2. The Related Arts

To comply with develop of economic society and display technology, the requirement of size of flat-panel television is larger than before for people. The larger corresponding liquid crystal module, the more complicated whole equipment process is. Extra cost is even needed to solve some reliability problems. After forming, a large size of backplane will be deformed, even unstable curvature if the backplane is curved surface.

As shown in FIG. 1a and FIG. 1b, the traditional approach is adding crisscrossed stiffeners a (as shown in FIG. 1) or extra braces (as shown in FIG. 2) on the surface of backplane 1 to ensure the strength and stuffiness of whole backplane; however, the problem that whole backplane is deformed, especially in corners could not be solved very well.

SUMMARY

In view of the disadvantages in the conventional art, a backplane with deformation, reliable structures and low cost is provided in the present disclosure.

In order to achieve the aforementioned objects, the present disclosure provides the technical solutions as following:

A backplane comprises a backplane main body and a stiffener assembly disposed on the surface of the backplane main body, the stiffener assembly comprises a first inclined rib extending from each corner of the backplane main body toward the center and a second inclined rib surrounding triangle areas with every corners; wherein, the first inclined rib sets up a cross relative to the nearest second inclined rib.

Further, the extending terminal point of the first inclined rib is located on the second inclined rib.

Further, the first inclined rib is perpendicular to the second inclined rib.

Further, the first inclined rib is collinear with the angular bisector of a corner on which located the first inclined rib.

Further, an end of the second inclined rib is located at the middle point of the short side of the backplane main body.

Further, another end of the second inclined rib is located at the one-third point of the long side of the backplane main body.

Further, the stiffener assembly further comprises four third inclined ribs, and the third inclined ribs form a closed quadrilateral located at the center of the backplane main body.

Further, the angular bisectors of the quadrilateral match together with the two symmetry axes of the backplane main body.

Further, the quadrilateral is a square.

Further, the stiffener assembly further comprises at least one fourth inclined rib, and the fourth inclined rib is a diagonal connected between the two opposing corners of the square.

The surface of the backplane main body of the present disclosure comprises a stiffener assembly with a plurality of stiffener ribs, a first inclined rib extending from each corner toward the center, and a second inclined rib disposed at every corners. Triangle areas are surrounded by the second inclined rib and corners corresponding to the second inclined rib, and the first inclined rib sets up a cross relative to the nearest second inclined rib to increase deformation ability, strengthening force, structural reliability and low cost.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1a is a structural schematic diagram showing a backplane of the previous disclosure.

FIG. 1b is a structural schematic diagram showing another backplane of the previous disclosure.

FIG. 2 is a structural schematic diagram showing a backplane of an embodiment in the disclosure.

FIG. 3 is a structural schematic diagram showing a backplane of another embodiment in the disclosure.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

In order to make the objects, technical solution and advantages of the present disclosure will become apparent from the accompanying drawings and the following embodiments, the present disclosure will be described in further detail. It should be understood that the specific embodiment described herein are only for explaining the present disclosure and are not intended to limit the present disclosure.

The backplane of the disclosure can be utilized in varies kinds of display devices. Please refer to FIG. 2, the backplane of the disclosure comprises a backplane main body 10 and a stiffener assembly 20 disposed on the surface of the backplane main body 10; the stiffener assembly 20 comprises a first inclined rib 21 extending from each corner of the backplane main body 10 toward the center and a second inclined rib 22 surrounding triangle areas with every corner; wherein, the first inclined rib sets up a cross relative to the nearest second inclined rib.

Every corner can be strengthened to increase strengthening forces at deformation portions of the backplane, both flat backplane and curved backplane, by this technology in the disclosure.

The backplane main body 10 is a standard curved board or rectangular board with long sides of length direction and short sides of width directions, horizontal symmetry axis X and vertical symmetry axis Y of backplane main body 10 are symmetrical, and the two symmetry axes divide the backplane main body 10 into four small subareas; wherein, horizontal symmetry axis X and vertical symmetry axis Y of stiffener assembly 20 are symmetrical, in other words, two symmetry axes of four first inclined ribs 21 and four second inclined ribs 22 related to the backplane main body 10 are both symmetrical. Therefore, whole backplane main body 10 can be ensured to have symmetrical standard force, and curvature stability of backplane can be ensured even inside curved backplane,

Further, the extending terminal point of the first inclined rib 21 is located on the second inclined rib 22 to save unnecessary extending lengths; the first inclined rib 21 is perpendicular to the second inclined rib 22 and intersects in the midpoint with the second inclined rib 22; every first inclined rib 22 is collinear with the angular bisector of a corner on which located the first inclined rib 22, in the other words, the included angles between the second inclined rib 22 and both long sides and short sides of backplane main body 10 are all 45°. Furthermore, an end of the second inclined rib 22 is located at the middle point of the short side of the backplane main body 10, and another end of the second inclined rib 22 is located at the one-third point of the long side of the backplane main body 10.

Meanwhile, the stiffener assembly 20 further comprises four third inclined ribs 23, and the third inclined ribs 23 form a closed quadrilateral located at the center of the backplane main body 10 to further confirm no deformation situation occurred in the whole backplane, and further strengthen strength and stuffiness of backplane. Here, the angular bisectors of the quadrilateral match together with the two symmetry axes of the backplane main body 10. Furthermore, the third inclined ribs 23 are parallel to the second inclined ribs 22 on the same subarea to obtain a quadrilateral as a square, and two corners of the square are located at midpoints of long sides of backplane main body 10. It is known that inclined angles of inclined ribs can be adjusted if necessary.

As shown in FIG. 3, FIG. 3 is another backplane structure of an embodiment in the present disclosure, wherein, the stiffener assembly 20 further comprises at least one fourth inclined rib 24, and the fourth inclined rib 24 is parallel to the long sides and connected between the two opposing corners of the square to further enhance curvature of backplane for reducing structure of external frame support in conditional curve backplane, decreasing component costs, saving researching and developing cost in molding in external frame support, and then increasing compatibilities of whole product.

The above description is only the specific embodiment of the present application, it should be noted that those of ordinary skill in the art, in this disclosure without departing from the principles of the premise, but also a number of improvements modifications can be made, these improvements and modifications are to be considered the scope of the present disclosure.

Claims

1. A backplane, wherein, comprises a backplane main body and a stiffener assembly disposed on the surface of the backplane main body, the stiffener assembly comprises a first inclined rib extending from each corner of the backplane main body toward the center and a second inclined rib surrounding triangle areas with every corner; Wherein, the first inclined rib sets up a cross relative to the nearest second inclined rib.

2. The backplane according to claim 1, wherein, the extending terminal point of the first inclined rib is located on the second inclined rib.

3. The backplane according to claim 1, wherein, the first inclined rib is perpendicular to the second inclined rib.

4. The backplane according to claim 3, wherein, the first inclined rib is collinear with the angular bisector of a corner on which located the first inclined rib.

5. The backplane according to claim 1, wherein, an end of the second inclined rib is located at the middle point of the short side of the backplane main body.

6. The backplane according to claim 5, wherein, another end of the second inclined rib is located at the one-third point of the long side of the backplane main body.

7. The backplane of claim 5, wherein, the stiffener assembly further comprises four third inclined ribs, and the third inclined ribs form a closed quadrilateral located at the center of the backplane main body.

8. The backplane according to claim 7, wherein, the angular bisectors of the quadrilateral match together with the two symmetry axes of the backplane main body.

9. The backplane according to claim 8, wherein, the quadrilateral is a square.

10. The backplane according to claim 8, wherein, the stiffener assembly further comprises at least one fourth inclined rib, and the fourth inclined rib is a diagonal connected between the two opposing corners of the square.

11. The backplane according to claim 2, wherein, an end of the second inclined rib is located at the middle point of the short side of the backplane main body.

12. The backplane according to claim 11, wherein, another end of the second inclined rib is located at the one-third point of the long side of the backplane main body.

13. The backplane of claim 11, wherein, the stiffener assembly further comprises four third inclined ribs, and the third inclined ribs form a closed quadrilateral located at the center of the backplane main body.

1. The backplane according to claim 13, wherein, the angular bisectors of the quadrilateral match together with the two symmetry axes of the backplane main body.

15. The backplane according to claim 14, wherein, the quadrilateral is a square.

16. The backplane according to claim 14, wherein, the stiffener assembly further comprises at least one fourth inclined rib, and the fourth inclined rib is a diagonal connected between the two opposing corners of the square.

17. The backplane according to claim 4, wherein, an end of the second inclined rib is located at the middle point of the short side of the backplane main body.

18. The backplane according to claim 17, wherein, another end of the second inclined rib is located at the one-third point of the long side of the backplane main body.

19. The backplane of claim 17, wherein, the stiffener assembly further comprises four third inclined ribs, and the four third inclined ribs form a closed quadrilateral located at the center of the backplane main body.

20. The backplane according to claim 19, wherein, the angular bisectors of the quadrilateral match together with the two symmetry axes of the backplane main body.